Hans J. Kupka
Transitions in Molecular Systems
Hans J. Kupka Transitions in Molecular Systems
Hans J. Kupka
Transitions in Molecular Systems
The Author Prof. Hans J. Kupka Düsseldorf, Germany
[email protected] Cover Picture A representation of the multi-dimensional FC factor at different rotations between the normal coordinates.
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V
Contents Preface
1 1.1 1.1.1 1.1.2 1.1.3 1.1.4 1.2 1.3 1.4 1.4.1 1.4.2 1.4.3
IX
Introduction 1 The Adiabatic Description of Molecules 1 Preliminaries 1 The Born–Oppenheimer Approximation 3 The Crude Born–Oppenheimer Basis Set 6 Correction of the Crude Adiabatic Approximation 7 Normal Coordinates and Duschinsky Effect 9 The Vibrational Wavefunctions 13 The Diabatic Electronic Basis for Molecular Systems 14 Preliminaries 14 Conical Intersection Between the States B˜ 2B2/2A0 and A˜ 2A1/2A0 of H2Oþ 16 The Linear Model for Conical Intersection 18
2.2
Formal Decay Theory of Coupled Unstable States 21 The Time Evolution of an Excited State 21 Some Remarks About the Decay of a Discrete Molecular Metastable State 26 The Choice of the Zero-Order Basis Set 27
3 3.1 3.2 3.2.1 3.2.2 3.2.3 3.2.4 3.2.5 3.2.6
Description of Radiationless Processes in Statistical Large Molecules Evaluation of the Radiationless Transition Probability 31 The Generating Function for Intramolecular Distributions I1 and I2 The Generating Function G2(w1,w2,z1,z2) 36 Properties of dm1m2, n1n2, am1m2, n1n2, and bm1m2, n1n2 41 Case w1 ¼ w2 ¼ 0 42 Case w1 6¼ w2 6¼ 0 42 Symmetry Properties of I2 45 Case w ¼ 0 47
2 2.1 2.1.1
31 36
VI
Contents
3.3 3.4
Derivation of the Promoting Mode Factors Kg(t) and Ig(t) 48 Radiationless Decay Rates of Initially Selected Vibronic States in Polyatomic Molecules 52
4 4.1 4.1.1 4.2 4.2.1 4.2.2 4.2.3 4.2.4 4.2.5 4.2.6 4.3 4.3.1 4.3.2 4.3.3 4.3.3.1 4.4 4.4.1 4.4.2 4.4.3 4.4.3.1 4.4.4 4.4.5 4.4.6 4.4.7 4.4.8 4.5 4.5.1 4.5.2 4.6
Calculational Methods for Intramolecular Distributions I1, I2, and IN 57 The One-Dimensional Distribution I1(0, n; a, b) 57 The Addition Theorem 60 The Distributions I1(m, n; a, b) 61 Derivation of I1(m, n; a, b) 61 The Addition Theorem for I1(m, n; a, b) 65 The Recurrence Formula 65 Case b ¼ 0 67 Case b 6¼ 0 68 Numerical Results 69 Calculation of the Multidimensional Distribution 71 Preliminary Consideration 71 Derivation of Recurrence Equations 75 The Calculation Procedure 78 Some Numerical Results 79 General Case of N-Coupled Modes 82 The Generating Function GN 82 Properties of dm,n, am,n, and bm,n 87 The Distribution and its Properties 89 Symmetry Property of IN 91 A Special Case 92 Concluding Remarks and Examples 93 Recurrence Relations 94 The Three-Dimensional Case 96 Some Numerical Results 97 Displaced Potential Surfaces 102 The Strong Coupling Limit 102 The Weak Coupling Limit 106 The Contribution of Medium Modes 107
5 5.1 5.2
The Nuclear Coordinate Dependence of Matrix Elements The q-Centroid Approximation 111 Determination of the q-Centroid 123
6 6.1 6.2 6.3 6.3.1 6.3.2
Time-Resolved Spectroscopy 129 Formal Consideration 129 Evaluation of the Radiative Decay Probability of a Prepared State The Sparse Intermediate Case 137 Preliminary Consideration 137 The Molecular Eigenstates 139
111
131
Contents
6.4 6.5 6.5.1 6.5.2 6.5.3 6.5.4 7 7.1 7.1.1 7.1.2 7.1.2.1 7.2 7.2.1 7.2.2 7.2.3 7.2.3.1 7.2.4 7.3 7.4 7.4.1 7.5 7.5.1 7.5.2 7.5.3 7.5.4 7.5.5 7.5.6 7.6 7.6.1 7.6.2 7.6.2.1 7.6.2.2
8 8.1 8.1.1 8.1.2 8.2
Radiative Decay in Internal Conversion by Introduction of Decay Rates for {y1} 142 Dephasing and Relaxation in Molecular Systems 145 Introduction 145 Interaction of a Large Molecule with a Light Pulse 146 Free Induction Decay of a Large Molecule 149 Photon Echoes from Large Molecules 151 Miscellaneous Applications 155 The Line Shape Function for Radiative Transitions 155 Derivation 155 Implementation of Theory and Results 160 Excited-State Geometry 169 On the Mechanism of Singlet–Triplet Interaction 171 Phosphorescence in Aromatic Molecules with Nonbonding Electrons 171 Radiative T1 (pp)!S0 Transition 172 Nonradiative Triplet-to-Ground State Transition 178 Theory and Application 179 Remarks on the Intersystem Crossing in Aromatic Hydrocarbons Comment on the Temperature Dependence of Radiationless Transition 184 Effect of Deuteration on the Lifetimes of Electronic Excited States Partial Deuteration Experiment 186 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals 191 Transport Phenomena in Doped Molecular Crystals 191 The System Pentacene in p-Terphenyl 191 Techniques 194 Nature of the Energy Transfer: Theory 198 Time Evolution of the Guest Excitations 201 The Decay of the Transient Grating Signal 208 Electronic Predissociation of the 2B2 State of H2Oþ 211 Evaluation of the Nonadiabatic Coupling Factor 211 The Basis State Functions 216 The Initial-State Wavefunction xi 216 The Final Vibrational Wavefunction xf : The Closed Coupled Equations 217 Multidimensional Franck–Condon Factor 225 Multidimensional Franck–Condon Factors and Duschinsky Mixing Effects 225 General Aspects 225 Derivation 228 Recursion Relations 238
183
186
VII
VIII
Contents
8.3 8.4 8.4.1 8.4.2 8.4.3 8.5
Some Numerical Results and Discussion 241 Implementation of Theory and Results 244 The Resonance Raman Process and Duschinsky Mixing Effect 244 Time-Delayed Two-Photon Processes: Duschinsky Mixing Effects 247 Results 249 The One-Dimensional Franck–Condon Factor (N ¼ 1) 255 Appendices
A.1 A.2
259
Appendix A: Some Identities Related to Greens Function The Greens Function Technique 261 Evaluation of the Diagonal Matrix Element of Gss 264
261
Appendix B: The Coefficients of the Recurrence Equation
267
Appendix C: The Coefficients of the Recurrence Equations Appendix D: Solution of a Class of Integrals
271
273
Appendix E: Quantization of the Radiation Field
277
Appendix F: The Molecular Eigenstates 281 Appendix G: The Effective Hamiltonian and Its Properties
285
H.1 H.2
Appendix H: The Mechanism of Nonradiative Energy Transfer Single-Step Resonance Energy Transfer 287 Phonon-Assisted Energy Transfer 289
I.1
Appendix I: Evaluation of the Coefficients bmn, cmn, and bm in the Recurrence Equations 8.28 and 8.29 293 Application 294
287
Appendix J: Evaluation of the Position Expectation Values of xsm(qs) 299 Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect 301 References Index
327
313
IX
Preface The analysis of electronic relaxation processes, especially of radiationless transitions in molecular systems, has rapidly evolved in the last few decades and today plays a central role in almost all investigations of molecular physics and spectroscopy. The development of lasers has significantly contributed to this evolution. The purpose of this book is to give a self-contained and unified presentation of this development, with applications to molecular and solid-state physics. It is primarily intended for graduate students in theoretical physics and chemistry, who are beginning their research careers, although it is hoped that any physicist and chemist working with lasers, molecular spectroscopy, and solid-state physics will also find it useful. The greatest possible emphasis has been placed on clarity, and to this end, presentation is often made in strict mathematical detail. I hope that the reader will thus be able to rederive many of the formulas presented without much difficulty. Some basic understanding of symmetry principles in solid state and molecular physics may be helpful for the reader. The book consists of eight chapters and several appendices. In Chapter 1, the different basis sets used to classify molecular eigenstates and to study molecular dynamics, including molecular vibrations, are discussed within the context of the Duschinsky mixing effect. This mixing caused by the normal coordinate rotation has been elucidated further in following chapters. In Chapter 2, the treatment of radiationless transition probability is presented on the basis of Greens function formulation for the transition amplitude, in which the states of interest are selected by suitable projection operators. A discussion of the proper basis set for describing electronic relaxation processes in large molecules is given for each of the cases treated. Chapter 3 provides a detailed description of radiationless processes in a statistical large molecule embedded in an inert medium. In this chapter, we are for the first time able to express the vibrational overlap between the electronic states under consideration in terms of intramolecular distributions in the full harmonic approximation taking into account the effects of vibrational frequency distortion, potential surface displacement, and the Duschinsky rotation. Chapter 4 deals in greater detail with the symmetry properties, the evaluation and presentation of the intramolecular distributions for arbitrary vibrational degrees of freedom.
X
Preface
An important example of the utility and power of the aforementioned intramolecular distributions is presented in Chapter 5. This chapter, which is of a more advanced nature, is entirely devoted to the investigation of the nuclear dependence of the electronic matrix element for radiationless transitions. It leads the reader, employing a class of integrals found in Appendix D, to a fix-point theorem for determining the q-centroid at which the electronic matrix element is to be evaluated. It is not recommended that the reader uninterruptedly attempt to master all of these derivations that lead to the proofs of the fundamental theorems. Instead, this chapter or a part of it, may be bypassed on the first reading, proceeding to the less complex following chapters and referring back, as necessary. Chapter 6 deals with the time evolution of radiative decaying states of polyatomic molecules with special emphasis on radiative decay in internal conversion. The decay of a manifold of closely spaced coupled states is handled by the Greens function formalism, where the matrix elements are displayed in an energy representation that involves either the Born–Oppenheimer or the molecular eigenstate basis set. The features of radiationless transitions in large, medium-sized, and small molecules are elucidated, deriving general expressions for the radiative decay times and for the fluorescence quantum yields. Chapter 7 introduces the reader to solutions of many selected problems in molecular physics. In particular, the following important problems are studied in detail: the fluorescence spectrum of p-terphenyl crystal, the vibrational fine structure of the spin-allowed absorption band of trans-[Co(CN)2(tn)2]Cl3H2O, and transport phenomena of electronic excitation in pentacene-doped molecular crystals. It is followed by an analysis of phosphorescence and radiationless transition in aromatic molecules with nonbonding electrons as well as predissociation of the 2B2 state of H2Oþ by nonadiabatic interaction via conical intersection. Finally, Chapter 8 deals with the evaluation of multidimensional Franck–Condon integrals. As an illustration of the complexity of the latter upon the normal mode rotation, a study of sequential two photon processes is presented. At the beginning of each chapter, there is a brief summary of what the reader will find in the particular chapter. These summaries provide a detailed survey of the subject matter covered in this book. No attempt was made to provide all-inclusive references. References are not prioritized and are presented as supplementary reading for students. Some people have made important contributions to this book at various stages of its development. In particular, I would like to mention here my scientific colleagues G. Olbrich, C. Kryschi, D. Gherban, A. Urushiyama, J. Degen, Th. Ledwig, and P.H. Cribb. In addition, I wish to express my deep appreciation to G. Moss for suggested improvements to text readability and to G. Pauli for preparing most of the graphics, which form an essential part of the presentation. December 2008 Düsseldorf, Germany
Hans J. Kupka
j1
1 Introduction
In this chapter we shall provide a brief overview of a number of different basis sets to classify molecular eigenstates and study molecular dynamics. The basic procedure is described in Section 1.1, where the solution of the Schr€ odinger equation for the molecular system is given by separating the electronic motion from the nuclear motion in the molecule. This procedure, called the adiabatic description, represents the basis set that most often describes the initially excited states in large molecules. Alternatively, Section 1.1.3 introduces the crude Born–Oppenheimer (BO) basis, and Section 1.1.4 gives a description of the Herzberg–Teller adiabatic approximation. Sections 1.2 and 1.3 are devoted to the vibrational wavefunctions and their normal coordinates as well as to the Duschinsky effect. Section 1.4 concludes the chapter with a mathematical analysis of two strongly coupled adiabatic states, one of the fundamental and difficult problems of physics. The analysis is performed by using a diabatic basis set, and as an application a formal and compact solution is derived for the predissociation of a triatomic molecule via a conical intersection. We assume that the reader is familiar with the basic notions of quantum theory. However, to make our study reasonably self-contained, we have included some of the derivations in the appendices.
1.1 The Adiabatic Description of Molecules 1.1.1 Preliminaries
In the treatment of electronic states in large molecules, one usually neglects the details concerning the rotation and translation motions and rather concentrates on the dynamics of the electronic and vibrational motions. The starting point for the description of these motions in a molecule consisting of electrons and K nuclei is the complete Hamiltonian H of the molecule. To write down the Hamiltonian, the origin of the molecular coordinate system is placed at the center of mass. It is assumed that the positions of the K nuclei will deviate only by small amounts from some reference
j 1 Introduction
2
configuration. The molecules with large amplitude motions, such as internal rotations, are therefore explicitly excluded. The nuclear inertia tensor is then approximated by the inertia tensor of the reference configuration and the axes of the internal coordinate system are directed along the principal axes of this reference inertia tensor. If now the center of mass motion is removed, the nuclear motion can be described by a vector of 3K 6 dimensions for a (nonlinear) system with K atoms. The latter are normally taken as linear combinations of mass-weighted vectors describing the displacements from the reference configuration [1–3]. With this approximation and, for the sake of simplicity, taking only the electrostatic Coulomb interaction, the vibronic Hamiltonian can be written as H ¼ Te ðrÞ þ TN ðqÞ þ Uðr; qÞ:
ð1:1Þ
Here the vector r ¼ (r1 ; r2 ; . . . ; rn ) where ri ¼ ðxi ; yi ; zi Þ denotes collectively all electronic coordinates and the coordinates of the nuclei are specified by q ¼ ðq1 ; q2 ; . . . ; qN Þ, where N ¼ 3K6. In the following, we shall adopt the convention that the components of the vector q are labeled by Greek indices if they range from 1 to N, and the Latin ones denote the components of the electronic coordinates. The electronic kinetic energy operator Te ðrÞ and the nuclear kinetic operator TN ðqÞ are presented in a diagonal form: X h2 q2 Te ðrÞ ¼ ð1:2Þ 2m qri2 i and TN ðqÞ ¼
X h2 m
2
! q2 ; qq2m
ð1:3Þ
where m is the mass of the electron and qm are mass-weighted (dimensioned) nuclear coordinates given by R ¼ R0 þ M1=2 Aq;
where R and R0 are ð3K6Þ-dimensional column vectors of the instantaneous and equilibrium Cartesian coordinates, respectively, associated with the nonzero frequency normal modes. M is the ð3K6Þ ð3K6Þ mass-weighted matrix, A is the orthogonal transformation that diagonalizes the mass-weighted Cartesian force constant matrix, and q is the dimensioned normal coordinate vector. Uðr; qÞ in Equation 1.1 is the total (internal) potential energy and includes all the electron–electron, nucleus–nucleus, and electron–nucleus interactions. In spite of the approximation already made, the exact molecular vibronic eigenstates Yðr; qÞ in a stationary state satisfy the time-independent Schr€ odinger equation ½Te ðrÞ þ TN ðqÞ þ Uðr; qÞ Yðr; qÞ ¼ E Yðr; qÞ:
ð1:4Þ
Serious approximations become necessary when one tries to solve Equation 1.4. One of these solutions is the adiabatic separation, which will be outlined below. This
1.1 The Adiabatic Description of Molecules
outline will serve as a guide to the possible classifications of molecular states and as an aid to the solution of specific quantum mechanical problems. 1.1.2 The Born–Oppenheimer Approximation
The first step of the adiabatic description is the Born–Oppenheimer approximation, according to which the nuclear kinetic energy is neglected, and the nuclear configuration is fixed at the position R. The adiabatic approximation is based on the fact that typical electronic velocities are much greater than typical nuclear (ionic) velocities. (The significant electronic velocity is v ¼ 108 cm=s, whereas typical nuclear velocities are at most of order 105 cm=s.) One therefore assumes that, because the nuclei have much lower velocities than the electrons, at any moment the electrons will be in their ground state for that particular instantaneous nuclear configuration. Under circumstances where TN ðqÞ ¼ 0, and at particular arrangement of the ion cores, we can separate electronic and nuclear motions. This can be accomplished by selecting some basis set of electronic wavefunctions ja ðr; qÞ, which satisfy the partial Schr€odinger equation ½Te ðrÞ þ Uðr; qÞ ja ðr; qÞ ¼ Ea ðqÞ ja ðr; qÞ;
ð1:5Þ
where Ea ðqÞ corresponds to the electronic energy at this fixed nuclear configuration. The configuration q is chosen arbitrarily, but for the solution of Equation 1.5 it must be fixed. In other words, the electronic wavefunction ja ðr; qÞ depends on the electronic coordinate r and parametrically on the nuclear coordinates. For any value of q, the ja are assumed to be orthonormal and complete (i.e., span the subspace defined by the electronic coordinates r). They are also assumed to vary in a continuous manner with q. The total (molecular) wavefunction Yðr; qÞ can be expanded in terms of the electronic basis function [4, 5] X Yv ðr; qÞ ¼ jb ðr; qÞxbv ðqÞ; ð1:6Þ b
where the nuclear wavefunctions xbv ðqÞ are initially treated as coefficients in the series (1.6). These coefficients are selected such that Equation 1.4 is satisfied. We have to substitute Equation 1.6 for Yðr; qÞ in Equation 1.4. Remarking that ! ! q2 ðjb xbv Þ q2 jb qjb qxbv q2 xbv xbv þ 2 ð1:7Þ ¼ þ jb qq2m qqm qqm qq2m qq2m and 2 q2 ðjb xbv Þ q jb ; ¼ xbv qri2 qri2
j3
j 1 Introduction
4
we find according to Equation 1.6 that ( X X Eb ðqÞjb ðr; qÞxbv ðqÞ þ TN ðqÞjb ðr; qÞxbv ðqÞ H jb xbv ¼ b
b
) X h2 qj ðr; qÞ qx ðqÞ bv b 2 þ jb ðr; qÞTN ðqÞxbv ðqÞ qqm qqm 2 m X ¼E jb ðr; qÞxbv ðqÞ: b
In deducing this result, we have used Equation 1.5 and the fact that the wavefunction jb is an eigenfunction of Equation 1.5. Multiplying from the left by ja and integrating over the electronic coordinates, we obtain the usual set of coupled equations for the xav [4, 5] (see also Ref. [6] with modifications given by McLachlan [7] and Kolos [8]): ½TN ðqÞ þ Ea ðqÞ þ hja jTN jja iE xav ðqÞ X X 2 þ ð h =2Þhja q=qqm jb ir q=qqm xbv ðqÞ ¼ 0: hja jTN ðqÞjjb ir 2 b6¼a
m
ð1:8aÞ
The restriction b 6¼ a in Equation 1.8a is a consequence of the orthonormality of the jb ; hjb jja ir ¼ dab . Here and in Equation 1.8a, angle brackets indicate integration over the electronic coordinates only. To avoid confusion resulting from numerous subscripts, it is often convenient to adopt a matrix notation, writing Equation 1.8a as ½TN ðqÞ þ Ea ðqÞ þ hja jTN ðqÞjja iE xav ¼
X b6¼a
Xab xbv ;
ð1:8bÞ
where Xab ¼ hja ½TN ; jb ir and ½A; B ¼ ABBA. The adiabatic approximation (or BO adiabatic approximation in the nomenclature of Ballhausen and Hansen) is obtained by neglecting the coupling term in Equation 1.8a (the expression in the curly brackets). The molecular wavefunction now reduces to the simple product Yav ðr; qÞ ¼ ja ðr; qÞxav ðqÞ
ð1:9Þ
and the corresponding equation for the nuclear function xav ðqÞ in this approximation has the form ½TN ðqÞ þ Ea ðqÞxav ðqÞ ¼ Eav xav ðqÞ;
ð1:10Þ
where Eav is the eigenvalue for the nth vibrational level in the ath electronic state. Thus, from Equations 1.5 and 1.10, we see that, in the BO approximation, the nuclei move in an effective potential Ea ðqÞ generated by the electron distribution, while the electron distribution is a function of the nuclear configuration q. Ea ðqÞ is designated as the adiabatic potential surface of ja . The additional diagonal term hja jTN ðqÞjja ir in Equation 1.8 is omitted in the BO approximation, as we have done in Equation 1.10. Alternatively, if this term (designated as the adiabatic correction to the potential energy surface) is taken into account, we speak of the Born–Huang approximation [5].
1.1 The Adiabatic Description of Molecules
From numerical calculations of the low-lying electronic states of H2 þ and H2 , it is known that this correction is invariably small [9, 10] and can usually be neglected. The approximate wavefunctions of the adiabatic approximation are characterized by the following off-diagonal matrix elements between different electronic states [11]: ðhYav jH jYav0 ir Þq ¼ Eav dvv0
ð1:11Þ
(i.e., the adiabatic basis set is diagonal within the same electronic configuration) and hYav jHjYbv0 ir q ¼ xav hja jTN jjb ir xbv0 q X h2 xav ja q=qqm jb r qxbv0 =qqm : ð1:12Þ m
q
In Equation 1.12, we have indicated convenient abbreviations for the two integrals: hj ji for the integral over electronic coordinates and ðj jÞ for the integral over nuclear coordinates. Equation 1.12 represents the so-called Born–Oppenheimer coupling, which promotes transitions between potential energy surfaces via the nuclear kinetic energy operator. If these terms in the basis defined by Equation 1.9 are small relative to the separation of vibronic states Eav Ebv0 , the BO approximation will give a very good approximation and will lead to tremendous simplification. In the case of close lying vibronic states belonging to different electronic configurations Eav Ebv0 , the adiabatic approximation can fail. The interaction of nuclear vibrations with the electronic motion in molecules gives rise to interesting effects that have been attributed to linear and quadratic terms in the nuclear displacements from the equilibrium configuration. Linear vibronic coupling terms lead to vibrational borrowing, an effect that appears most clearly with forbidden electronic transitions made allowed through the simultaneous excitation of certain asymmetric vibrations. The other physical situations associated with linear displacements along certain asymmetric normal coordinates lead to the Jahn–Teller [12–25] and the pseudo-Jahn–Teller effects (see Appendix K). The effect of quadratic nuclear displacement terms is manifested in the Renner effect [26]. Although the study of these effects is of considerable interest, their observation is limited to systems of high symmetry that have degenerate or nearly degenerate electronic states. Going back to expression (1.12) for the coupling term, we shall now elucidate the situation that occurs when the potential energy surfaces belonging to different electronic states cross. This is easily obtained on introducing the following expressions [27]: ½Eb ðqÞEa ðqÞ ja q=qqm jb ¼ ja qU=qqm jb ð1:13Þ and E D E D ½Eb ðqÞEb ðqÞ ja q2 =qq2m jb ¼ ja q2 U=qq2m jb þ 2 ja ðqU=qqm Þq=qqm jb : ð1:14Þ
In the region where the two potential energy surfaces do not cross, Ea ðqÞ 6¼ Eb ðqÞ; Equation 1.13 may obviously be rewritten as ja q=qqm jb ¼ ja qU=qqm jb =½Eb ðqÞEa ðqÞ ð1:15Þ
j5
j 1 Introduction
6
and relation (1.15) is well behaved. At the surface intersections Ea ðqÞ ¼ Eb ðqÞ, relation (1.15) is not as such without further ado valid. To see this, we differentiate the general expression (1.13) with respect to qm and then evaluate the result at the surface intersection to yield
ð1:16Þ ja q=qqm jb ¼ q ja qU=qqm jb =qqm = qEb =qqm qEa =qqm ; where we have assumed, for simplicity, that the intersection surface results from the variation of a single coordinate qm and that ðqEb =qqm Þc 6¼ ðqEa =qqm Þc at the intersection point c. This means that hja jq=qqm jjb i is well behaved over the whole range of values of qm . Indeed, Equation 1.16 can be rederived directly from Equation 1.15 by applying lHospitals rule. Expression (1.15) should likewise be well behaved (nonsingular) in the more general case of multidimensional surface intersections, where qm in Equation 1.16 denotes the coordinate normal to the intersection surface defined by Ea ðqÞ ¼ Eb ðqÞ. The property of hja jq2 =qq2m jjb i and its nonsingularity clearly follow in a completely analogous way. The behavior of hja jq=qqm jjb i and hja jq2 =qq2m jjb i has been examined in Ref. [28] for H2 þ as a function of the internuclear distance R. Both these quantities were shown to vary smoothly with R. Subsequently, Nitzan and Jortner [29] have used Equation 1.15 in the whole range of values of qm , including the region of the intersection of the adiabatic surfaces by assuming the principal value for ½Ea ðqÞEb ðqÞ1 at the intersection point. This leads to a finite but peaked value of (1.15) at the surface intersection. A representative example of a similar situation will be shown in Sections 1.6 and 7.6, where the nonadiabatic coupling (1.15) near the conical intersection between states 2 B2 and 2 A1 of H2 O þ is shown. 1.1.3 The Crude Born–Oppenheimer Basis Set
In this and the following sections, we will discuss ways of selecting the basis function ja by separating the nuclear and electronic motions in a manner different from that in the previous section. In the present approach, the electronic Hamiltonian is assumed to be Helec ¼ Te ðrÞ þ Uðr; q0 Þ þ DUðr; qÞ;
ð1:17Þ
where q0 is a reference configuration and DU ¼ Uðr; qÞUðr; q0 Þ is taken as a perturbation. In what follows, we will first briefly discuss the crude approximation and then the improvement of the crude BO basis set by using the Herzberg–Teller approximation. In addition to its practical utility, the Herzberg–Teller approximation provides an instructive way of viewing the (improved) crude BO basis complementary to that of the adiabatic basis derived in Section 1.1, permitting a reconciliation between the apparently contradictory features of both the crude BO basis set and the BO adiabatic basis set. The situation we have in mind occurs in the case of widely separated electronic states, which when mixed with each other give rise to vibronically induced allowed electronic transitions [30, 31] (see, for example, the mixing of odd parity states with the even parity states of transition metal complexes).
1.1 The Adiabatic Description of Molecules
In the crude adiabatic (CA) approximation [1, 32–40], the electronic wavefunctions odinjCA a ðr; qÞ defined at a specific nuclear configuration q0 satisfy the following Schr€ ger equation: CA CA ½Te ðrÞ þ Uðr; q0 Þ jCA a ðr; q0 Þ ¼ Ea ja ðr; q0 Þ;
ð1:18Þ
where EaCA is the ath eigenvalue and q0 implies all the nuclear coordinate positions of the reference configuration. Since these wavefunctions form a complete set (which span the Longuet–Higgins space), the eigenstate of the total Hamiltonian Yv ðr; qÞ may be expanded (analogous to Equation 1.6) in terms of jCA a ðr; q0 Þ: X Yv ðr; qÞ ¼ jCA ð1:19Þ b ðr; q0 Þ xbv ðqÞ: b
As before, xbv ðqÞ are initially treated as expansion coefficients, which must be determined. Inserting Equation 1.19 in Equation 1.4 results in the usual infinite set of coupled equations for the xbv ðqÞ:
CA TN ðqÞ þ EaCA þ jCA a ðr; q0 Þ jDU j ja ðr; q0 Þ Et xav ðqÞ X ð1:20Þ CA jCA þ a ðr; q0 Þ jDU j jb ðr; q0 Þ xbv0 ðqÞ ¼ 0: b6¼a
The functions xav ðqÞ are therefore determined by the set of coupled equations (1.20). CA are usually represented as power series DU The potential functions jCA j jj a b expansions in the normal coordinates qm around q0 , where q0 is usually chosen at the minimum of the ground state. Provided that CA ¼0 ð1:21Þ ja jDU jjCA b for a 6¼ b, Equation 1.19 is simply written as a product CA CA YCA av ðr; qÞ ¼ ja ðr; q0 Þxav ðqÞ;
ð1:22Þ
where the coefficient xCA av is the eigenstate of the following equation: CA CA CA CA TN ðqÞ þ EaCA þ jCA xav ðqÞ: ð1:23Þ xav ðqÞ ¼ Eav a jDU jjb CA The diagonal matrix elements ja jDU jjCA are the effective potential energy a surface that governs nuclear motion. From Equations 1.10 and 1.23, it is evident BO that the vibrational wavefunction xCA av differs from the adiabatic wavefunction xav : As ðr; q Þ is complete in the electronic space, the CA basis is long as the basis set jCA 0 a perfectly adequate (independent of the choice of q0 ). The two matrix representations 1.8 and (1.20) are merely two different representations of the same operator. 1.1.4 Correction of the Crude Adiabatic Approximation
The electronic wavefunction in the crude adiabatic approximation is defined according to Equation 1.18 at a specific nuclear configuration q0 and therefore it does not
j7
j 1 Introduction
8
depend on the nuclear coordinates fqm g. To calculate corrections to this extreme case, we apply the Rayleigh–Schr€odinger (RS) perturbation calculation, taking DU as perturbation operator. This leads to X ja ðr; qÞ ¼ jCA jCA ð1:24aÞ a ðrÞ þ b ðrÞcba ðqÞ; b6¼a
where CA CA CA X jCA ðrÞjDU jjCA jb ðrÞjDU jjCA a ðrÞ c ðrÞ jc ðrÞjDU jja ðrÞ b þ EaCA EbCA EaCA EbCA EaCA EcCA c6¼a;b
cba ðqÞ ¼
ð1:25Þ
and CA Ea;b ¼ Ea;b ðq0 Þ:
The same procedure gives for the eigenvalues (in second order) Ea ðqÞ ¼ EaCA þ ðDUÞaa þ
X ðDUÞ ðDUÞ ab ba ; CA E CA E a b b6¼a
ð1:26Þ
where CA ðDUÞab ¼ jCA a ðrÞjDU jjb ðrÞ :
ð1:27Þ
Expansion of DU in the vicinity of q0 in terms of nuclear coordinates fqm g gives DU ¼
X qUðqÞ m
qqm
qm þ
q0
1 X q2 UðqÞ q m qn þ : 2 m;n qqm qqn q
ð1:28Þ
0
After inserting (1.28) into (1.26), we have Ea ðqÞ ¼
EaCA
þ
X m
Umaa qm
( ) X Umab Unba 1X aa þ qm qn Um;n þ 2 2 m;n E CA EbCA b6¼a a
ð1:29Þ
with * Umab
¼
+ qUðr; qÞ CA jb ðrÞ qqm q
jCA a ðrÞ
ð1:30Þ
0
and quadratic terms in qm : ab Umn ¼
2 q Uðr; qÞ CA j ðrÞ : jCA ðrÞ a qq qq b m n
ð1:31Þ
In writing Equation 1.29, we have taken into account the linear terms from Equation 1.28 in second order and quadratic terms in q in first order. Correspondingly, the coefficients cba ðqÞ in (1.25) are expressed as (in second order)
1.2 Normal Coordinates and Duschinsky Effect
j9
" # ba X Umba X 1 Umn X Umbc Unca qm qn : cba ðqÞ ¼ q þ þ CA m CA 2 EaCA EbCA c6¼a EaCA EbCA EaCA EcCA m Ea Eb m;n ð1:32Þ
The correction of the CA approximation performed above is known as vibronic coupling and the wavefunction (1.24a) is sometimes designated as the Herzberg– Teller approximation. In this approximation, the corrected molecular eigenfunction can be written as " # X CA CA Yav ðr;qÞ ¼ ja ðrÞþ jb ðrÞcba ðqÞ xBO ð1:33Þ av ðqÞ b6¼a
and is still (of product form) adiabatic. Ballhausen and Hansen [1] have introduced the term Herzberg–Teller adiabatic approximation to emphasize the adiabatic nature of Equation 1.33 [40]. An obvious generalization of Equation 1.24a results if we choose X ja ðr; qÞ ¼ jCA cba ðqÞ ð1:24bÞ b ðrÞ b
for an adiabatic electronic wavefunction ja ðr; qÞ. Upon substituting Equation 1.24b into Equation 1.6, we obtain X X ccb ðqÞxBO Yv ðr; qÞ ¼ jCA ð1:34Þ c ðrÞ bv ðqÞ; c
b
which can be compared with Equation 1.19 to yield the relation X c cb ðqÞxBO xCA cv ðqÞ ¼ bv ðqÞ
ð1:35Þ
b
between the vibrational wavefunction in the CA approximation and the vibrational wavefunction in the BO approximation. The classic cases of the Herzberg–Teller mechanism relate to coupling between two electronic states of different symmetry. An important example of this case occurs when electric dipole transitions of one of the two states are forbidden (e.g., the Laporte-forbidden d–d and f–f transitions). In this case, the forbidden transition may acquire absorption intensity by Herzberg–Teller mixing with an allowed transition via a nontotally symmetric mode of appropriate symmetry (the irreducible representation of the active mode must be contained in the direct product of the irreducible representations for the two states coupled by the Herzberg–Teller mechanism). We shall illustrate our results in Chapter 7 by evaluating the vibronic induced d–d transitions in transition metal complexes.
1.2 Normal Coordinates and Duschinsky Effect
Let us now return to Equation 1.29 for the potential energy surface of the ath electronic state and reformulate it in a more suitable (canonical) form:
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Ea ðqÞ ¼ Ea ðq0 Þ þ
X m
lam qm þ
1X a 1 fmn qm qn ¼ Ea0 þ ðIa Þt q þ qt Fa q; 2 m;n 2
ð1:36Þ
with lam ¼ Umaa
and a aa fmn ¼ Umn þ2
X Umab Unba b6¼a
EaCA EbCA
:
ð1:37Þ
In Equation 1.36, the boldface letters q and F are column vector and square matrix, respectively. The superscript t indicates matrix transposition. Apart from the linear terms in qm , the potential of the ath electronic state contains in the harmonic approximation pure and mixed quadratic terms. The linear terms lm 6¼ 0, especially for total symmetric vibrational modes m (see Equations 1.30 and 1.37) is closely related to the geometrical displacement associated with the electronic transition between the electronic ground state and the ath electronic state. The pure quadratic a force constant coefficients fmm describe the curvature of the potential energy surface of the ath electronic state along the axes of the nuclear coordinate system, whereas the mixed quadratic terms fmna ðm 6¼ nÞ are responsible for the mixing of vibrational coordinates (modes) upon electronic excitation (see later). Therefore, our first goal is to transform them from the expression of Ea ðqÞ. Since Fa is a real and symmetric square matrix, it can be diagonalized by the following transformation: qa ¼ Aa q þ ka ;
ð1:38Þ
where Aa is an orthogonal matrix that diagonalizes the mass-weighted force constant matrix F. Applying Equation 1.38 on the electronic ground state a ¼ 0 and noting that ðABÞt ¼ Bt At for any two matrices, we have E0 ðqÞ ¼E0 ðq0 Þ þ ðl0 Þt ðA0 Þ1 q0 ðl0 Þt ðA0 Þ1 k0 1 0 1 0 0 t 0 0 1 0 0 ½ðA Þ ðq k Þ F ½ðA Þ ðq k Þ 2 1 1 ¼E0 ðq0 Þ þ ðl0 Þt ðA0 Þ1 q0 þ ðq0 Þt A0 F0 ðA0 Þ1 q0 ðq0 Þt A0 F0 ðA0 Þ1 k0 2 2 1 0 t 0 0 0 1 0 0 t 0 1 0 1 0 t 0 0 0 1 0 ðk Þ A F ðA Þ q ðl Þ ðA Þ k þ ðk Þ A F ðA Þ k 2 2 1 ¼ E0 ðq0 Þ þ ððl0 Þt ðA0 Þ1 ðk0 Þt A0 F0 ðA0 Þ1 Þq0 þ ðq0 Þt A0 F0 ðA0 Þ1 q0 2 1 ðl0 Þt ðA0 Þ1 k0 þ ðk0 Þt A0 F0 ðA0 Þ1 k0 : ð1:39Þ 2 þ
In deriving (1.39), we have made use of the relation A1 ¼ At for A being orthogonal. (The inverse of the matrix is its transpose At A ¼ E.) The linear term in q in
1.2 Normal Coordinates and Duschinsky Effect
Equation 1.39 vanishes, if ðl0 Þt ðA0 Þ1 ðk0 Þt A0 F0 ðA0 Þ1 ¼ 0
and hence ðl0 Þt ðA0 Þ1 k0 ¼ ðk0 Þt A0 F0 ðA0 Þ1 k0 :
ð1:40Þ
Inserting (1.40) into (1.39) yields E0 ðqÞ ¼ E0 ðq0 Þ þ
1 0 t 0 0 1 0 t 0 0 ðq Þ L q ðk Þ L k ; 2 2
ð1:41Þ
where L0 ¼ A0 F0 ðA0 Þ1 ¼ diag ðl01 ; l02 ; . . . ; l0N Þ is composed of diagonal elements lm , which arises from the nonzero frequency normal modes. Thus, Equation 1.41 represents the potential surface of the ground electronic state in the diagonal (canonical) form in mass-weighted ground-state normal coordinates. The last term in Equation 1.41 is a constant and can be included in E0 ðq0 Þ. Thus, the transformation (1.38) that diagonalizes the potential energy for the nuclear motion is determined uniquely by the coefficients l0m and fmn0 of the respective electronic state. Equation 1.41 pertains to the normal coordinates in the ground electronic state; an analogous expression holds for any electronic state a, where again La ¼ Aa Fa ðAa Þ1 ¼ diag ðla1 ; la2 ; . . . ; laN Þ and Aa is the transformation matrix to mass-weighted coordinates, defined by qa ¼ Aa q þ ka :
ð1:42Þ
It can be proved that Ea ¼ Ea0 þ
1 a t a a ðq Þ L q : 2
ð1:43Þ
Combining (1.42) for a 6¼ 0 and (1.38) leads to qa ¼ Aa ðA0 Þ1 q0 þ ka Aa ðA0 Þ1 k0 ;
which we abbreviate to qa ¼ Wq0 þ k0a ;
ð1:44Þ
where W ¼ Aa ðA0 Þ1 thus formed is known as the Duschinsky rotation matrix associated with the 0 ! a electronic transition and k0a is related to the geometrical displacement vector between these states. (To simplify notation, we shall henceforth drop the 0a superscript on k.) According to Equation 1.44, the normal coordinates of an excited electronic state qa relative to those of the ground electronic state q0 are rotated (rotation matrix W) and displaced by the vector k. This rotation is called the Duschinsky rotation or Duschinsky mixing effect [41–44] (of the vibrational modes among each other). This mixing effect is subject to symmetry rules of the molecular symmetry group. Since in the most common instances vibrational modes of the same symmetry are mixed with each other (Equations 1.29–1.31 and 1.37), the matrix W assumes the
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quasi-diagonal form indicated below: ===== ==== 0 ; W ¼ 0 === == where the elements outside the shaded area are zero, since they correspond to modes aa 6¼ 0 if qm qn of different symmetry. Simple symmetry arguments show that Umn ab ba transform as the totally symmetric transformation and Um Un 6¼ 0 if qm qn transform as the direct product of ja and jb . Rotations of normal coordinates in an excited electronic state relative to the ground-state normal coordinate space can therefore be expected for such a molecule if it possesses at least two different modes transforming as the same irreducible representation [41]. Cross-terms, and hence rotations in aa term in Equation 1.29, whereas totally symmetric modes, are generated by the Umn rotations in the nontotally symmetric modes are generated by the terms in the summation over b 6¼ a. As we shall see, this feature plays a crucial role in the derivation of transition probabilities. Vibrational modes of the same symmetry species assigned to the same shading fields in the matrix W cannot be represented as single separable modes and are said to be mixed or nonseparable modes. A very thorough survey of the Duschinsky effect is given in Refs [45–57]. A 8 8 Duschinsky matrix W has been determined by quantum mechanical calculation of the potential energy surfaces to interpret the vibronic structure of the 1 Bu 1 Ag transition of trans,trans-1,3,5,7-octatetraene in alkane matrices at 4.2 K [45]. The mixed modes are of a1g symmetry. Supersonic jet excitation and single vibronic level dispersed fluorescence spectra of a- and b-methyl naphthalene (S1 state) presented in Ref. [46] reveal that mode mixing of the ground-state normal coordinates and energy redistribution appear to be active in the S1 state. The vibronic spectra and related phenomena such as fluorescence–absorption mirror symmetry breakdown are found in azulene and certain azaazulenes [47–49]. On the basis of an analysis of vibronic spectra and calculation of normal vibrations, a complete assignment of the vibrational frequencies of s-tetrazine-d0 and s-tetrazine-d8 in the 1B3u excited state is given in Ref. [50]. In this connection, the rotation matrix W calculated from the data on the intensities of the vibronic band is used to estimate the force field in the excited electronic state. In Ref. [51], a Duschinsky effect that results from two nontotally symmetric vibrations involved in the vibronic coupling in the S1 --S0 systems of benzonitrile and phenyl acetylene is reported. An ab initio calculation of multidimensional FC (MFC) factors used to analyze the vibronic spectrum of ethylene corresponding to the p–p excitation was presented in Ref. [52] taking into account 12 normal coordinates of ethylene among which 4 totally symmetric modes are mixed. ~ 2 B2 Þ and D2 O þ , Jia-Lin Recently, in a study of the photoelectron spectra of H2 O þ ðB Chang has calculated MFC integrals including the Duschinsky effect. He found that the photoelectron spectra were mainly composed of v2 progressions and combination bands of v1 and v2 vibrations [53]. The idea that the Duschinsky effect plays a crucial role in the identification of band structures is also confirmed by the vibrational ~ 1 B2 --X ~ 1 A1 transition in tropolone. This molecule possesses an assignment for the A
1.3 The Vibrational Wavefunctions
intramolecular hydrogen bond and the hydroxyl proton tunnels from one oxygen atom to the other. Spectroscopic studies indicate that tropolone exhibits a double minimum energy potential along the tunneling coordinate and tunneling doublings have been detected in many vibronic bands in the absorption and laser excitation spectra [54–56]. However, the band structure is exceedingly complex and some of the complexity in the vibrational bands around the 0–0 band is due to strong Duschinsky mixing involving the two lowest b1 modes v25 and v26 . The importance of determining the potential energy surfaces of molecular states is clear. The shape of these BO surfaces of the molecular states is intimately involved in the electronic transitions between vibronic states belonging to crossing BO surfaces. This was applied by Paluso et al. to the dynamics of electronic transfer in neutral mixed valence monoradicals, using the diabatic representation (as will be illustrated in Section 1.4) and by considering a significant Duschinsky effect [57]. Generally, a significant Duschinsky effect might be expected when the change in equilibrium geometry upon excitation has components of large and comparable magnitude along two or more totally symmetric (ground-state) coordinates. This point will be clarified in detail in Chapter 3 and also in our subsequent consideration, where the Duschinsky effect will play an important role.
1.3 The Vibrational Wavefunctions
The introduction of mass-weighted normal coordinates fqm g obtained by diagonalizing the mass-weighted force constant matrix F in the respective electronic states allows us to solve Equation 1.10 for the vibrational wavefunctions in these states in a very convenient manner. Indeed, writing the kinetic operator (1.3) in mass-weighted coordinates qm and taking the diagonalized form (1.43) of the potential energy surface Ea ðqa Þ, Equation 1.10 is written as " # h2 X q2 1 X a a2 þ l q x ðqa Þ ¼ Eav xav ðqa Þ; a2 2 m m m av 2 m qqm
ð1:45Þ
where the superscript a denotes the respective electronic state to which xav is assigned. In our formulation of Equation 1.45, we have made use of the fact that the kinetic energy operator remains invariant under the transformation (1.44). The Hamiltonian of the nuclear motion in Equation 1.45 separates now into parts, each of which is represented by an individual harmonic oscillator Hm with 2 2 h q 1 2 Hm ¼ þ lam qam : 2 qqam2 2
ð1:46Þ
For local stable molecules, lam > 0 (m ¼ 1; 2; . . . ; N), and we can set lam ¼ va2 m , where vam is the vibrational frequency of the mth oscillator. The eigenfunctions and eigenvalues of (1.46) are known and given by
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1=2 1=2 Hm xanm bam qam ¼ Eanm xanm bam qam ;
ð1:47Þ
Eanm ¼ hvam ðnm þ 1=2Þ;
ð1:48Þ
where nm ¼ 0; 1; 2; . . .
and xanm
1=2 bam qam
bam pffiffiffi nm p2 nm ! 1=2
¼
!1=2
1=2 1 2 exp bam qam Hnm bam qam : 2
ð1:49Þ
Here Hnm is the Hermite polynomial of the degree nm : Hn ðxÞ ¼
X ð1Þk n! ð2xÞn2k k!ðn2kÞ! k¼0
and bam ¼ ðvam =hÞ. The qam s are dimensioned mass-weighted normal coordinates and the transformation to dimensionless normal coordinates is accomplished by the corresponding frequency factors of the vibrational modes m in the electronic state 1=2 a, ba ¼ ðvam =hÞ1=2 . The eigenfunction and eigenvalue of the total Hamiltonian P m m Hm are 1=2 1=2 1=2 xan1 n2 ...nN ðqa1 ; qa2 ; . . . ; qaN Þ ¼ xan1 bam qa1 xan2 bam qa2 xanN bam qaN
and Ean1 n2 ...nN ¼ Ean1 þ Ean2 þ þ EanN ;
ð1:50Þ
where the vibrational quantum numbers n1 ; n2 ; . . . ; nN assume in mutual independence of one another the values nm ¼ 0; 1; 2; . . ..
1.4 The Diabatic Electronic Basis for Molecular Systems 1.4.1 Preliminaries
The Born–Oppenheimer adiabatic approximation derived in Section 1.1 is very useful in classifying molecular eigenstates and calculating molecular dynamics. As long as adiabatic potential energy surfaces remain well separated, it is generally a good approximation to consider the nuclear motion to be confined to one such surface. When two or more surfaces intersect or pass close to one another, it becomes necessary to consider more than one surface in the calculation of nonradiative transition probabilities. When more than one surface must be considered, the adiabatic function is not necessarily more advantageous than various possible linear combinations of these functions. In particular, if the combination is taken over a small number of electronic states presumed to be of interest for a particular problem,
1.4 The Diabatic Electronic Basis for Molecular Systems
they can be chosen by means of a proper transformation such that the nuclear derivative coupling terms (e.g., in Equation 1.12) vanish with respect to the new basis functions. The coupling for the new so-called diabatic basis occurs then as a potential operator. Consider an example in which only two adiabatic states (say j1 and j2 ) are strongly coupled and assume that the coupling involving the other states can be safely neglected. In this case, the nuclear derivative coupling term in Equation 1.12 is given by the components gm ¼ j2 q=qqm j1 ð1:51Þ of a nuclear momentum vector gðqÞ ¼ ðrq Þ21. Here rq stands for the vectorial operator rq ¼ ðq=qq1 ; q=qq2 ; . . . ; q=qqN Þ. In this two-state approximation, it is convenient to consider as an alternative a diabatic basis set ðw1 ; w2 Þ defined by the condition [58–65] ð1:52Þ w2 rq w1 ¼ 0: In the diabatic representation, the nuclear coupling is eliminated or drastically reduced. The new diabatic states ðw1 ; w2 Þ are thereby allowed to move along with the nuclei [7, 65]. They are not the fixed functions considered in Section 1.2 and referred to as crude adiabatic. Hence, they will be denoted by wi ðr; qÞ to emphasize the fact that rwi 6¼ 0. In this two-state approximation, it is always possible to transform the pair of adiabatic functions ðj1 ; j2 Þ by a q-dependent orthogonal transformation [7, 63, 65]: ! ! ! w1 j1 cos qðqÞ sin qðqÞ ¼ : ð1:53Þ j2 w2 sin qðqÞ cos qðqÞ Substituting Equation 1.53 into Equation 1.52 now leads to gðqÞ ¼ rq qðqÞ þ w2 rq w2 :
ð1:54Þ
Note that Equation 1.54 is a vector equation. Thus, condition (1.52) implies that there should exist an angle q such that gðqÞ ¼ rq qðqÞ:
ð1:55Þ
As discussed in Ref. [63], this can only be the case if curl gðqÞ ¼ 0;
ð1:56Þ
which means that if qm and qn are two of the nuclear coordinates, we can have a solution only if q q gn gm ¼ 0: qqm qqn
ð1:57Þ
As proved in Ref. [63], this follows trivially for a polyatomic molecule if one adopts as diabatic functions a set of q-independent functions for which rwi ¼ 0. This can be seen if we use Equation 1.53 to prove another very useful result [66, 67]:
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X rw i ¼ ðgðqÞrqÞw i þ ½cos q hja jrj1 isin q hja jrj2 ijja i; 1 2
ð1:58Þ
a
which follows from the fact that ðrq Þ21 ¼ ðrq Þ12 . Here ja are adiabatic eigenfunctions of Hel other than j1 and j2 . This is a most remarkable fact. It asserts that there can be no solution if rw1 6¼ 0. Then, one must be either ðgrqÞ 6¼ 0 or hja jrjji i 6¼ 0 (i ¼ 1; 2), or both of them. In the first case, this is in striking contrast to the concept of a strictly diabatic basis (see Equation 1.55). In the second case, there is an interaction with the other (higher) electronic states. The possibility remains, however, that it might be possible to eliminate the largest part of the coupling through transformation, so that the remainder can be neglected and Equation 1.55 can be replaced by the less stringent condition:
w2 rq w1 0:
ð1:59Þ
A particularly nice discussion to this subject can be found in Refs [7, 60, 63, 68, 69]. Let us now return to Equation 1.55. The angle qðqÞ; which depends on N internal nuclear coordinates, can be obtained by a multidimensional integration of the coupling matrix element gm [62]. For example, in a two-dimensional configuration space ðqx ; qy Þ; one has ð qx ð qy qðqx ; qy Þ ¼ qðqx0 ; qy0 Þ þ gx ðx; qy0 Þdx þ gy ðqx0 ; yÞdy: ð1:60Þ qx0
qy0
In the case where g is an irrotational vector and q a single-valued function, the value of q should be independent of the integration path. We shall return in Chapter 7 to a more extensive discussion of applications of the approximation just described. Now we consider the coupling between two electronic states, the potential energy surfaces of which cross in one point. 1.4.2 Conical Intersection Between the States B~ 2B2/2A0 and A~ 2A1/2A0 of H2O þ
The method we have described for studying unimolecular decay of electronically excited molecules may be applied to a variety of problems. These include, for example, the study of properties of conical and Jahn–Teller intersections. Illustrative calculations are presented for the H2 O þ ion, whose dissociation mechanisms are controlled by a conical intersection between the states 2B2 and 2A1 ðC2v Þ, the potential energy surfaces of which have been calculated in Refs [70, 71]. A schematic view of these surfaces is given in Figure 1.1. The coordinates ðr; aÞ are defined as follows: coordinate r is the asymmetric stretch r ¼ R1 R2 , where R1 and R2 are the two OH bond lengths and a is the valence angle between R1 and R2 . When the two OH bond lengths are equal (r ¼ 0; C2v point group) and q ¼ 1=2ðR1 þ R2 Þ, the symmetric ~ and B ~ belong to the 2A and 2B stretching coordinate is equal to 1.15 A, the states A 1 2 representations. Their potential energy surfaces cross at ac ¼ 71:6 [70] and the energy at the conical intersection is equal to 74.4385 hartree. The minimum of the
1.4 The Diabatic Electronic Basis for Molecular Systems
~ 2 A1 potential surfaces of H2 O þ in the adiabatic ~ 2 B2 and A Figure 1.1 The actual form of the B representation. The upper adiabatic potential energy surface E2 consists of parts of the surfaces of the states 2 B2 and 2 A1 . (After Ref. [35].)
potential function of the state 2 B2 lies at an absolute energy of 75.4435 hartree and the 2 B2 state equilibrium conformation has an HOH bond angle of 55.7 . When the antisymmetric stretching coordinate r differs from zero, that is, when the two OH bond lengths are unequal, both electronic states then belong to the 2 A0 representation of the Cs point group and therefore the corresponding potential energy surfaces repel each other. As a result, a region of strong nonadiabatic interaction is centered around ~ the apex of the double cone. It is important to note that the two interacting states A ~ and B are well separated in energy from the remaining states. If it did, one is dealing here with a two-state conical intersection problem (with the second term in Equation 1.58 having been omitted). The ab initio calculations at the SCF level of the nonadiabatic coupling matrix element ga ¼ qq=qa for different cross sections r ¼ constant have shown [70] that ga has a Lorentzian shape with a unique maximum centered at the crossing between the two surfaces (e.g., at ac ¼ 71:6 ). Along the direction r, the function gr exhibits again a unique maximum and a Lorentzian shape, although the two contributions grMO and grCI sometimes add and sometimes subtract. The resulting gr ¼ grMO þ grCI is therefore found to be positive at values of a smaller than ac and negative for a larger than ac , where ac denotes the value of the valence angle at the apex of the cone. The closer the cross section lies to the apex of the cone, the narrower the g-function becomes. In the case, where the cross section passes through the apex of the cone, the linear model (which will be encountered later) predicts that the g-function should become a Dirac delta function with an area close to the theoretical value of p=2 [70, 73–76]. Adiabatic surfaces are defined as the eigenvalues of the electronic Hamiltonian (see Equation 1.5). In the diabatic representation defined above, the potential energy
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surfaces are defined by the diagonal elements H11 and H22 . They can cross freely and are coupled by an off-diagonal matrix element H12 . Adiabatic surfaces are related to diabatic matrix elements Hii by the equation
1 1 2 1=2 Ei ðqÞ ¼ ðH11 þ H22 Þ ðH11 H22 Þ2 þ 4H12 ; 2 2
i ¼ 1; 2:
ð1:61Þ
This expression is the equation of a double cone with expansion of the Hij functions around the apex and retention of first-order terms only. The linear approximation will be discussed later in this section. The unitary transformation (1.53) (of the Hamiltonian matrix in the diabatic basis ðw1 ; w2 ÞÞ leading to Ei ðqÞ is determined by the angle 1 q ¼ arctanf2H12 =ðH11 H22 Þg; 2
ð1:62Þ
which depends on three internal nuclear coordinates q ¼ qðq; r; aÞ. Furthermore, one has from (1.55) gm ¼ qq=qqm ; with gm ¼ j2 q=qqm j1 or equivalently (see Equation 1.60) ðr ða qðr; aÞ ¼ drgr ðr; aÞ þ da ga ðr0 ; aÞ r0
a0
ð1:63Þ
ð1:64Þ
if we restrict ourselves to an integration at fixed value of q (the symmetric stretching coordinate). In the case of H2 O þ ; q ¼ 1:15 A , that is, the value of q at the apex of the cone. The integration in Equation 1.64 of the ab initio calculated gm matrix elements can be performed numerically. Before giving a more quantitative discussion, we first note that Equation 1.64 defines generally a multivalued function (i.e., qðqÞ is of modulus p). This behavior of q is a result of the singularities of the functions ga and gr at a ¼ 71:6 and r ¼ 0 (the apex of the cone). This problem is better understood within the framework of the linear model of the conical intersection, which will be dealt with later. Once the angle q is known as a function of the internal coordinates, it is not difficult to obtain the diabatic energies H11 and H22 and the coupling matrix element H12 by inverting the orthogonal transformation (1.53). A schematic view of the diabatic surfaces H11 and H22 is given in Figure 1.2. 1.4.3 The Linear Model for Conical Intersection
The linear model of a conical intersection [58, 66, 77–79] is obtained by neglecting terms of order higher than one in the expansion of the matrix elements Hij around the apex of the cone ðr ¼ 0; ac ¼ 71:6 Þ: H11 H22 ¼ Fa ðaac Þ;
ð1:65Þ
1.4 The Diabatic Electronic Basis for Molecular Systems
~ states. The thin line marks the seam. ~ and A Figure 1.2 The diabatic representation of the B
H12 ¼ ð1=2Þ Fr r:
ð1:66Þ
Note that ac depends on the value of q ¼ 1=2ðR1 þ R2 Þ. The same applies to the quantities Fa and Fr . This leads to a particular simple model of conical intersections, the features of which are as follows. Equation 1.61 can be cast in the convenient form 1 qða; rÞ ¼ arctan ½Fr r=Fa ðaac Þ: 2
ð1:67Þ
The coupling matrix elements ga and gr along cross sections parallel to the symmetry lowering a and symmetry conserving r axes derived from Equation 1.63 have the form qq Fa =ð2Fr rÞ ga ðaÞ ¼ ¼ ð1:68Þ qa q;r 1 þ ðFa =Fr rÞ2 ðaac Þ2 and gr ðrÞ ¼
qq Fr =½2Fa ðaac Þ ¼ : qr q;a 1 þ ½Fr =Fa ðaac Þ2 r 2
The parameters Fa and Fr can be estimated directly from the shape of the adiabatic potential energy surfaces. Fa can be read directly on a cross section along the axis a at r ¼ 0. The result is Fa ¼ 4:5 103 hartree/deg, compared to the value of 4:2 103 hartree/deg obtained from Refs [71, 72]. Fr can be determined from the shape of the adiabatic curves along the axis r, via Equation 1.66 and DE ¼ 2H12 =sin q, where DE ¼ E2 E1 is the energy difference between the adiabatic curves. This leads to Fr ¼ 0:045 hartree/bohr [70], compared to a value of 0.054 hartree/bohr obtained from Refs [71, 72]. Hence, for any cross section obtained by varying only one nuclear degree of freedom a or r, the nonradiative coupling elements are Lorentzians, which is in accord with the ab initio prediction [70].
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j 1 Introduction
20
Equation 1.67 represents graphically in a coordinate system with the axes ða; rÞ a series of straight lines around the apex of the cone for the locus of constant q in conformity with the result of numerical integration of (1.64) [70]. In particular, the line of intersection between diabatic states corresponds to the locus H11 ¼ H22 or q ¼ p=4 þ kp=2. It thus follows that as q ! p=4, the intersection coincides precisely with axis r at a ¼ 71:6 . At a complete rotation around the apex of the cone, the angle q increases from 0 to p only. According to Equation 1.68, the closer the cross section lies to the apex of the cone, the sharper the Lorentzian. Therefore, Equation 1.68 correctly describes the nonradiative coupling matrix elements gm well in accordance with the numerical calculations of the g-function cited above.
j21
2 Formal Decay Theory of Coupled Unstable States
The special methods for solving the Schr€odinger equation for molecular systems, which were discussed in Chapter 1, are used in the study of the decay of metastable states. This includes such familiar examples as the decay by nonradiative transitions of excited molecular states. Prior to the principal discussion, a description of the time evolution of a single excited state of an isolated molecule based on the Greens function technique is given in Section 2.1. This leads to an expression for the rate constant of nonradiative transitions with a matrix element of the transition operator T. Following the basis of this treatment, Section 2.2 addresses the question of the proper choice of the basis set for calculating transition probabilities in greater detail than that presented in Chapter 1.
2.1 The Time Evolution of an Excited State
We begin by considering an isolated molecule that is initially in a given discrete electronic state ys .1) Let Es be the energy of this state. The state ys interacts with a dense manifold of vibronic states belonging to a lower lying electronic state ylv0 by the presence of a perturbation that induces a transition from the original state. The state ylv0 is assumed to be of the same spin multiplicity as the original state ys (internal conversion) or of different spin multiplicity (intersystem crossing). No other electronic states ybv or different vibronic components of the same electronic state are close to ys in the energy region under study. If, for example, the prepared single state ys is excited by an electromagnetic field, we assume that only ys carries oscillator strength from the ground state j0i, whereas the states fyln0 g are optically inactive (Figure 2.1). When the manifold fylv0 g is of triplet species and ys is a singlet, spin selection rules are sufficient to fulfill this condition. On the other hand, if the manifold fylv0 g is singlet and the energy gap between ys and the lowest vibronic level of fylv0 g is sufficiently large, then the Franck–Condon factor for excitation of 1) Strictly speaking, truly isolated systems are not known in physics. They are extremely useful idealization.
j 2 Formal Decay Theory of Coupled Unstable States
22
|b> Vbs Vsl
|s>
µ0s
{|l>}
µ0l = 0
0 Figure 2.1 A schematic representation of the molecular states and relevant couplings. The zero-order molecular levels h0j, jsi, jbi, and fjlig are BO states for intrastate dynamics. They correspond, respectively, to the ground state h0j, the optically accessible doorway state jsi,
and the background manifold fjlig. jbi is a higher lying excited state separated from the state jsi. Arrows indicate dipole coupling via the interaction with radiation field. Wave lines represent intramolecular coupling.
the states that are quasi-degenerate with ys are small, so that hykv jmjys i hykv jmjylv0 i, where m is the transition moment operator and ykv is the wavefunction of the ground state. In Section 6.4, we return to the general case for which the last inequality is relaxed. To make the discussion simple, we use Dirac notation and accordingly denote the state vector ys by jsi and the basis set ylv0 by fjlig, where jli stands for jlv0 i. We suppose that the state ys ¼ jsi of the unstable system described above to be represented by an approximate Hamiltonian H0 at time t ¼ 0: H0 jsi ¼ Es jsi:
ð2:1Þ
Our central problem is now the study of the dynamical behavior of the system, as determined by the exact Hamiltonian H ¼ H0 þ V;
ð2:2Þ
with V being the perturbation. The development of jsi in time has the explicit form2) yðtÞ ¼ expðiHtÞjsi;
ð2:3Þ
which may be formally integrated to yield ð 1 yðtÞ ¼ dEeiEt GðEÞys ð0Þ: 2pi c
ð2:4Þ
The function GðEÞ that appears inside the integrand is the Greens function GðEÞ ¼ ðEH þ ieÞ1 ;
e ! 0;
ð2:5Þ
2) In this chapter, we use a system of units in which h ¼ 1, except when the value of h is important for our discussion.
2.1 The Time Evolution of an Excited State
and the contour c runs from þ 1 to 1 above the real E-axis, since the eigenvalues of H are real or they lie below the real axis (see Appendix A). To find the probability that the system remains in the initial state jsi (or in other words, the evolution at time t of the state jsi), we write the amplitude ð 1 Iss ðtÞ ¼ dEeiEt hsjGðEÞjsi: ð2:6Þ 2pi c The probability that the system is in the state jsi at time t is then Ps ðtÞ ¼ jIss ðtÞj2 :
ð2:7Þ
To simplify the calculation of Iss ðtÞ, we make use of the Feshbach projection formalism [80, 81] by introducing the operators P and Q satisfying the relations P þ Q ¼ 1;
QP ¼ PQ ¼ 0;
P2 ¼ P:
ð2:8Þ
Introducing the operator P ¼ jsihsj;
ð2:9Þ
which projects any vector on the isolated state function jsi, then the states jli are selected out by Q. To specify the matrix element Gss ¼ hsjGðEÞjsi corresponding to the state jsi, we must know the projection of the Greens function PGP. The latter can be expressed (see Appendix A.1) in the form PGP ¼ ½EPH0 PPRP1 :
ð2:10Þ
The quantity R in Equation 2.10 is called the level shift operator or self-energy and is given by R ¼ V þ VQðEQHQÞ1 QV:
ð2:11Þ
To evaluate this operator, we rewrite Equation 2.10 in a modified form. To do this, we use an operator identity. Let A and B be two operators for which the respective reciprocals ðA þ BÞ1 and A1 are defined. Then, 1 1 1 ¼ 1þB : AþB A AþB On taking A ¼ EPH0 P and B ¼ PRP, we find PGP ¼ ðEPH0 PÞ1 þ ðEPH0 PÞ1 PRPðEPH0 PPRPÞ1 :
Thus, we may write Equation 2.10 as hsjPGPjsi ¼
1 ; EEs hsjRjsi
where RðEÞ ¼ V þ VQ½ðEQH0 QÞ1 þ ðEQH0 QÞ1 QVðEQHQÞ1 QV:
ð2:12Þ
j23
j 2 Formal Decay Theory of Coupled Unstable States
24
This equation permits us to expand it in powers of V. Then, RðEÞ ¼ V þ VQðEQH0 QÞ1 QV þ higher order terms in V
and the matrix element of PRP becomes X
hsjRðEÞjsi ¼
hsjV jli
l
1 hljV jsi þ : EEl
ð2:13Þ
Here use has been made of the relationships QH0 Q jli ¼ El jli and ðEQH0 QÞ1 jli ¼ ðEEl Þ1 jli. From Equation 2.13 it is clear that as E approaches some El , then one term in the sum on l will become very large. Using the identity 0 1 1 1 1 1 1 1 A ¼ lim @ þ þ EEl 2 e ! 0 EEl þ ie EEl ie EEl þ ie EEl ie ¼ PP
1 1 e 1 ip limþ ¼ PP ipdðEEl Þ; 2 EEl EEl e ! 0 p ðEEl Þ þ e2
ð2:14Þ
Equation 2.13 can be written as [81] hsjRðEÞjsi ¼ DðEÞiCðEÞ=2;
ð2:15Þ
where DðEÞ, the level shift, is given by Equation 2.13, replacing there the energy denominator 1=ðEEl Þ by its principal part PPð1=ðEEl ÞÞ and X CðEs Þ ¼ 2p jhsjV jlij2 dðEs El Þ þ l
¼ 2p
X
ð2:16Þ
jhsjTðEÞjlij2 dðEs El Þ;
l
where hsjTðEÞjli ¼ hsjV jli þ
X hsjV jcihc jV jli c
EEc
þ ;
ð2:17Þ
with jc i being the intermediate states belonging to the space spanned by Q. The last relation follows by observing that the inclusion of higher order terms in the probability amplitude is achieved by replacing V by the transition operator TðEÞ ¼ V þ VGV ¼ V þ TG0 V ¼ V þ VG0 T. The first term in Equation 2.16 is the well-known Fermi Golden width. Inserting Equation 2.15 into Equation 2.12 yields Gss ðEÞ ¼
1 1 ¼ s þ iCðEÞ=2 ; EEs DðEÞ þ iCðEÞ=2 EE
ð2:18Þ
s ¼ Es þ DðEÞ. where we have absorbed the level shift DðEÞ in the term E It follows from Equation 2.18 that the integrand in Equation 2.6 has poles, so we need a well-defined prescription to avoid these singularities and give a meaning to the
2.1 The Time Evolution of an Excited State
integral. Some aspects of these questions will be explored in somewhat greater detail in later chapters of this book, where in addition to manifold fjlig, the state jsi interacts with a radiation field. For this it is important to know the analytical properties of the level shift operator RðEÞ in the complex E-plane. For the case of a single isolated state with a projection operator defined by Equation 2.9, the analytical properties of RðEÞ have been presented by Goldberger and Watson [81]. Returning finally to Equation 2.16, we use d functions to ensure energy conservation. Evaluation of the trace (sum) in Equation 2.16 evidently requires some care since the individual terms diverge. This is purely a mathematical problem and the first indication of the subtlety of our limiting procedure; we get a contribution to the width CðEs Þ as e ! 0, when the energy El of the set ðlÞ overlaps Es . Before contemplating the passage to the limit e ! 0, we must discuss the nature of the singularity of (2.16) near the energy Es ¼ El to give a precise instruction as to how this singularity is to be dealt with. First of all, the reader will note that the d function used in Equation 2.16 was adopted as a bookkeeping expedient and has meaning only in terms of distributions. However, it is really illogical to interpret Equation 2.16 in terms of distributions, whereas the width CðEs Þ is finite and continuous. The idea of a transition rate becomes somewhat absurd. On the other hand, the introduction of d function is convenient but not essential. To gain some insight into radiationless processes, Chock et al. [82] show that Lorentz distributions with a width directly related to the spectroscopic linewidth (resulting from the radiative and nonradiative decay width) are much more suitable to use. We here adopt this latter procedure, interpreting the density of state function rl as a row of Lorentz functions instead of a row ofXsharp equal d function peaks at the allowed final energies E ¼ El , dðEEl Þ. This is most easily accomplished by the definition of generrl ðEÞ ¼ l alized functions, according to which the d function is defined as a regular sequence of good functions [83], such as was derived in Equation 2.14 in terms of Lorentzians. With this tacit understanding, which will play an important role later, we shall interpret the limit in Equation 2.14 and the sum in Equation 2.16. The d functions are used further only in abbreviation. The introduction of a width associated with each state of fyl g may be seen in somewhat greater detail as follows. The states yl in Figure 2.1 are isoenergetic with ys and vibrationally hot, so that they would spontaneously emit infrared radiation leading to a molecule with energy too low to cross back to ys . Resulting from the time limitation on the duration of our experiment, we can question whether irreversibility behavior prevails for the time limit tmax . Our physical intuition tells us that if a relaxation for time tmax can be found, then the phenomena may be considered irreversible. In this case, the energy levels of states fyl g become continuous during portion of time that our experiment is being performed. Since the system is considered for a finite time tmax , all energy levels, except the ground state of the system (molecule and radiation field), have a vibrational relaxation width in energy DEl, as required by the uncertainty principle [84]: tl DEl ¼ ðh=Cl ÞDEl h;
where Cl is directly related to the level width DEl .
j25
j 2 Formal Decay Theory of Coupled Unstable States
26
This is the case of an isolated molecule. Our discussion can readily be extended to include other dissipation channels due to collisions of the molecule with one another after some time (tcollis 104 s at 1 mm pressure) in the system (molecule and radiation) and interaction of the molecule with the wall of the vessel containing them, Hwall . Then the appropriate Hamiltonian is described by an effective Hamiltonian with a small non-Hermitian component. Thus, the energies are complex, E ¼ El iCl =2, with a negative imaginary part, Cl > 0, directly related to the spectroscopic linewidth. The lifetimes are then just tl ¼ h=Cl and the above equation has a clear physical sense. It is instructive to give each state an average lifetime due to the existence of these other dissipative channels. In practice this can be quite difficult to do and a more practical approach is to consider the quantity Cl as impirical parameter, to be measured directly by experiment (Chapter 7). 2.1.1 Some Remarks About the Decay of a Discrete Molecular Metastable State
The Greens function method described in the previous section is based on the observation that the time evolution of the initially prepared state jsi is given by the Fourier transformation of the diagonal matrix element hsjGjsi of the Greens operator for the system G ¼ ðEH þ ieÞ1 , and that the decay characteristic of this state is determined by the complex pole of this diagonal element: hsjGjsi ¼ ðEEs iCs =2Þ1 ;
ð2:19Þ
where Cs is the half width of energy distribution given by the Fermi Golden Rule: Cs ðEs Þ ¼ 2
X
jhsjTðEs Þjlij2
l
C ðEs El Þ2 þ C2
:
ð2:20Þ
According to our remarks about the d functions, we have here used Equation 2.16 to set 1 C ¼ dðEs El Þ p ðEs El Þ2 þ C2
consistent with the finite lifetime of the state or the finite duration of any real experiment. We are now in position to calculate the probability for the transition between states jsi and jli per unit time as a result of V acting during the infinite period 1 to 1: 2X C wnonrad ¼ ; ð2:21Þ jhsjTðEs Þjlij2 h l ðEs El Þ2 þ C2 where the matrix element of the transition operator TðEÞ contains terms to all order in perturbation theory [84], that is, hsjTðEs Þjli ¼ hsjV jli þ
X hsjV jcihc jV jli c6¼s
Es Ec0
þ
X hsjV jcihcjV jc0 ihc0 jV jli þ : ðEs Ec0 ÞðEs Ec00 Þ c;c 0 6¼s ð2:22Þ
2.2 The Choice of the Zero-Order Basis Set
Here the intermediate states fjc ig arising from the projector 1P ¼ 1jsihsj may include the final states fjlig. The energies Ec0 are the corresponding eigenvalues of H0 . Equation 2.21 together with Equation 2.22 has a very attractive look, but an exact evaluation of the expression (2.22) is not feasible. To provide a rather remarkable amount of physical insight into this matter, let as return to the results of Chapter 1, where we have solved the Schr€odinger equation for the molecular system by expanding the molecular wavefunction in terms of either the adiabatic or the crude adiabatic basis set.
2.2 The Choice of the Zero-Order Basis Set
In this section we will discuss the problem of the nature of intramolecular interstate coupling and criteria for the choice of a basis set and consider the aspect whether these basis sets mentioned above is appropriate for describing the electronic relaxation processes. We begin by considering a complete set of zero-order functions, where electronic and nuclear motions have been separated arbitrarily. The index a refers to electronic state, while the second index v labels the vibrational state. X Utilizing the completeness assumption janihanj ¼ 1 and the trivial relation a;v X X 0 0 0 0 H¼ j av i h va j H ja v i h v a j , we decompose the total Hamiltonian in the form a;v a0 ;v0 H ¼ H0 þ V;
where both H0 ¼
ð2:23Þ
X javihvajHjavihnaj
ð2:24Þ
a;v
and the perturbation XX V¼ javihvajHja0 v0 ihv0 a0 j
ð2:25Þ
a;v ¼ 6 a0 ;v0
are specified by the zero-order basis set. In the BO representation, javi ¼ jAa ðr; qÞxAav ðqÞ, where the electronic jAa and the nuclear xAav wavefunctions satisfy (Equations 1.5 and 1.10) the equations ½Te þ Uðr; qÞjAa ðr; qÞ ¼ Ea ðqÞjAa ðr; qÞ
and
TN þ Ea ðqÞ þ jAa jTN jjAa xAav ðqÞ ¼ Eav xAav ðqÞ;
ð2:26Þ
while (Equation 1.12) VA ¼
A A X X jA xA h2 xA ja jqU=qqjja0 q xA0 0 a av av E ðqÞE 0 ðqÞ qq a v a;v a0 ;v0
a
A A
A A
A A þ xav ja jTN jja0 xa0 v0 ja0 xa0 v0
a
ð2:27Þ
j27
j 2 Formal Decay Theory of Coupled Unstable States
28
is the so-called nonadiabatic operator. In the crude adiabatic representation, CA CA CA javi ¼ jCA a ðr; q0 Þxav ðqÞ, where the electronic ja and nuclear xav wavefunctions satisfy (Equations 1.18 and 1.23) CA ½Te þ Uðr; q0 ÞjCA a ðr; q0 Þ ¼ Ea ðq0 Þja ðr; q0 Þ
and CA CA CA CA TN þ Ea ðq0 Þ þ jCA xav ðqÞ; xav ðqÞ ¼ Eav a jDUðr; qÞjja
ð2:28Þ
where DU ¼ Uðr; qÞUðr; q0 Þ and q0 is a fixed nuclear configuration (presumably the equilibrium configuration of the electronic ground state). In this representation, the perturbation is V CA ¼
X X CA CA CA jCA xCA jCA xCA jTN þ DUðr; qÞjjCA j 0 x 0 0 : 0 x 0 0 a;v6¼ a0 ;v0
a
av
a
av
a
av
a
av
ð2:29Þ
Before we return to our problem, we must note that the nonradiative probability wnonrad (Equation 2.21) as a spectroscopic observable is independent of the zero-order basis set. Thus, we have to take into account all terms of the transition operator (2.22). In this case, both A and CA sets (untruncated and complete) are adequate. Since this condition is very difficult to fulfill, we decide to choose the basis set in such a way that the second term and the higher order terms in Equation 2.22 are small and negligible. More specifically, which choice of basis gives rise to the smallest higher order corrections and/or leads to the fastest convergence of (2.22)? This can be achieved if the off-diagonal coupling matrix elements in Equation 2.22 are small relative to the first near-resonance coupling term. Thus, since only the leading term in the series (2.22) is ordinarily used, Equation 2.21 reduces to the physically interesting quantity, namely, the (first order) transition probability per unit time. It is given by w¼
2X C jðhjs xsv jV jjl xlv0 iÞj2 : h v0 ðEsv Elv0 Þ2 þ C2
ð2:30Þ
This formula, first obtained by Dirac, has played such an important role in timedependent perturbation theory that Fermi called it the Golden Rule. The interstate coupling matrix element (Equation 2.27) was conventionally treated by the application of the Condon approximation, (a) replacing the denominator in Equation2.27 by the constant electronic energy gap and (b) assuming that the matrix element jAa jqU=qqjjAa0 is independent of the nuclear configuration. This is almost certainly incorrect and unnecessary. A much more thorough discussion of such matrix elements is given in Chapter 5. Another formulation of this subject was given by Nitzan and Jortner [85] in an approximate scheme, relaxing both assumption (a) and (b). The point of view of that formulation will be followed here. For
2.2 The Choice of the Zero-Order Basis Set
near-resonance coupling between states jsi and jli having energy in the neighborhood of Es , they obtained for the nonadiabatic element (2.27) D s s E jCA r; q0 ðqU=qqk Þq0 jCA r; q0
A A A A A
s l k
xAsv ðqÞxAlv0 ðqÞ ; js xsv V jl xlv0 ¼ g DEsl = hv ð2:31Þ
where DEslk is the effective electronic energy gap between states s and l modified by a promoting mode k (to be explained later) and v is an average vibrational frequency. The correction factor g in Equation 2.31 is a linear function of DEslk = hv and exhibits a weak dependence on the coupling strength. Thus, for near-resonance coupling, Equation 2.31 is practically independent of the energy gap. For off-resonance coupling (e.g., with state jbi having an energy far from Es ) in the weak coupling limit, g 1, so that D E CA jCA A A
A A A A A
s ðqU=qqk Þq0 jb xsv ðqÞxbv0 ðqÞ : js xsv V jb xbv0 ¼ ð2:32Þ ðDEsbk =hvÞ Thus, the off-resonance coupling matrix element in the A basis is small. In the CA basis, the coupling terms are of the same form for both near-resonance and off-resonance couplings: CA CA CA CA CA CA CA js xsv V jc xcv0 js jDU jjCA Fv;v0 ; c
c ¼ l; b;
ð2:33Þ
CA where Fv;v 0 is the Franck–Condon factor between the CA states. Comparing (2.31) with (2.33), we see that off-resonance matrix elements in the CA basis are relatively large. The ratio of the off-resonance coupling terms in the CA and A basis is of the order of magnitude DE=hv ffi 10. Before we conclude this section, let us summarize what we have learned from this discussion. The choice of the basis set, which describes the bound-level structure of molecules is merely a matter of convenience. Assuming that the zero-order basis set is formulated such that it minimizes off-resonance coupling terms and thus allows to describe electronic relaxation processes in a two electronic level system, (a) the adiabatic basis set is superior to the crude adiabatic basis. At the same time, if the effect of off-resonance interactions can be disregarded, then (b) only a single or a few doorway states (which carry oscillator strength from the ground state) are accessible by transition on light absorption (accessible criterion). On the other hand, the appreciable contamination of the zero-order states jsi and jli by other states jbi in the crude adiabatic basis set implies that it is meaningless to consider the decay of an initial crude adiabatic state. (c) Generally, the appropriate basis set has to be chosen to satisfy the so-called similarity criteria according to which the basis set of H0 should be close to that of H (the entire Hamiltonian). (d) Another important point concerns the vibrational wavefunctions. The adiabatic potential surface Ea ðqÞ required for the calculation of the vibrational wavefunction xAan ðqÞ is known from molecular calculations, whereas little information is available about the crude adiabatic potential
j29
j 2 Formal Decay Theory of Coupled Unstable States
30
CA and the vibrational wavefunctions xCA surface jCA a jDUðr; qÞjja an ðqÞ. This last point is very crucial in view of the fact that the vibrational overlap enters into the calculation of the interstate matrix elements and thus can influence the latter to an appreciable extent. This depends on the manner in which the potential energy surfaces of the electronic states under study differ in their linear and (all) quadratic interaction terms (as we shall see later). Finally, we note that only in the case in which all off-resonance states are included in the calculations of relaxation processes, the crude adiabatic basis set is perfectly adequate. These conclusions remove the considerable confusion and intense discussions in the literature at the turn of the seventies, concerning the nature of the interaction responsible for the intramolecular radiationless transitions and the choice of the proper zero-order vibronic wavefunctions [86–91].
j31
3 Description of Radiationless Processes in Statistical Large Molecules In this chapter, a general scheme for calculating nonradiative rates of polyatomic molecules embedded in an inert medium is developed. Here we are concerned with the case of fast vibrational relaxation limit within an electronically excited state. These descriptions explain the experimental phenomena observed in widely varying environments, such as high-pressure gases, liquid solution, and solid hosts. The transition probability is calculated by taking proper account of the effects of geometry and frequency distortions as well as Duschinsky mixing of modes involved in the transition. Finally, a discussion of the decay of initially selected vibronic levels in the large molecule statistic limit is presented.
3.1 Evaluation of the Radiationless Transition Probability
We now apply the formalism of Chapter 2 to calculate the nonradiative decay probability of statistical large molecules embedded in an inert medium. The basic ideas used to describe the transition probability follow logically from the following assumptions: 1)
two-manifold electronic system is considered consisting of a limited number of zero-order vibronic states ys1 ; ys2 ; . . . ; and so on belonging to one electronic state s and a dissipative manifold of levels yln belonging to a lower electronic state l of the same multiplicity (see Figure 2.1). It is assumed that the density of states in fylnm g is so large in the region of fysmm g that we can safely assume that the (large molecule) statistical limit ensures. If this condition is not satisfied, then the situation corresponds to the small molecule case or to the intermediate case situations, and more consideration is required (see Section 6.3). The
j 3 Description of Radiationless Processes in Statistical Large Molecules
32
zero-order Born–Oppenheimer (BO) wavefunctions are ysm ðr; qÞ ¼ js ðr; qs Þxsm ðqs Þ; yln ðr; ql Þ ¼ jl ðr; ql Þxln ðql Þ;
xsm ðqs Þ ¼ xln ðql Þ ¼
N Y m
N Y m
1=2 xsmm bsm qsm ;
1=2 xlnm blm qlm ;
ð3:1Þ
where the first index refers to the electronic state, while the second corresponds to the vibronic levels within a given electronic manifold a ¼ s; l. The variable r stands for the totality of electronic coordinates and qa ¼ fqam g labels the set of normal modes. The molecular vibrational wavefunctions are here represented in terms of products of 1=2 1=2 harmonic–oscillator wavefunctions xsmm ðbsm qsm Þ and xlnm ðblm qlm Þ for the individual vibrational modes m. The qam s are dimensioned mass-weighted normal coordinates and the transformation to dimensionless normal coordinates is accomplished by the frequency factor of the corresponding vibrational mode m in the electronic state a, bam ¼ ðvam =hÞ. 2) Interference effects between resonances are neglected. It is thus assumed that the spacing between consecutive resonances centered about the energies Esm of the zero-order states ysm considerably exceeds the widths of these resonances. 3) The inert medium is characterized (with some exception) by the following features [92]:
4)
a. It does not modify the energy levels (e.g., it produces negligible level shift). b. It does not provide promoting modes influencing the radiationless transitions. The promoting modes correspond only to intramolecular vibrations. c. The inert medium does not enhance the coupling between electronic states. d. The inert medium may contribute low-frequency vibrational modes that can only accept energy, that is, acts as aheat bath. The inert medium contributes to the widths of the levels lnm in the dense molecular manifold by vibrational relaxation (see chapter 4). Acting as a heat bath the inert medium enhances the population of higher vibronic states in the smm manifold. Only in special cases, which are referred to as Shpolskii matrices, the medium does not contribute to accepting modes for electronic relaxations. Direct evidence supporting this vibrational relaxation is obtained from the phonon broadening of single lines in optical spectra. However, in the statistical limit, these effects are of no importance as the intramolecular density of states is sufficiently large. Therefore, electronic relaxation processes of large molecules in inert host matrices hardly reveal any medium effects. In the case of small molecules, which are characterized by a small number of vibrational degrees of freedom, the situation is quite different and the low-frequency medium vibrations may act as accepting modes in the electronic relaxations. As a further assumption, we adopt the so-called fast vibrational relaxation limit, according to which the vibrational relaxations in the excited electronic states are more efficient than electronic relaxations. Provided that vibrational relaxation rates considerably exceed the nonradiative decay probability, thermal equilibri-
3.1 Evaluation of the Radiationless Transition Probability
um prevails and the nonradiative decay probability is expressed by a thermal weighted sum of transitions originating from individual vibrational states smm . The coupling operator in Equation 1.12 involves first and second derivatives of js and jl , qj=qqg and q2 j=qqg qqm . The former are generally larger than the latter, so only they are retained. In the event that the second derivative is also of importance, it can easily be treated analogously to the first one. Hence the form taken by Vsm;ln of (1.12) is Vsm;ln ¼ ðhysm jH0 BO jyln iÞ ¼ h2
X g
D E xsm js ðr; qs Þq=qqlg jl ðr; ql Þ qxln =qqlg : ð3:2Þ
As we have discussed in Section 2.2 and shall treat more precisely in Chapter 5, the coupling matrix element (3.2) for nonradiative transition between the Born–Oppenheimer adiabatic states can be calculated at a configuration q0 , the so-called qcentroid. This permits Equation 3.2 to be rewritten in the form g
Vsm;ln ¼ h2
E X D js iq=qqlg jl xsm iq=qqlg xln ; g
q0
ð3:3Þ
where the electronic matrix element is evaluated at q0 . These matrix elements will be nonvanishing only for vibrations qg that corresponds to the same representation of the molecular point group belonging to the direct product js xjl . Such modes are designated as promoting modes. The remaining modes of a totality of N modes, which belong to the same molecular point group, are accepting modes. The specification of what constitutes an accepting mode will be given later. The thermal average nonradiative decay probability from the manifold fysm g to the manifold fyln g in the two-level approximation is given by the Golden Rule expression hwiT ¼
2 2X C pðm; TÞ Vsm;ln ; m;n h ðDE þ Esm Eln Þ2 þ C2
ð3:4Þ
where DE ¼ Es0 El0 is the energy gap between the lowest vibronic levels of the two s and l electronic states and Esm ¼
X m
mm hvsm
ð3:5Þ
nm hvlm
ð3:6Þ
and Eln ¼
X m
are the energies of the vibronic levels in each electronic manifold measured from the zeroth level of that manifold. When the temperature is not zero, it is necessary to
j33
j 3 Description of Radiationless Processes in Statistical Large Molecules
34
properly weight the sum over the states m ¼ fmm g. According to the basic principles of statistical mechanics, if a system (molecule) is in thermal equilibrium at temperature T, then its properties should be calculated by averaging over all states ysm , assigning to each state a weight pðm; TÞ proportional to expðEsm =kB TÞ: expðEsm =kB TÞ pðm; TÞ ¼ P : m expðEsm =kB TÞ
ð3:7Þ
The sum indexed by m in the denominator of Equation 3.7 shall always be understood to run over all vibrational levels of the s electronic state. pðm; TÞ is nothing more than the probability that the molecule will initially be in the zero-order state ysm . The geometric series in the denominator is easily summed to give Y 1 ðsÞ Z 1 ¼ Zm1 ; Zm ¼ 1exp hvm =kB T ; ð3:8Þ m
Q where kB is the Boltzmann constant. The product Z1 ¼ m Zm1 is known as the partition function. The double sum in Equation 3.4 weighted with the Lorentz distribution represents a density of states function over the manifold of initial and final states. The energies El0 þ Eln do not differ from the initial energies Es0 þ Esm by more than C. Hence, the transitions approximately conserve the energy, the spread in energy being given by C. This is the difference to dðDE þ Esm Eln Þ. The latter strictly vanishes when Es0 þ Esm 6¼ El0 þ Eln , so that it disappears for transitions between different states. For calculation of this weighted sum of density of states, we utilize the generating function (GF) approach derived for different potential parameters in a fully harmonic approximation. The latter involves the effects of frequency distortion and surface displacement, as well as the normal coordinate rotation on the two electronic states under consideration. The latter will be induced (as we have shown in Section 1.4) by a matrix (to be called W) that leads to mixing of normal coordinates belonging to these (different) electronic states. We begin by making use of the following Fourier transformation: 2C 2
ðDE þ Esm Eln Þ þ C
2
¼ h
1
1 ð
dt exp ith1 ðDE þ Eln Esm ÞC h1 jtj
1 1 ð
Y
¼ h 1 dt exp iVtC h1 jtj exp it nm vlm mm vsm ; 1
m
ð3:9Þ
where hV ¼ DE ¼ Es0 El0 is the energy gap between both s and l electronic states. Upon substituting Equations 3.7 and 3.9 into Equation 3.4, we obtain 1 ð X 1 1 hwiT ¼ 2 Z dt exp it VCh1 jtj Vsmm ;lnm exp itnm vlm Vlnm ;smm h mm ;nm 1 s
s exp mm itvm þ hvm =kB T :
3.1 Evaluation of the Radiationless Transition Probability
j35
If the explicit form for the matrix element (3.3) with the states (3.1) is used, then we are left with ( 1 ð
1 1 X g 2 hwiT ¼ 2 Z Rsl dt exp itVC h1 jtj Kg ðtÞGN1 ðtÞ h g 1 ð3:10Þ ) 1 X g g0 ð
1 þ Rsl Rsl dt exp itVCh jtj Ig ðtÞIg0 ðtÞGN2 ðtÞ ; g;g0
where
1
Rgsl ¼ ih js q=qqg jl q0 ; Y m Y m G1 ðtÞ; GN2 ðtÞ ¼ G1 ðtÞ; GN1 ðtÞ ¼ m6¼g;g0
m6¼g
with m
G1 ðtÞ ¼
X
ð3:11Þ ð3:12Þ
exp mm itvsm þ hvsm =kB T exp itnm vlm
mm ;nm 1 ð ð 1
1=2 1=2 1=2 1=2 dqlm dqlm xsmm bsm qsm xlnm blm qlm Þxsmm bsm qsm xlnm blm qlm :
1 1
ð3:13Þ
Here the square of the vibrational matrix element is written as a double integral in respect to qm and qm , the latter of which represents the same nuclear coordinate. The Kg ðtÞ corresponds to the single-mode generating function that involves the nuclear momentum operator for the promoting mode qg : X
Kg ðtÞ ¼ exp mg itvsg þ hvsg =kB T exp itng vlg mg;ng
1 ð 1 ð
h 2 1 1
1=2 q 1=2 1=2 q 1=2 dqlg dqlg xsmg bsg qsg i l xlng blg qlg xlng blg qlg i s xsmg bsg qsg : qqg qqg ð3:14Þ
Finally, analogous to (3.14), the mixed-type single-mode generating function Ig ðtÞ appearing in Equation 3.10 is given by X
Ig ðtÞ ¼ exp mg itvsg þ hvsg =kB T exp itng vlg mg ;ng
1 ð ð 1
h 1 1
1=2 q 1=2 1=2 s l1=2 l dqlg dqlg xsmg bsg qsg i l xlng blg qlg xsmg bs1 g qg xlng bg qg : qqg ð3:15Þ
Ig0 ðtÞ is defined in the same manner as Ig ðtÞ except with qxlng =qqlg replaced by xlng and xsmg replaced by qxsmg =qqsg. We note at this point that Equation 3.10 contains a direct contribution from each promoting mode g and an interference term between pairs of promoting modes g and g0 . Analysis of optical spectra of aromatic hydrocarbons [87, 93] and of transition
j 3 Description of Radiationless Processes in Statistical Large Molecules
36
metal ions [94–105] have shown that molecular normal modes include a small number p (p N) of promoting modes g and a large number of accepting modes m. According to the definition given above, the classification is based on the magnitude of the g electronic factor Rsl, Equation 3.14, the distortion of the excited electronic state relative to the lower (ground) electronic state Dm , and in smaller measure on the frequency factor bm ¼ bsm =blm ¼ vsm =vlm. For the promoting modes g, g
Rsl 6¼ 0;
Dg ¼ 0;
bg 1 ðor strictly bg ¼ 1Þ
(writing Dg as the dimensionless nuclear displacement Dqg associated with the s ! l transition, see below). Modes m characterized by m
Rsl ¼ 0;
Dm 6¼ 0;
bm 6¼ 1;
are called accepting modes. If bg 6¼ 1, the promoting mode can simultaneously act as an accepting mode. In aromatic hydrocarbons, the displacement Dm 6¼ 0 for totally symmetric carbon–hydrogen stretching modes and skeletal C–C symmetric stretching modes [93]. In transition metal complexes having an octahedral or nearly octahedral skeleton, accepting modeswith Dm 6¼ 0 arerepresented by the even parity modes, presumably the totalsymmetricstretchingmodes [94, 99, 103]. It is shown below that Ig ðtÞ andtherefore the second term in Equation 3.10 vanishes if the promoting modes are nontotally symmetric or if there is only one promoting mode as in this case Dg ¼ 0. Hence, Ig ðtÞ ¼ 0
and the transition probability of Equation 3.10 becomes 9 8 1 ð =
1 1 <X g 2 hwiT ¼ 2 Z Rsl dt exp itVC h1 jtj Kg ðtÞGN1 ðtÞ ; ; : g h
ð3:16Þ
1
m
where N is the totality of vibrational modes. For some of them, Rsl ¼ 0, Dm ¼ 0, and bm 1 and their contribution to Equation 3.16 will be unity. Such modes are completely inactive and will not affect the nonradiative decay probability. 1 Aswasobservedearlier,theoccurrenceofexpðC jtjÞ in(3.10)impliesthedamping h 1 of the integrand in the Fourier integral. (The exp C h jtj factor makes the integrand good atinfinity.)Ontheotherhand, byassigningthevibrationalrelaxationwidths dueto smm and lnm , the damping the coupling with the mediumto the zero-order states factor exp C h1 jtj ensures irreversible decay.
3.2 The Generating Function for Intramolecular Distributions I1 and I2 3.2.1 The Generating Function G2(w1,w2,z1,z2)
Before we analyze in more detail the expression for the transition probability (3.16), let us consider the generating function of Equation 3.12 for the case N1 ¼ 2,
3.2 The Generating Function for Intramolecular Distributions I1 and I2
j37
that is, for two accepting modes. To put Equation 3.12 into a more useful form, we write wm ¼ expðivsm thvsm =kB TÞ; zm ¼ exp itvlm ; ð3:17Þ and X 1=2 1=2 m rs qsm ; qsm ; wm ¼ xsmm bsm qsm xsmm bsm qsm wm m mm
0 11=2
bsm 1=2 2 2 1 i 1 h m þ qsm qsm w m ; ¼@ A exp bsm qsm þ qsm w 1wm2 4 p ð3:18aÞ
where m ¼ w
1wm ; 1 þ wm
1 w m ¼
1 þ wm ; 1wm
ð3:19aÞ
have been set. Analogously, X 1=2 1=2 n rl qlm ; qlm ; zm ¼ xlnm blm qlm xlnm blm qlm zmm nm
0 11=2
blm 1=2 2 2 i 1 h 1z2m ¼ @ A exp blm qlm þ qlm zm þ qlm qlm z1 ; m 4 p ð3:18bÞ
with zm given by zm ¼
1zm : 1 þ zm
ð3:19bÞ
The calculation of the sum in (3.18) is performed in close analogy to the Slater sum (Mehler formula) [106]. Using Equations 3.17 and 3.18, Equation 3.12 can be recast for N1 ¼ 2 as ! 1 D12 D212 b1 b2 G2 w1 ; w2 ; z1 ; z2 12 ; ¼ b12 b21 D1 D12 2 s s l l 1=2 ðð 1 ð ð 2 2 1 b1 b2 b1 b2 1 1 1 bs1 qs1 qs1 w 1 exp bs1 qs1 þ qs1 w
1=2 4 4 p2 1z2 1z2 1w 2 1w 2 1
2
1
2
1
2 2 1 1 l l 2 2 1 1 1 2 bs2 qs2 qs2 w 2 b1 q1 þ ql1 z1 bl1 ql1 ql1 z1 bs2 qs2 þ qs2 w 1 4 4 4 4 2 2 1 1 bl2 ql2 þ ql2 z2 bl2 ql2 ql2 z1 dql1 dql1 dql2 dql2 : 2 4 4 ð3:20Þ
j 3 Description of Radiationless Processes in Statistical Large Molecules
38
In our mathematically lax manner, we ignore in Equation 3.20 possible difficulties in interchanging orders of integration and summation. To calculate this fourfold integral, we need the transformation (1.44) of Chapter 1 between the coordinates qs and ql , which in the two-dimensional case is written as l s kð1Þ q1 w11 w12 q 12 1 þ ¼ : ð3:21Þ ql ð2Þ qs w 21 w22 k 2 2 12
In dealing with several modes, which we shall study in Chapter 4, it is customary to ð1Þ ð2Þ use this notation for the displacement vector k12 ¼ colðk12 ; k12 Þ. To facilitate integration, we introduce new coordinates qm ¼ 21=2 qlm þ qlm ð3:22aÞ qm ¼ 21=2 qlm qlm ; m ¼ 1; 2; and correspondingly qm0 ¼ 21=2 qsm þ qsm qm0 ¼ 21=2 qsm qsm ; m ¼ 1; 2: If we combine the transformations (3.22) with (3.21), we find that 1=2 ð1Þ 0 q 1 w11 0 w12 0 q1 2 k12 q0 0 w 0 w12 q1 0 11 1 : þ 0 ¼ 1=2 ð2Þ q 2 w21 0 w22 0 q2 2 k 12 q q0 0 w 0 w 21 22 0 2 2
ð3:22bÞ
ð3:23Þ
With this transformation, the integral appearing in (3.20) is easily performed, giving [107] l 2 s w 2 bs w 1 1 þ w21 w22 bs2 w 2 z1 w11 w12 bs1 w 2 þ b1 11 1 1 þ w21 b2 w q1 dq1 dq1 dq2 dq2 exp kq1 ; q2 k s l q2 w w bs w 2 s 2 s 2 þ w w b w b þ w b þ b w w w z 11 12 1 1 21 22 2 2 12 1 1 22 2 2 2 2 1 l 1 s 1 s 1 1 2 s 1 w 2 bs w 1 q þ w b þ b w w b w þ w w b w z w 11 12 21 22 1 1 1 1 2 2 11 1 1 21 2 2 1 q1 ; q2 s 1 w w bs w q 1 2 s 1 2 s 1 2 2 w12 b1 w 1 þ w22 b2 w 2 þ bl2 z1 2 11 12 1 1 þ w21 w22 b2 w 2
2 2 q s ð1Þ 1 1 þ bs2 kð2Þ 2 : 21=2 w11 bs1 kð1Þ 1 þ w21 bs2 kð2Þ 2 w12 bs1 kð1Þ 1 þ w22 bs2 kð2Þ 2 12 w q2 b1 k12 w 12 w 12 w 12 w 12 w 1 ð
ð3:24Þ
We see that the fourfold integral (3.24) is written as a product of two Gaussian integrals of the form 1 ð
1
1 1 dq1 dq2 exp qt xq þ yt q ¼ 2pðdet xÞ1=2 exp yt x1 y ; 2 2
where q ¼ colðq1 ; q2 Þ
ð3:25Þ
3.2 The Generating Function for Intramolecular Distributions I1 and I2
j39
and
ð1Þ 1 þ w21 bs2 kð2Þ 2 ; 21=2 w12 bs1 kð1Þ 1 þ w22 bs2 kð2Þ 2 y ¼ col 21=2 w11 bs1 k12 w 12 w 12 w 12 w
are the column vectors in the first integral of Equation 3.24. Correspondingly, q ¼ colðq1 ; q2 Þ and y ¼ colð0; 0Þ are in the second integral. The quantity x ¼ xij stands for the square matrices in Equation 3.24. Note that the matrix x in the second 1 m and zm by w integral is obtained from that in the first integral by replacing w m and z1 ðm ¼ 1; 2Þ. Carrying out the integration in (3.24) by twice applying formum la (3.25), the two-dimensional generating function G2 now becomes (by a lot of algebra) [107] 1 D D212 b1 b2 1 1=2 1=2 1 Þð1 þ w 2Þ G2 w1 ; w2 ; z1 ; z2 12 ; ¼ b1 b2 ð1 þ w 12 12 4 D1 D2 b12 b21 2 ; z1 ; z2 Þ w1 ; w A1 ð exp ~ 2 ; z1 ; z2 Þ w1 ; w B 1 ð ð1 þ z1 Þð1 þ z2 Þ ; 2 ð 2 ; z1 z2 Þ 2 ; z1 ; z2 ÞB ½B1 ð w1 ; w w1 w ð3:26Þ where the following abbreviations have been introduced: 2
2
2
1 ð 2 ; z1 ; z2 Þ ¼ b1 Dð1Þ 1 z1 z2 þ b2 Dð2Þ 2 z1 z2 þ b2 Dð12Þ 1w 2 z1 w1 ; w w A 12 w 12 w 1 ð12Þ2
þ b1 D2
1w 2 z2 ; w
2 2 2 1 ð 1w 2 þ w11 1 z2 þ w12 1 z1 þ w22 2 z1 2 ; z1 ; z2 Þ ¼ b1 b2 w B w1 ; w b1 w b12 w b2 w 2 2~ þ w21 b21 w z 2 þ z1 z2 ; 2 2 2 2 ð 2 ; z1 ; z2 Þ ¼ w 1w 2 þ w11 2 z1 þ w12 2 z2 þ w22 1 z2 B w1 ; w b1 w b12 w b2 w 2 1 z1 þ b1 b2 z1 z2 : þ w21 b21 w
ð3:27Þ
Here bm ¼ bsm =blm ;
bmn ¼ bsm =bln ;
ð3:28Þ
m; n ¼ 1; 2;
are the changes of the vibrational frequencies in the s state relative to those in the ðmÞ are the dimensionless displacement parameters scaled as state l and D12 ; Dð12Þ m ðmÞ2
ðmÞ2
ð12Þ2
D12 ¼ blm k12 ; Dð12Þ ¼ bsm km m
where
kð12Þ w11 1 ð12Þ ¼ k w21 2
2
;
ð3:29Þ
m ¼ 1; 2;
1 kð1Þ w12 12 ð2Þ : k w22
ð3:30Þ
12
ðmÞ
ðmÞ
The dimensionless displacement parameters D12 describe the shift k12 of the origin of the electronic state s relative to that of the electronic state l along the displacements coordinate qlm in the unit of ðblm Þ1=2 . The dimensionless Dð12Þ m ð12Þ are related according to Equation 3.29 to the dimensioned displacements km .
j 3 Description of Radiationless Processes in Statistical Large Molecules
40
The latter in turn are obtained from the inverse transformation (3.30) of those ðmÞ ð12Þ given by k12 ðm ¼ 1; 2Þ. Thus, km (the so-called reciprocal displacement compoð12Þ nents), or strictly k , describes the difference of the equilibrium positions of l and s electronic states in the coordinate system with base vectors qlm . We may restate ðmÞ this by saying that an electron sees the displacements D12 during the transition ð12Þ fsmm g ! flnm g in emission and the parameters Dm ðm ¼ 1; 2Þ in absorption flnm g ! fsmm g. We shall return to this question in Section 3.2.5, where the symmetry properties of G2 are discussed. We have purposely used here a rather ðmÞ detailed (and therefore sometimes cumbersome) notation for the parameters D12 ð12Þ and Dm . This has been done to make the discussion in the following sections all the more clear. In Chapter 8, it will often be convenient to extend this notation to higher vibrational degrees of freedom. Returning to our original variables wm and zm ðm ¼ 1; 2Þ, we may also write A1 ðw1 ; w2 ; z1 ; z2 Þ exp B1 ðw1 ; w2 ; z1 ; z2 Þ 1=2 1=2 G2 ðw1 ; w2 ; z1 ; z2 Þ ¼ 4b1 b2 ; ð3:31Þ ½B1 ðw1 ; w2 ; z1 ; z2 ÞB2 ðw1 ; w2 ; z1 ; z2 Þ1=2 where w1 ; w2 ; z1 ; z2 are generally complex variables in the polydisc [108] D4 ð0; 1Þ [|wm | < 1, |zm | < 1 ðm ¼ 1; 2Þ] (Equation 3.17), and A1 ðw1 ; w2 ; z1 ; z2 Þ ¼
1 X
1 X
m1 ;m2 ¼0 n1 ;n2 ¼0
B1 ðw1 ; w2 ; z1 ; z2 Þ ¼
1 X
1 X
m1 ;m2 ¼0 n1 ;n2 ¼0
m
m
ð3:32Þ
am1 m2 ;n1 n2 w1 1 w2 2 zn11 zn22 ;
m
m
ð3:33Þ
m
ð3:34Þ
dm1 m2 ;n1 n2 w1 1 w2 2 zn11 zn22 ;
and B2 ðw1 ; w2 ; z1 ; z2 Þ ¼
1 X
1 X
m1 ;m2 ¼0 n1 ;n2 ¼0
m
bm11 m2 ;n1 n2 w1 1 w2 2 zn11 zn22 :
The quantities dm1 m2 ;n1 n2 ; am1 m2 ;n1 n2 ; and bm11 m2 ;n1 n2 in Equations 3.32, 3.33 and 3.34, respectively, which constitute tensors of the fourth rank, are real and given by ð1Þ2
ð2Þ2
dm1 m2 ;n1 n2 ¼ ðÞm1 þ n1 þ n2 b1 D12 þ ð1Þm2 þ n1 þ n2 b2 D12 ð12Þ2
þ ð1Þm1 þ m2 þ n1 b2 D1
ð12Þ2
þ ð1Þm1 þ m2 þ n2 b1 D2
;
2 2 b1 þ ð1Þm1 þ n1 w12 b12 am1 m2 ;n1 ;n2 ¼ ð1Þm1 þ m2 b1 b2 þ ð1Þm1 þ n2 w11 2 2 þ ð1Þm2 þ n1 w22 b2 þ ð1Þm2 þ n2 w21 b21 þ ð1Þn1 þ n2
ð3:35Þ
ð3:36Þ
and bm1 m2 ;n1 n2 ¼ ð1Þm1 þ m2 þ n1 þ n2 am1 m2 ;n1 n2 :
ð3:37Þ
3.2 The Generating Function for Intramolecular Distributions I1 and I2
Equation 3.35 defines in the representation of nonseparable modes a new set of displacement parameters, whereas Equation 3.36 defines the new set of terms, which depend on all frequency factors. Equations 3.35–3.37 are functions of eight dimensionless parameters, namely, four positive b-parameters b1 ; b2 ; b12 ; and b21 and four D-parameters, which are real numbers. In our special case, where the matrix in Equation 3.21 is orthogonal, the latter are reduced to three independent parameters D1 ; D2 , and w, where w is a rotation angle, which (see later) parameterizes the matrix (3.21). 3.2.2 Properties of dm1m2,
n1n2,
am1m2, n1n2, and bm1m2,
n1n2
First, note that the 16 components of the tensor dm1 m2 ;n1 n2 are not independent and we can reduce them to 8 by noting that dm1 m2 ;n1 n2 ¼ d1m1 ;1m2 ;1n1 ;1n2 :
ð3:38Þ
A further reduction is accomplished with the help of the relations d00;00 þ d00;10 þ d00;01 þ d00;11 d01;00 þ d01;10 þ d01;01 þ d01;11 d10;00 þ d10;10 þ d10;01 þ d10;11 d11;00 þ d11;10 þ d11;01 þ d11;11
¼0 ¼0 ¼0 ¼0
ð3:39Þ
in which the last two relations are obtained from the first two by taking into account Equation 3.38. This indicates that six independent components are required to specify the generating function. It can be reduced still further to five in the special case if we assume that the matrix (3.21) is orthogonal. According to the definition (3.35), the parameters dm1 m2 ;n1 n2 can be treated as new displacement parameters. Similarly, it follows directly from (3.36) that am1 m2 ;n1 n2 is unaltered by the interchange m1 ! 1m1 ; m2 ! 1m2 ; n1 ! 1n1 ; and n2 ! 1n2 . Thus, it is sufficient to specify the values of am1 m2 ;n1 n2 for the two values of the pair ðm1 m2 Þ and the same two values of the pair (n1 n2 ). The reader may also convince himself that a00;00 þ a00;10 þ a00;01 þ a00;11 a01;00 þ a01;10 þ a01;01 þ a01;11 a10;00 þ a10;10 þ a10;01 þ a10;11 a11;00 þ a11;10 þ a11;01 þ a11;11
¼ 4b1 b2 ¼ 4b1 b2 ¼ 4b1 b2 ¼ 4b1 b2 ;
ð3:40Þ
which reduces the number of independent components to two. Finally, according to Equation 3.37, we obtain in the same manner b00;00 þ b00;10 þ b00;01 þ b00;11 b01;00 þ b01;10 þ b01;01 þ b01;11 b10;00 þ b10;10 þ b10;01 þ b10;11 b11;00 þ b11;10 þ b11;01 þ b11;11
¼4 ¼ 4 ¼ 4 ¼ 4:
ð3:41Þ
j41
j 3 Description of Radiationless Processes in Statistical Large Molecules
42
3.2.3 Case w1 ¼ w2 ¼ 0
Before we analyze the generating function G2 and the corresponding distributions in greater detail, let us consider the special case of the so-called zero-temperature limit, which is adequate for many practical purposes. In that case, w1 ¼ w2 ¼ 0 and we obtain from (3.31) ! ð1Þ ð2Þ D12 D12 b1 b2 G2 0; 0; z1 ; z2 ð12Þ ; ð12Þ b b21 D1 D2 12 ð3:42Þ d00;00 þ d00;10 z1 þ d00;01 z2 þ d00;11 z1 z2 exp a00;00 þ a00;10 z1 þ a00;01 z2 þ a00;11 z1 z2 1=2 1=2 ; ¼ 4b1 b2 ½ða00;00 þ a00;11 z1 z2 Þ2 ða00;10 z1 þ a00;01 z2 Þ2 1=2 which represents the kernel of G2 ðw1 ; w2 ; z1 ; z2 Þ. The mathematical subtleties in two dimensions though are more difficult than they are in one. We are restating here conclusions obtained in Equation 4.4. The functions G1 ð0; zÞ and G2 ð0; 0; z1 ; z2 Þ exhibit a remarkable regularity. This is manifested in the similarity of the functions with respect to their exponents, which have many of the same structural features. (They have the topology of a torus of the dimension one for N ¼ 1 and of two for N ¼ 2, respectively). Both of them vanish when z ¼ 1 or z1 ¼ z2 ¼ 1, respectively. Analogous to the one-dimensional case, the mapping of the bidisc [108] D2 ð0; 1Þ [|z1 | 1, |z2 | 1] by G2 ð0; 0; z1 ; z2 Þ constitutes a domain confined by exp½b1 D21 b2 D22 jG2 ð0; 0; z1 ; z2 Þj 1 and in particular G2 ð0; 0; z1 ; z2 Þ is 1, when both z1 and z2 reach 1. The point G2 ¼ 0 is a bifurcation point of infinity order. This behavior of the generating function is valid, as will be further substantiated, for higher dimensions N. 3.2.4 Case w1 6¼ w2 6¼ 0
The G2 ðw1 ; w2 ; z1 ; z2 Þ of Equation 3.31 is holomorphic in the polydisc D4 ð0; 1Þ and has the expansion in a series of w1m1 w2m2 zn11 zn22 : ! ð1Þ ð2Þ D12 D12 b1 b2 G2 w1 ; w2 ; z1 ; z2 ð12Þ ; ð12Þ b D1 D2 12 b21 ! ð3:43Þ ð1Þ 1 1 X X b1 b2 m1 ; m2 D12 Dð2Þ 12 m1 m2 n1 n2 w 1 w2 z 1 z 2 ; I2 ; ¼ n1 ; n2 Dð12Þ Dð12Þ b12 b21 m1 ;m2 ¼0 n1 ;n2 ¼0 2 1 m1 m2 is, as will be shown below, for each pair of nonnegative integers where I2 n1 n2 (m1 ; m2 ), a two-dimensional probability distribution of n1 ; n2 and vice versa. On the other hand, from Equations 3.17–3.20, it follows that I2
m1 n1
m2 n2
ð ð1 ¼ 1
dq1 dq1 dq2 dq2 xsm ðqs Þxsm ð qs Þxln ðql Þxln ð ql Þ:
ð3:44Þ
3.2 The Generating Function for Intramolecular Distributions I1 and I2
In Equation 3.43, the dependence of the generating function and their distributions on the parameters are exhibited explicitly. For the physical situation described above, ðlÞ we can set zm ¼ exp ivm t and wm ¼ exp a=Tivsm t ðm ¼ 1; 2Þ, with a being a positive number, especially a ¼ hvsm =kB T, or in another modification, ðlÞ zm ¼ exp a=T þ ivm t and wm ¼ exp ivsm t , where t is a time variable.1) m1 m2 To verify that the coefficients I2 in the series (3.43) are for each pair of n1 n2 levels ðm1 ; m2 Þ and values of a distribution for several sets of choices ðn1 ; n2 Þ and vice versa, we first note the simple property of G2 : A1 ðw1 ; w2 ; z1 ; z2 Þ exp B1 ðw1 ; w2 ; z1 ; z2 Þ 1=2 1=2 G2 ðw1 ; w2 ; z1 ; z2 Þ ¼ 4b1 b2 ; ð3:45Þ ½B1 ðw1 ; w2 ; z1 ; z2 ÞB2 ðw1 ; w2 ; z1 ; z2 Þ1=2 which follows directly from Equations 3.31–3.34. In other words, the complex conjugate of G2 is obtained simply by replacing the variables wm and zm with their with conjugates wm and zm ðm ¼ 1; 2Þ. In conjunction (3.43), it follows that the m1 m2 coefficients of the series (3.43), I2 n1 n2 , are real. In particular, m1 m2 0 for all pairs of levels (m1 ; m2 ) or ðn1 ; n2 Þ by definition. (This I2 n1 n2 point emerges clearly from the fourfold integration approach to evaluation of the generating function G2 and Equation 3.44). Finally, it is a simple matter to verify that for each pair of levels ðm1 ; m2 Þ, 1 X m1 m2 I2 ¼ 1: ð3:46Þ n1 n2 n ;n ¼0 1
2
For the proof of (3.46), it is convenient to express bilinear form [109]: d00;00 d 10;00 A1 ðw1 ; w2 ; z1 ; z2 Þ ¼ k1; w1 ; w2 ; w1 w2 k d01;00 d 11;00
A1 ðw1 ; w2 ; z1 ; z2 Þ in terms of a d00;10 d10;10
d00;01 d10;01
d01;10 d11;10
d01;01 d11;01
d00;11 1 d10;11 z1 d01;11 z2 z z d 11;11
1 2
¼ wt kdm;n k41 z; ð3:47Þ
where W and z are column matrices col(1, w1 ; w2 ; w1 w2 ) and col(1; z1 ; z2 ; z1 z2 ), respectively, m ¼ ðm1 ; m2 Þ; and n ¼ ðn1 ; n2 Þ. The sign t in (3.47) denotes transposition. This matrix approach is very convenient for generalization of three, four, or more dimensions. If the number of the vibrational modes becomes very large, that is, N, then the order of the square matrix in (3.47) is 2N . It follows from (3.39) that the
1) We note a certain ambiguity in the definition of the variables wm and zm. The ambiguity is, however, not genuine and therefore the definition can not be arbitrarity. This becomes evident in the applications. The simplest case is, if we assume wm and zm to be dummy variables.
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44
sum of the elements of each row, each column, and any main diagonals is the same, namely, zero (compare with a magic square). Similarly, representing B1 ðw1 ; w2 ; z1 ; z2 Þ in the form of a product of three matrices, a row, a square, and a column matrix, 4 B1 ðw1 ; w2 ; z1 ; z2 Þ ¼ wt am;n 1 z; ð3:48Þ where, according to (3.40), the sum of elements in the first, second, third, and fourth row of the square matrix in (3.48) are 4b1 b2 ; 4b1 b2 ; 4b1 b2 , and 4b1 b2 , respectively. Correspondingly, the sum of elements in the first, second, third, and fourth columns are 4, 4, 4, and 4, respectively. Finally, we note that 4 B2 ðw1 ; w2 ; z1 ; z2 Þ ¼ wt bm;n 1 z: ð3:49Þ 4 Here the sum of the elements in each 4 row of bm;n 1 is the same as the sum of the elements in the columns of am;n 1 and vice versa. By direct substitution in Equations z1 ¼ z2 ¼ 1 and taking into 4 3.47–3.49 4 4 account the above properties of dm;n 1 ; am;n 1 , and bm;n 1 , we have after matrix multiplication A1 ðw1 ; w2 ; 1; 1Þ ¼ 0 B1 ðw1 ; w2 ; 1; 1Þ ¼ 4b1 b2 ð1w1 Þð1w2 Þ B2 ðw1 ; w2 ; 1; 1Þ ¼ 4ð1w1 Þð1w2 Þ:
ð3:50Þ
Note that the right-hand side of (3.43) converges as z1 ! 1 and z2 ! 1. Substituting these expressions in (3.31) gives G2 ðw1 ; w2 ; 1; 1Þ ¼
1 X 1 ¼ w m1 w m2 : ð1w1 Þð1w2 Þ m1 ;m2 ¼0 1 2
ð3:51Þ
Comparing this result with (3.43), we have m1 m2 G2 ðw1 ; w2 ; 1; 1Þ ¼ I2 w1m1 w2m2 n1 n2 m1 ;m2 ¼0 n1 ;n2 ¼0 ! 1 1 X X m1 m2 w1m1 w2m2 ; ¼ I2 n n 1 2 m1 ;m2 ¼0 n1 ;n2 ¼0 1 X
1 X
ð3:52Þ
which completes the proof of (3.46). Equation 3.46 underlines the correctness and m1 m2 . generality of our definition of I2 n1 n2 4 ð0; 1Þ [|zm | < 1, Similarly, if we consider the function (3.31) in the polydisc D |wm | 1; m ¼ 1; 2], we have for each pair of levels (n1 ; n2 ) 1 X m1 ;m2 ¼0
I2
m1 n1
m2 n2
¼ 1:
ð3:53Þ
3.2 The Generating Function for Intramolecular Distributions I1 and I2
Proof Analogous to the foregoing treatment, we have A1 ð1; 1; z1 ; z2 Þ ¼ 0 B1 ð1; 1; z1 ; z2 Þ ¼ 4ð1z1 Þð1z2 Þ B2 ð1; 1; z1 ; z2 Þ ¼ 4b1 b2 ð1z1 Þð1z2 Þ
ð3:54Þ
and this gives the series for the generating function (3.31) G2 ð1; 1; z1 ; z2 Þ ¼
1 X 1 zn1 zn2 : ¼ ð1z1 Þð1z2 Þ n1 ;n2 ¼0 1 2
Expressing (3.43) in a different manner, we obtain ! 1 1 X X m1 m2 zn11 zn22 : G2 ð1; 1; z1 ; z2 Þ ¼ I2 n n 1 2 n ;n ¼0 m ;m ¼0 1
2
1
ð3:55Þ
ð3:56Þ
2
On comparison with the series (3.55) follows Equation 3.53. 3.2.5 m1 Symmetry Properties of I2 n1
m2 n2
The matrix representation of A1 ðw1 ; w2 ; z1 ; z2 Þ (and similarly of B1 and B2 ) introduced above allows us to investigate the question of how the distribution I2 is affected by exchange of parameters. To be explicit, we will investigate the behavior of I2 under the following change of parameters: ð1Þ
ð12Þ
ð2Þ
ð12Þ
1 1 D12 to D1 ; D12 to D2 ; b1 to b1 1 ; b2 to b2 ; b12 to b21 :
ð3:57Þ
Using formula (3.35), one can prove that utilizing the change (3.57), the coefficient matrix of the form A1 ðw1 ; w2 ; z1 ; z2 Þ in (3.47) transforms to dm;n 4 ! b1 b1 dn;m 4 ; 1 2 1 1
ð3:58Þ
where the matrix on the right-hand side of (3.58) is the transposition of the original in (3.47). Analogously, it follows from Equations 3.36 and 3.37 that by changing the parameters as (3.57), 4 am;n ! b1 b1 an;m 4 1 2 1 1
ð3:59Þ
and similarly, 4 bm;n ! b1 b1 bn;m 4 ; 1 2 1 1
ð3:60Þ
where use has been made of the fact that the matrix elements of (3.21) obey w11 ¼ w22 ¼ cos w and w12 ¼ w21 ¼ sin w after parametrization of the rotation matrix W.
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Combining the above change of parameters (3.57) with the interchange of the variables ðw1 ; w2 Þ $ ðz1 ; z2 Þ, the following relations hold:2) 4 4 4 1 t 1 1 t A1 ðw1 ; w2 ; z1 ; z2 Þ ¼ wt dm;n 1 z ! b1 1 b2 z dn;m 1 w ¼ b1 b2 w dm;n 1 z; ð3:61Þ 4 4 4 1 1 1 1 B1 ðw1 ; w2 z1 ; z2 Þ ¼ wt am;n 1 z ! b1 b2 zt an;m 1 w ¼ b1 b2 wt am;n 1 z; ð3:62Þ
and
4 4 4 1 t 1 1 t B2 ðw1 ; w2 z1 ; z2 Þ ¼ wt bm;n 1 z ! b1 1 b2 z bn;m 1 w ¼ b1 b2 w bm;n 1 z: ð3:63Þ
Combining Equations 3.61 through 3.63, the exchange of parameters (3.57) produces the result: A1 ðw1 ; w2 ; z1 ; z2 Þ A1 ðz1 ; z2 ; w1 ; w2 Þ ¼ ; B1 ðw1 ; w2 ; z1 ; z2 Þ B1 ðz1 ; z2 ; w1 ; w2 Þ
and correspondingly ! Dð1Þ Dð2Þ b b Dð12Þ Dð12Þ b1 b1 12 1 2 12 1 2 ¼ G2 z1 ; z2 ; w1 ; w2 ð1Þ ð2Þ ; 11 21 : G2 w1 ; w2 ; z1 ; z2 ð12Þ ð12Þ ; D D D b21 b12 b12 b21 D2 1 12 12 ð3:64Þ
If we now expand both sides of the identity (3.64) in the polydisc D4 ð0; rÞ according to (3.43) in a power series and equate the terms of w1m1 w2m2 zn11 zn22 , we have the following: Corollary 3.1 The distribution I2 is unaltered by the exchange of parameters (3.57), provided that the integer variables mm and nm are simultaneously exchanged, mm $ nm ! ! ð1Þ ð2Þ ð12Þ ð12Þ b1 b1 m1 m2 D12 D12 b1 b2 n1 n2 D1 D2 1 2 ¼ I2 : I2 ; ; n1 n2 Dð12Þ Dð12Þ b12 b21 m1 m2 Dð1Þ Dð2Þ b1 b1 21 12 2 1 12 12 ð3:65Þ This says that due to the presence of the cross-frequency parameters b12 and b21 ðmÞ in (3.65), as well as the fact that Dð12Þ 6¼ D12 , there exists no mirror images in respect m to ðm1 ; m2 Þ $ ðn1 ; n2 Þ (i.e., in emission and absorption spectra). This holds only if the rotation angle w ¼ 0 and the frequency changes b1 ¼ b2 ¼ 1 (see below). Similarly, since the indices 1 and 2 in (3.43) are indistinguishable, they can exchange roles: ! ! ð1Þ ð2Þ ð2Þ ð1Þ b b m1 m2 D12 D12 b1 b2 m2 m1 D12 D12 2 1 ¼ I2 : I2 ; ; n1 n2 Dð12Þ Dð12Þ b12 b21 n2 n1 Dð12Þ Dð12Þ b21 b12 2 2 1 1 ð3:66Þ 2) In the expressions 3.61–3.63 the variables w and z are treated as dummy variables.
3.2 The Generating Function for Intramolecular Distributions I1 and I2
The proof of this identity results from the fact that the coefficients dm1 m2 ;n1 n2 and am1 m2 ;n1 n2 appearing in the generating function G2 are invariant under the operation F (flip), which follows simply by changing m1 to m2 and n1 to n2 dm1 m2 ;n1 n2 ¼ dm2 m1 ;n2 n1 ¼ Fdm1 m2 ;n1 n2 am1 m2 ;n1 n2 ¼ am2 m;n2 n1 ¼ Fam1 m2 ;n1 n2
as well as the parameters of I2 as displaced in (3.66) explicitly. Equations 3.65 and 3.66 are very valuable for calculating I2 . 3.2.6 Case w ¼ 0 ð12Þ
ðmÞ
If w ¼ 0, it 2follows from (3.21), (3.29), and (3.30) that km ¼ k12 and 2 ðmÞ ¼ bm D12 ðm ¼ 1; 2Þ. In this special case, Equations 3.32–3.37 can be written Dð12Þ m as follows: A1 ðw1 ; w2 ; z1 ; z2 Þ ¼
ð1Þ2
b1 D12 ð1w1Þ Þð1z1 Þ½ð1 þ w2 Þð1z2 Þ þ b2 ð1w2 Þð1 þ z2 Þ ð2Þ2
þ b2 D12 ð1w2 Þð1z2 Þ½ð1 þ w1 Þð1z1 Þ þ b1 ð1w1 Þð1 þ z1Þ Þ; 2 Y B1 ðw1 ; w2 ; z1 ; z2 Þ ¼ ½bm ð1wm Þð1 þ zm Þ þ ð1 þ wm Þð1zm Þ; m¼1
and B2 ðw1 ; w2 ; z1 ; z2 Þ ¼
2 Y
½bm ð1 þ wm Þð1zm Þ þ ð1wm Þð1 þ zm Þ:
m¼1
Dividing A1 by B1, we find that ð1Þ2
A1 ðw1 ; w2 ; z1 ; z2 Þ b1 D12 ð1w1 Þð1z1 Þ ¼ B1 ðw1 ; w2 ; z1 ; z2 Þ b1 ð1w1 Þð1 þ z1 Þ þ ð1 þ w1 Þð1z1 Þ ð2Þ2
b2 D12 ð1w2 Þð1z2 Þ þ ; b2 ð1w2 Þð1 þ z2 Þ þ ð1 þ w2 Þð1z2 Þ
where the right-hand side breaks down into two terms, each of which depends on ðmÞ variables wm ; zm and parameters D12 and bm of only one component m (the crossparameters b12 and b21 disappear). Thus, in the case of w ¼ 0, the two-dimensional GF can simply be written as a product of two single-mode GF: G2 ðw1 ; w2 ; z1 ; z2 Þ ¼ G1 ðw1 ; z1 ÞG1 ðw2 ; z2 Þ;
ð3:67Þ
where exp
bD2 ð1wÞð1zÞ bð1wÞð1 þ zÞ þ ð1 þ wÞð1zÞ
G1 ðw; zÞ ¼ 2b1=2
1=2 ð1 þ b2 Þð1w 2 Þð1z2 Þ þ 2b½ð1 þ w 2 Þð1 þ z2 Þ4wz ð3:68Þ
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is clearly an one-dimensional GF (see later). The result obtained can be stated as follows: Corollary 3.2 If the angle w ¼ 0, the two-dimensional GF G2 ðw1 ; w2 ; z1 ; z2 Þ factors into a product of one-dimensional terms G1 , each of which depends on variables and parameters belonging to one component only.
3.3 Derivation of the Promoting Mode Factors Kg(t) and Ig(t)
Before we examine further the behavior of the generating function G2 ðtÞ, let us return to Equation 3.16 for the transition probability. To this end, we have yet to obtain the expression for the factor Kg ðtÞ, which includes the q=qqg overlap integral arising from the promoting mode (3.14). Proceeding as in the previous manner and writing Equation 3.14 explicitly with the help of Equation 3.18, we find that
1=2
ð1 ð bsg blg 2 2 1 i q 1 h 2 g þ qsg qsg w g Kg ðtÞ¼ dqlg dqlg i s exp bsg qsg þqsg w 1=2 h qqg 4 p 1wg2 1z2g
1 h 2 2 i q 1 i l exp blg qlg þqlg zg þ qlg qlg z1 g 4 qqg 1=2
ð1 ð bsg blg s s 2 1 i 1 s h s s 2 2 l l q w w ¼ h dq d q þ q þ q q b exp g 1=2 g g g g g 4 g g g p 1wg2 1z2g 1
2 2 i 1 h exp blg qlg þqlg zg þ qlg qlg z1 g 4
h 1 i i 1 1 h g þ qsg qsg w g blg qlg þqlg zg qlg qlg z1 : bsg qsg þqsg w g 2 2 ð3:69Þ
Introducing now, as above, new coordinates for the gth promoting mode qg ¼ 21=2 qlg þ qlg qg ¼ 21=2 qlg qlg
q0g ¼ 21=2 qsg þ qsg q0g ¼ 21=2 qsg qsg
ð3:70Þ
according to (3.23), the relations q0g ¼ qg þ 21=2 kg q0g ¼ qg
ð3:71Þ
are obtained. Substituting (3.70) and (3.71) into Equation 3.69 and integrating, we obtain
3.3 Derivation of the Promoting Mode Factors Kg(t) and Ig(t)
Kg ðtÞ ¼
8 9 > > = 2bsg blg k2g 1 2 s l < 1 1 ðgÞ þ h bg bg h i 2 G1 ðtÞ s l l 1 > 2 s 1 l 1 > g bsg z1 g :bg zg þ bg w ; g þ bg w g bg zg þ bg w ðgÞ
¼ Kg0 ðtÞG1 ðtÞ;
ð3:72Þ
where bsg ¼ vsg =h and blg ¼ vlg =h are the frequency factors of the promoting mode g in the states s and l and kg is the geometrical displacement between the potential surfaces in the configuration space along the promoting mode coordinate qg . If the promoting mode is nontotally symmetric, one can assume that kg ¼ 0 and bg ¼ bsg =blg 1
and it is clearly sufficient to reduce Equation 3.72 to the much simpler form in conformity with [110]
1 Kgð0Þ ðtÞ ¼ h hvg =2kB TÞ1 eivg t ; vg cothðhvg =2kB TÞ þ 1 eivg t þ cothð 4 ð3:73Þ
where the substitutions (3.17) have been made for the variables wg and zg . Analogously, one can prove from Equation 3.15 that Ig ðtÞ ¼ ih
bsg blg kg l 1 g bsg z1 g þ bg w
g
G1 ðtÞ:
ð3:74Þ
This vanishes if, as in this case, the promoting mode g is nontotally symmetric, giving kg ¼ 0. Having calculated the generating functions Kg ðtÞ and GN1 ðtÞ, we are now in a position to obtain the final expression for the transition probability (3.16). Substituting the expression for Kg ðtÞ (Equation 3.73) into Equation 3.16 yields ( 1 ð X 1 vg g 2 R ½cothðhvg =2kB TÞ þ 1 dt hwnonrad iT ¼ Z sl 4 h g 1
1 exp itðVvg ÞCh jtj GN ðtÞ ) 1 ð
1 þ ½cothðhvg =2kB TÞ1 dt exp itðV þ vg ÞC h jtj GN ðtÞ : 1
1
ð3:75Þ
In writing Equation 3.75, we have included the single-mode generating function g G1 ðtÞ from (3.72) into GN ðtÞ. The former is reduced in the approximation used above g to G1 ðtÞ ¼ ð1expðhvg =kB TÞÞ1 and its contribution to GN ðtÞ is approximately unity. From Equation 3.75, we deduce that the effect of the promoting mode is to decrease or increase the effective energy gap to hðV vg Þ. For transitions that terminate in the first vibrational excited level ng ¼ 1 of the l electronic state, the
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energy gap is decreased by an amount hvg . It is increased at about the same vibrational energy if the transition take place from the first vibrational excited level mg ¼ 1 of the s electronic state (see also Appendix K, case b). Since the second term in Equation 3.75 appears only at high temperatures, at low temperatures extending to room temperatures, it is negligibly small. This development bears a strong resemblance to vibronic induced optical transitions (see Section 7.1). The latter are characterized, as the nonradiative transitions, by a false origin at the energy hvg off the 0–0 line and can be formally regarded as a symmetry-forbidden emission process, where the nontotally symmetry modes play the roles of promoting modes that induce the optical transition. We now return to the calculation of (3.75). Using Equations 3.16 and 3.43 and the transformation 1 ð 1 2c expðcjxjÞ ¼ dy expðixyÞ 2 ; ð3:76Þ 2p y þ c2 1
by setting c ¼ C=h for the decay time, the integrals in Equation 3.75 may now be represented in terms of the following lineshape function: I 2 ðV vg Þ ¼
1 ð
dt exp itðV vg Þcjtj GN ðtÞ
1
! 2 X 2c X X m1 m2 s exp h mm vm =kB T dy 2 I2 n1 n2 y þ c2 m¼1 m n f g f g m m 1 " !# 1 ð 2 2 X X mm vsm nm vlm þ y dt exp it V vg þ 1 ¼ 2p
1 ð
m¼1
1
¼
P P fmm g fnm g
I2
m1 n1
m¼1
2 X 2c exp h mm vsm =kB T
!
m¼1
2 2 X X mm vsm nm vlm V vg þ m¼1 m¼1 ! ð1Þ ð2Þ m2 D12 D12 b1 b2 : ; n2 Dð12Þ Dð12Þ b12 b21 1
ð3:77Þ
!2 þ c2
2
To evaluate the last result we use the representations 1 ð
dteiVt ¼ 2pdðVÞ
ð3:78Þ
f ðxÞdðxyÞdx ¼ f ðyÞ
ð3:79Þ
1
and 1 ð
1
with the latter being valid for each continuous function f ðxÞ.
3.3 Derivation of the Promoting Mode Factors Kg(t) and Ig(t)
Equation 3.75 in conjunction with Equation 3.77 provides an explicit expression for the nonradiative transition probability, where the width c is assumed to be independent of the particular vibronic levels lnm . This expression is general, being applicable for both the statistical limit and for the small molecule cases. The Lorentzian function in (3.77) exhibits a sharp peak around P P V vg ¼ m mm vm þ m nm vm . The height of this peak is 2=c, while its width is given by c. The sharp peak of the Lorentzian function around P V ¼ vg m ðmm vsm nm vlm Þ very strongly favors the transitions toward those final resonance levels nm of the l electronic state, the so-called close coupled levels, for P which the quantity V vg þ m ðmm vsm nm vlm Þ does not deviate from zero by an amount larger than c. Thus, the nonradiative transitions occur mainly toward those P final states, the energies of which El0 þ m nm hvlm do not differ from the initial energy P hðV vg þ m mm vsm Þ by more than DE þ Esm Eln c h. Hence, the transition results in an approximate conservation of energy, the spread in energy being given by c. Since the manifold of final states lnm becomes more densely spaced with the increase in the energy gap DE ¼ Es0 El0 between the two electronic states s and l in view of the large number of possible combinations of fundamental vibrational modes, the background of states lnm consists of a dense distribution of vibronic states. In this case, for the so-called statistical limit hc r1 l , where rl is the density of the final states, the overlapping Lorentzian peaks in the lineshape function (3.77) yield a smooth function of energy, which is practically independent of c [111]. The situation is quite different in the small molecule case, where only a few or a single intramolecular vibrational mode acts as an accepting mode. This situation ðmÞ prevails in diatomic and triatomic molecules. For D12 < 1, it is possible that the largest contribution to the decay rate (originating for instance from the lowest vibrational level of the excited state) will not originate from the close lying levels of the final electronic state, but rather from off-resonance low-lying states (with smaller nm values), which contribute via the tail of the Lorentzian distribution. In the P case of accidental degeneracy, when ðV m nm vlm Þ c and provided that the ðmÞ displacements of the potential surfaces D12 are not too small, it is usually justified to simply drop the frequency term in the denominator of (3.77) to write (in the zero-temperature limit) w
vg g 2 0 Rsl I2 n1 hc
0 : n2
ð3:80Þ
The main feature of this result is the dependence of w on the reciprocal of c. This situation corresponds to the Robinson–Frosch formula, applicable for the case of near-degeneracy in a small molecule embedded in an inert medium (Shpolskii matrix [112]). If the major contribution to (3.77) originates from the off-resonance P low-lying levels, that is, ðV m nm vlm Þ c, the transition decay rate will vary as hcðhVÞ2 I2 , so that the nonradiative transition probability is linear with the coupling to the medium, expressed in terms of the width hc. The energy gap law for the nonradiative decay of a small molecule in a dense medium is not expected to be of general validity, as in the case for large molecules. The energy gap law w / I1 ðnÞ,
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where n ffi V=vlm , applies only when the major contribution will originate from nearresonance coupling.
3.4 Radiationless Decay Rates of Initially Selected Vibronic States in Polyatomic Molecules
Until now the discussion of electronic relaxation processes in large molecules embedded in an inert medium implicitly assumed that the nonradiative decay occurs from a manifold of thermally equilibrated levels of the initial electronic state. In the present section, we present an expression for the nonradiative decay probability of a single vibronic level of a large isolated molecule. We consider a molecule that has a set of zero-order selectable vibronic states ysma , belonging to electronic state s, which are optically accessible and well separated from each other. These states can undergo radiationless transitions to some other zero-order set of vibronic states n o ylnm that belong to a lower electronic state l of any multiplicity but of a density sufficiently large in the region of ysmm so that we can safely assume that the largemolecule statistical limit ensures (Figure 2.1). The crucial questions that now arise are (1) is the initial step in the vibrational relaxation dominated by an intramolecular process or by direct energy transfer to the host and (2) if it is intramolecular, what is the role of the host. In this respect it is important to mention the results of Amirav et al. [113] in the relaxation of isolated large molecules (tetracene, pentacene) cooled in a supersonic jet. They observed predominantly unrelaxed fluorescence from levels with vibrational energy smaller than 1200 cm1 . This prove that a free molecule as large as pentacene with 102 vibrations does not have enough degrees of freedom to act as its own heat bath in the low vibrational energy range. Electronic relaxation in different excited vibronic levels corresponding to the same electronic configuration can be experimentally studied, provided that, as mentioned above, (1) single vibrational levels within the initial electronic state are populated and (2) the excited molecule decays nonradiatively on a timescale much shorter than the mean time between deactivating collisions or by other means such as infrared fluorescence [115]. For typical polyatomic molecules in the gas phase, a narrow-band optical excitation pulse (as small as 1 A) and shorter relative to the genuine decay times c1 s will result in the selection of a single vibronic state. Under these conditions, the emission lifetimes and quantum yields of individual vibronic levels have been measured for several organic molecules [115–121]. We assume further that upon optical excitation to the state ysma from the ground electronic state, only the ath vibrational mode (the optical mode) is excited with ma quanta. The theory can be easily generalized to include cases in which more than one vibrational mode is excited in the optical selected state ysmm . The rate for nonradiative decay of the initially prepared state can be written in the golden rule form 2 X g 2 C wsl ðma Þ ¼ ; ð3:81Þ Vsm;ln h n ðEsma Eln Þ2 þ C2
3.4 Radiationless Decay Rates of Initially Selected Vibronic States in Polyatomic Molecules g
where Vsm ln is the electronic factor that includes the q=qqg overlap integral arising from the promoting mode g (see Equation 3.3) and Esma Eln ¼ DE þ hma vsa hna vla
X m
hnm vlm ;
with DE ¼ Es0 El0
being the energy gap between the lowest vibronic levels in the s and l electronic states. The summation on n includes the set of vibronic levels of the final electronic states jlna i and that of the remaining modes that are not finally in the optical mode in jli. At first sight, it appears that much of the formal derivation can be taken over s directly from the theory in Section 3.3 by specifying the complex variable w ¼ eiva t (i.e., omitting the Boltzmann factor hvsa =kB T in the exponent). We must dispel any apprehensions that Equation 3.81 differs from the thermally averaged rate expression (3.16) since thermal averaging must be avoided here. At this point we have to depart from the previous derivation of the thermal averaging of the generating function Kg ðtÞ for the promoting mode(s) g. The corresponding factor now takes the form ~ g ðtÞ ¼ h2 K
1 Xð ð ng
1
dqlg dqlg i
s1=2 s l1=2 l s1=2 s q b q x b q x b q x qqsg smg g g lng g g smg g g
1=2 m n q i l xlng blg qlg wg g zgg ; qqg
ð3:82Þ
s
where now wg ¼ eivg t and zg are still given by Equation 3.17. Interchanging orders of summation and integration in (3.82) and noting that qxav ¼ qq
) rffiffiffiffiffiffiffiffiffiffi rffiffiffiffiffiffi(rffiffiffi va v vþ1 x x 2 av1 2 av þ 1 h
ð3:83Þ
(where use has been made of the fact that ba ¼ ðva = hÞ1=2 ), Equation 3.82 can be considerably simplified to Equation 3.84 by assuming as above that for nontotally symmetric promoting modes Dg ¼ 0 and bg ¼ 1, ~ g ðtÞ ¼ K
hvg ðmg þ 1Þeivg t þ mg eivg t : 2
ð3:84Þ
The expression for the nonradiative decay rate of the optically prepared state jsma i now becomes wsl ðma Þ ¼
v g g 2 Rsl ðmg þ 1Þ~I 2 ðVvg Þ þ mg~I 2 ðV þ vg Þ ; 2h
ð3:85Þ
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where for gthe present we have assumed that there is only one (promoting) mode for which Rsl 6¼ 0. The expression ~I2 ðV vg Þ in Equation 3.85 is written as ~I 2 ðV vg Þ ¼
X n
I2
2c ðV vg þ ma vsa na vla nm vlm Þ2 þ c2 ðaÞ ðmÞ ! ma 0m D12 D12 ba bm ð12Þ ð12Þ ; bam bma na nm Da Dm
ð3:86Þ
and differs from Equation 3.77 in that now the (normalized) Boltzmann weights (3.7) assigned to each state of energy Es;ma are omitted and the summation is restricted only to the final manifold of vibronic levels n ¼ ðna ; nm Þ. If the optical mode is parallel to those due to the rest of the molecule, it is natural to employ the partitioning technique to separate the optical mode from the other modes. Thus, the two-dimensional ID in Equation 3.86 decomposes in a convolution of two onedimensional IDs, each for the individual modes a and m. As is shown in Chapter 4, the theory is easily generalized to include cases in which more than one vibrational mode is optically selected and more than two accepting modes ða; mÞ are involved in the transition s ! l. Several comments should be made at this point. (a) The effective energy gap is modified by the energy of the promoting mode h vg . The propensity rule for the promoting mode (previously derived for molecular nonradiative processes under thermally equilibrium conditions) is also satisfied for the decay of any single vibronic state [122]. (b) Furthermore, it is instructive to see how that analysis emerges in the limit ma ! 0. The nonradiative decay rate from the lowest vibronic level of the excited electronic state, whereupon mm ¼ 0 for all modes m, is obtained from Equation 3.85 in the form v g g 2 Rsl I 2 ðVvg Þ; wsl ðma ¼ 0Þ ¼ ð3:87Þ 2h since in this case ~I 2 ðVvg Þ ¼ I 2 ðVvg Þ. This result coincides, as expected, with the zero-temperature case of Equations 3.75 and 3.77. (c) Equations 3.85 and 3.86 provide some insight into the dependence of the nonradiative decay rate of a single vibronic state on the excess of electronic energy above the true electronic origin Es0 , hma vsa , or generally, X Ev ¼ hma vsa ð3:88Þ a
(if more than one mode is excited in the prepared initial state), which is converted into vibrational energy in the electronic state jli. Depending on the energy gap hV ¼ DE, the nonradiative decay probability can either increase or decrease with increasing excess electronic energy. Precisely speaking, the expressions ~I2 ðV vg Þ in Equation 3.85 describe the density of states weighted with the intramolecular hV. The distribution I2 , which in the statistical limit increases with increasing
3.4 Radiationless Decay Rates of Initially Selected Vibronic States in Polyatomic Molecules
series in Equation 3.86 must be summed over all resonance levels na and nm that give the appreciable contributions to the transition rate wsl . In spite of this, it is also important to consider the influence of the geometry change of the excited state relative to the ground state on the properties of the intramolecular distribution. We shall state this more precisely in Section 4.2, where numerical results for the IDs and g multidimensional IDs are presented. The coupling element Rsl decreases matrix simultaneously with the density of states, rl in the lnm manifold increases with the growing excess of electronic energy Ev. Detailed calculations of the relative nonradiative rates for benzene and perdeuterobenzene have been given by Heller et al. [114]. Using numerical estimates for the double optical progression 6m 1n , they found that the nonradiative decay rate wsl ðm1 ; m6 ; n1 ; n6 Þ increases moderately with the increasing vibrational excitation within the first excited singlet state of benzene ðC6 H6 and C6 D6 Þ for the S1 ! T1 ð1 B2u ! 3 B1u Þ nonradiative transition. This is in agreement with the increase observed experimentally [115–120]. The spectroscopic data for both the optical ðCCÞa1g mode a of benzene ðva ¼ v1 Þ and the nontotally symmetric bending mode ðv6 Þ used for the calculations, as well as the energy gap are v1 ¼ 923 cm1 ; v6 ¼ 521 cm1 ; hV ¼ 8200 cm1 ;
Dv1 ¼ vTa1 vSa1 ¼ 25 cm1 ; Dv6 ¼ 50 cm1 ;
X1 ¼ XCCðv1 Þ ¼ 0:025; X6 ¼ 0;
vg ¼ 1500 cm1 ;
with D2a ¼ 2Xa . The calculations have accordingly been performed in the parallel mode approximation (the effect of Duschinsky rotation on the vibrational overlap for benzene is small), taking proper account of the effect of geometry ðD1 Þ and frequency changes ðDv1 ; Dv6 Þ. For large effective energy gaps, the increase in rl dominates and the nonradiative decay rate increases with increasing Esm [122]. For extremely large energy gaps ðhV ffi 30; 000 cm1 Þ, the increase in rl leads to sizable alternations of the nonradiative decay rates that may exhibit an exponential dependence on the excess vibrational energy [121, 122].
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The principal subject of this chapter is the calculation of the intramolecular distribution (ID) [109]. The computational procedure utilizes the generating functions derived in the previous chapter. We begin in Section 4.1 with the derivation of expressions (in closed form) of the one-dimensional ID in the special (zero temperature) case w ¼ 0. Then, on this basis we discuss some important properties that we will formulate in terms of addition theorems. Likewise, we show in the next section how the analysis can again be generalized to deal with the finite temperature case ðw 6¼ 0Þ and derive a sequence of further intramolecular distributions. We conclude this section by listing the principal aims of the method described for the special case, where one of the parameters, for example, bm becomes unity. Finally, we treat more complicated case of mode mixing and show how the generating function technique can be used to calculate multidimensional intramolecular distributions (MID). We will see this idea exploited in some routines given in this chapter. They are realized in terms of recurrence equations. As an illustration of the practical utility of this calculation, we discuss mode mixing in an unusual distribution behavior. Our discussion of the symmetry or invariance properties of the MID in respect to the exchange of parameters may appear to be very long and circuitous to people familiar only with the customary hit and run treatment of transition processes given in many elementary quantum mechanics texts. Indeed, we shall find ultimately the standard results that are usually qualified by the assurance that they can be justified by the consideration of algebraic manipulation. Our aim is to provide such assurance.
4.1 The One-Dimensional Distribution I1(0, n; a, b)
The previous discussion will be concluded by considering the simpler case of the one-dimensional generating function, Equation 3.68, derived in Section 3.2.6. A convenient representation of the generating function (or GF), from which the
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distributions are obtained, is obtained by writing the latter as a product of two functions, which have many of the same structural features (see below) 2 3 1z 2 6ð1þbÞ a 1bz w 7 7 6 exp 6 7 5 4 zb að1zÞ 1 w exp 1bz 1bz G1 ðw;z;a;bÞ ¼ ð1b2 Þ1=2 1=2 : ½ð1bzÞ ð1þbzÞ1=2 zb zþb 1 w 1 w 1bz 1þbz ð4:1Þ Here z and w are generally complex variables in the bidisc D1(0,1) D1(0,1). b 1b In writing (4.1), we have set in Equation 3.68 D2 ¼ a and ¼ b; so that a 1þb 1þb and b are real parameters within the intervals a 0 and 1 < b < 1. The obvious interpretation of the parameter a and b is that they represent the linear and quadratic interaction terms of a vibrational mode that is active in transitions between an excited electronic state with excited vibrational levels of a lower electronic state. The subscript 1 of the function G1 , denotes the first-order or the one-dimensional case and is associated with the power of the denominator of G1 . The function (4.1) is regular in the bidisc and its infinite series representation is G1 ðw; z : a; bÞ ¼
1 X 1 X
I1 ðm; n : a; bÞw m zn :
ð4:2Þ
m¼0 n¼0
It will be shown that for each integral values m 0, I1 ðm; n; a; bÞ is an integer valued probability distribution of n and vice versa. Hence, I1 0 and the sum 1 X
I1 ðm; n; a; bÞ ¼ 1;
ð4:3Þ
n¼0
holding for each value of m ¼ 0; 1; 2; 3 . . . . To investigate this point more clearly, we shall first examine the special case w ¼ 0, before studying it at w 6¼ 0. Physically, this case corresponds to the limit of zero temperature, where only the lowest (vibrational) level m ¼ 0 of the initial electronic state is occupied. For this case, (4.1) together with (4.2) can be written as að1zÞ exp 1 X 1bz G1 ð0; z; a; bÞ ¼ ð1b2 Þ1=2 ¼ I1 ð0; n; a; bÞzn : ð4:4Þ 1=2 ½ð1bzÞ ð1 þ bzÞ n¼0 The function in the exponent of (4.4) constitutes a homographic transformation, which describes a mapping of the unit circle |z| ¼ 1 in a circle lying in the left z-half plane and that passes tangential to the point z ¼ 0. Therefore, G1 is regular over the unit circle D1 ð0; 1Þ and univalent if a=ð1 þ bÞ p. For larger values of a, the function G1 ð0; z : a; bÞ becomes polyvalent. In general the mapping has a fix point, which is 1 at z ¼ 1; G1 ð0; 1; a; bÞ ¼ 1 and where max jG1 ð0; z; a; bÞj ¼ G1 ð0; 1; a; bÞ ¼ 1. 1 z2D ð0;1Þ
4.1 The One-Dimensional Distribution I1(0, n; a, b)
We expand the exponential term in (4.4) in a power series of z over the unit circle D1 ð0; 1Þ 1 X að1zÞ að1bÞ exp ck zk ; ð4:5Þ ¼ exp ðaÞ exp z ¼ exp ðaÞ 1bz 1bz k¼0 where c0 ¼ 1
and ck ¼
k X 1 k1 i¼1
i!
i1
ai ð1bÞi bki ;
k 1:
ð4:6Þ
Representing the denominator of G1 (or strictly, its regular branch of positive function value at z ¼ 0) in terms of binomial series, we obtain by forming the Chauchy product of the two series after rearranging and collecting terms of an , ( n X 1=2 1=2 2 1=2 I1 ð0; n; a; bÞ ¼ ð1b Þ exp ðaÞ ð1Þn bn ð1Þi ni i i¼0 þ ð1Þn1 þ ð1Þn2 þ ð1Þn3
n a n1 X 3=2 1=2 b ð1Þi1 ni i1 1! i¼1
n a2 n2 X 1=2 5=2 ð1Þi2 b i2 ni 2! i¼2 n a3 n3 X 1=2 7=2 b ð1Þi3 i3 ni 3! i¼3
þ
n X an1 1=2 in þ 1 n þ 1=2 þ ð1Þ b ð1Þ in þ 1 ni ðn1Þ! i¼n1 ) an n1=2 1=2 ; ð4:7aÞ þ 0 0 n! 1
which satisfies the recurrence relation ðn þ 1Þ I1 ð0; n þ 1; a; bÞ ¼ ða þ nbÞ I1 ð0; n; a; bÞ þ b ð a þ nbÞ I1 ð0; n1; a; bÞ ðn1Þ b3 I1 ð0; n2; a; bÞ;
ð4:8Þ
where a ¼ a ð1bÞ has been set. Equation 4.8 represents a preferred method for calculating the values of I1 ð0; n; a; bÞ, starting from the initial value I1 ð0; 0; a; bÞ ¼ ð1b2 Þ1=2 exp ðaÞ. The term in curly brackets in (4.7a) is a square, so that I1 ð0; n : a; bÞ can be written as a square of a polynomial of degree n in a1=2 . Thus, we have
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" ½n=2 #2 1 X n! 2 1=2 r n=2r a I1 ð0; n; a; bÞ ¼ ð1b Þ exp ðaÞ : b n! r¼0 2r ðn2rÞ!r!
ð4:7bÞ
The right-hand series of (4.4) converges as z ! 1. Hence, by a simple substitution of z ¼ 1 it follows immediately from (4.4) that 1 X
I1 ð0; n; a; bÞ ¼ 1
ð4:9Þ
n¼0
as was claimed. The relation (4.9) of I1 ð0; n; a; bÞ can be also verified directly using (4.7a). 4.1.1 The Addition Theorem
If G1 ð0; z; a1 ; bÞ and G1 ð0; z; a2 ; bÞ are generating functions described by (4.4), the product G1 ð0; z; a1 ; bÞ G1 ð0; z; a2 ; bÞ ¼ G2 ð0; z; a1 þ a2 ; bÞ
is a generating function of the same kind, but of order (dimensionality) two. At the same time, as a consequence of (4.4), we also have ! ! 1 1 X X G2 ð0; z; a1 þ a2 ; bÞ ¼ I1 ð0; n1 ; a1 ; bÞzn1 I1 ð0; n2 ; a2 ; bÞzn2 n1 ¼0
¼
1 X
I2 ð0; n; a1 þ a2 ; bÞzn
n2 ¼0
ð4:10Þ
n¼0
Equating the coefficients of equal powers of z on both sides, we find the combined (joined) distribution of order two n X I2 ð0; n; a1 þ a2 ; bÞ ¼ I1 ð0; n1 ; a1 ; bÞ I1 ð0; nn1 ; a2 ; bÞ ð4:11Þ n1 ¼0
as a convolution of two probability distributions of dimensionality one. Equation 4.11 expresses the so-called addition theorem in respect to the parameter a. The twodimensional probability distribution on the left side of (4.11) can simply be written as a convolution of one-dimensional probability distributions, the a parameter of which is the sum a ¼ a1 þ a2 . It must be emphasized that the one-dimensional distributions in (4.11) have the same b parameter (for arguments). If we define að1zÞ exp 1 X 1bz Gi ð0; z; a; bÞ ¼ ð1b2 Þi=2 ¼ Ii ð0; n; a; bÞzn ; ð4:12Þ ½ð1bzÞ ð1 þ bzÞi=2 n¼0 where i is an arbitrary positive integer, the following addition theorem can be considered and similarly calculated:
4.2 The Distributions I1(m, n; a, b) n X
Ii ð0; n1 ; a1 ; bÞ Ij ð0; nn1 ; a2 ; bÞ ¼ Ii þ j ð0; n; a1 þ a2 ; bÞ:
ð4:13Þ
n1 ¼0
Because of the convolution form of (4.13), it is obvious that the sum of Ii þ j ð0; n; a; bÞ over n equals 1. As before, the distribution addition theorem (4.13) is obtained by setting a1 þ a2 ¼ a and by summing the orders i þ j to obtain the order of the convoluted distribution. 4.2 The Distributions I1(m, n; a, b) 4.2.1 Derivation of I1(m, n; a, b)
Having determined the probability distribution for m ¼ 0, I1 ð0; n; a; bÞ, we proceed to the general case m 6¼ 0. For this purpose, the w-dependent factor of (4.1) must be expanded in power of wm . This can be done by analogy to the expansion of G1 ð0; z; a; bÞ, taking into account the following assignment: z ! w; a ð1zÞ ; 1bz zb b! : 1bz a!
Hence
1b ! 1
ð4:14Þ
zb 1z ¼ ð1 þ bÞ : 1bz 1bz
ð4:15Þ
With these substitutions, the kernel of G1 ð0; z : a; bÞ can be brought to the form G1 ðw; z; a; bÞ 2 3 1z 2 6að1 þ bÞ 1bz w 7 a ð1bÞ 7 6 ð4:16Þ exp z ! exp 6 7; zb 5 4 1bz 1 w 1bz or after expansion in power series of z and w, respectively, as ! 1 n 1 X X X 1 n1 k nk k a ð1bÞ b zn ! 1 þ 1þ Am ðzÞw m ; k1 k! n¼1 m¼1 k¼1
ð4:17Þ
where 2k m X 1 m1 k zb mk k 1z a ð1 þ bÞ Am ðzÞ ¼ ; k! k1 1bz 1bz
m 1:
k¼1
ð4:18Þ
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Note that by the assignment (4.14), the parameter a becomes complex in the að1zÞ zb z-plane, but with Re 0, as it should be. Accordingly, 1 Re 1 1bz 1bz for jzj 1, similar to 1 < b < 1. Expanding the regular branch of
1=2 X 1 zþb ¼ Bn ðzÞ w n ; ð4:19Þ w 1 þ bz n¼0 zb 1 assume positive function values) in terms of (which for 1 Re 1 bz binomial series, where 1
zb w 1bz
Bn ðzÞ ¼ ð1Þn
1
n X zb k z þ b nk 1=2 1=2 nk
k
k¼0
1 þ bz
1bz
;
ð4:20Þ
by forming the Chauchy product of the two series above, we obtain 3 1z 2 6ð1 þ bÞa 1bz w 7 7 6 exp6 7 5 4 zb 1 w 1bz 1=2 ¼ zb zþb 1 w 1 w 1bz 1 þ bz 2
¼
1þ
1 X
! n
An ðzÞw Þ
n¼1
1 X m¼0
1 X
! Bn ðzÞw
n
n¼0
ðmÞ
C1 ðz; a; bÞw m ; jw j < 1;
ð4:21Þ
where ðmÞ
C1 ðz; a; bÞ ¼ Bm ðzÞ þ
m X
Ak ðzÞBmk ðzÞ:
ð4:22Þ
k¼1
After substitution of (4.18) and (4.20) in (4.22) and subsequent lengthy derivation, we have ðmÞ C1 ðz; a; bÞ
¼ ð1Þ
m
m X zb mi z þ b i 1=2 1=2 mi
i¼0
m1
þ ð1Þ
i
1bz
1 þ bz
m a 1z 2 X 1=2 3=2 i1 1! 1bz i¼1 mi
_
zb mi z þ b i1 1bz 1 þ bz
4.2 The Distributions I1(m, n; a, b)
m _2 a 1z 4 X zb mi z þ b i2 1=2 5=2 þ ð1Þm2 i2 2! 1bz i¼2 mi 1bz 1 þ bz þ ð1Þm3
_3
a 3!
m 1z 6 X zb mi z þ b i3 1=2 7=2 i3 1bz i¼3 mi 1bz 1 þ bz
þ m a 1z 2m2 X zb mi 1=2 m þ 1=2 þ ð1Þ im þ 1 mi 1bz ðm1Þ! 1bz i¼m1 1
_ m1
_m z þ b im þ 1 1z 2m m1=2 1=2 a þ : 0 0 m! 1bz 1 þ bz
ð4:23Þ
where _ a ¼ að1 þ bÞ. Substituting (4.4) and (4.21) in (4.1) and equating terms of w m in the two resulting series gives exp ð1b2 Þ1=2
að1zÞ 1bz
ð1b2 z2 Þ1=2
ðmÞ
C1 ðz; a; bÞ ¼
1 X
I1 ðm; n; a; bÞzn :
ð4:24Þ
n¼0
Using Leibnitzs formula for the nth derivative of a product, we obtain " # n X 1 d k ðmÞ I1 ðm; n; a; bÞ ¼ I1 ð0; nk; a; bÞ C1 ð0; a; bÞ ; k! dz k¼0
ð4:25Þ
in which (4.4) has been used. Note that (4.24) and (4.25) are valid for m ¼ 0, since ð0Þ C1 ðz; a; bÞ ¼ 1. The left-hand side of (4.24) can be regarded as a generating function of I1 ðm; n; a; bÞ for each integer m 0. Summing both sides of (4.25) over n gives ! 1 1 n X X X 1 d k ðmÞ I1 ðm; n; a; bÞ ¼ I1 ð0; nk; a; bÞ C1 ð0; a; bÞ k! dz n¼0 n¼0 k¼0 ! ! 1 1 X X 1 d n ðmÞ I1 ð0; n; a; bÞ C1 ð0; a; bÞ ¼ n! dz n¼0 n¼0 1 X 1 d n ðmÞ C1 ð0; a; bÞ; ð4:26Þ ¼ n! dz n¼0 where we have used the fact that I1 ð0; n; a; bÞ satisfies (4.9). On the other hand, after simply substituting z ¼ 1 in (4.23) and (4.24), the interpretation yields 1 X n¼0
ðmÞ
I1 ðm; n; a; bÞ ¼ C1 ð1; a; bÞ ¼ 1;
m0
ð4:27Þ
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In view of the formulas (4.26) and (4.27), it is natural to expect simple relations ðmÞ among the developing coefficients of C1 ðzÞ appearing in the sum (4.26). To ðmÞ demonstrate this, it suffices to note that the functions C1 ðzÞ appearing in (4.24) are linearly connected with coefficients dependent of z, that is, " 1z 2 1 zb 1 ðm þ 1Þ ðm þ 1Þ C1 ðzÞ ¼ _ a þ 2m þ þ mþ 1bz 2 1bz 2 " zþb 1z 2 z þ b ðmÞ _ C1 ðzÞ a 1 þ bz 1bz 1 þ bz
1 zb 2 1 zb þ 2m þ m 2 1bz 2 1bz zþb zb 2 ðm1Þ C1 ðzÞ þ ðm1Þ 1 þ bz 1bz
zþb ðm2Þ ðzÞ: C 1 þ bz 1
ð4:28Þ
This may be formulated more compactly as ðm þ 1Þ
ðm þ 1Þ C1
ðmÞ
ðmÞ
ðmÞ
ðm1Þ
ðzÞ ¼ a0 ðz; a; bÞ C1 ðzÞ þ a1 ðz; a; bÞ C1 ðmÞ
ðm2Þ
þ a2 ðz; bÞC1
ðzÞ:
ðzÞ ð4:29Þ ðmÞ
We assume here and throughout of the rest of this section that C1 ðzÞ ¼ The relation (4.29) provides a convenient starting point in the determination of the distributions I1 ðm:n; a; bÞ (see below). One can obtain not only the ðmÞ functions C1 ðzÞ and their derivatives in succession starting with the lowest, ð0Þ specifically C1 ðzÞ ¼ 1, but also the other quantities of interest from them. The ðmÞ essential formulas are found in Ref. [109] where the derivatives of ai ðzÞ (i ¼ 0, 1, 2) at z ¼ 0 are also given. ðmÞ C1 ðz; a; bÞ.
Corollary Comparing (4.7a) with (4.23), we have the relation ðnÞ
I1 ð0; n; a; bÞ ¼ ð1b2 Þ1=2 exp ðaÞC1 ð0; a; bÞ ¼ I1 ðn; 0; a; bÞ:
ð4:30Þ
It may be shown that the general symmetry property I1 ðm; n; a; bÞ ¼ I1 ðn; m; a; bÞ
ð4:31Þ
holds. This follows immediately from the symmetry property of G1 ðw; z; a; bÞ ¼ G1 ðz; w; a; bÞ.
4.2 The Distributions I1(m, n; a, b)
This is an important conclusion. It represents a precise statement of the related conjecture made following Equation 3.65. The meaning of Equation 4.31 is essentially that a transition in emission is equivalent to a transition in absorption when b ¼ 0. Otherwise, there exists no mirror image between transition in emission and absorption. 4.2.2 The Addition Theorem for I1(m, n; a, b)
For completeness, we use (4.1) and (4.2) to derive the addition theorem for I1 ðm; n; a; bÞ. In close analogy to the case (m ¼ 0), we have G1 ðw; z; a1 ; bÞ G1 ðw; z; a2 ; bÞ ¼ G2 ðw; z; a1 þ a2 ; bÞ
ð4:32Þ
and referring to (4.2), we see that 1 X 1 X
G2 ðw; z; a1 þ a2 ; bÞ ¼
! I1 ðm1 ; n1 ; a1 ; bÞ w m1 zn1
m1 ¼0 n1 ¼0 1 X 1 X
! m 2 n2
I1 ðm2 ; n2 ; a2 ; bÞ w z
m2 ¼0 n2 ¼0
¼
1 X 1 X I2 ðm; n; a1 þ a2 ; bÞ w m zn ;
ð4:33Þ
m¼0 n¼0
where X
X
I2 ðm; n; a1 þ a2 ; bÞ ¼
I1 ðm1 ; n1 ; a1 ; bÞ I1 ðm2 ; n2 ; a2 ; bÞ
ð4:34Þ
m1 þ m2 ¼m n1 þ n2 ¼n
is again the convolution I1 I1 . As before, the parameters a1 and a2 and the orders or dimensionalities of the distributions on the right side are summed to give the a parameter and order of the convoluted distribution. The successive application of (4.34) gives IN ¼ I1 I1 . . . I 1 :
ð4:35Þ
They have the norm 1 X n¼0
IN m; n;
N X k¼1
! ak ; b
¼
N þ m1 : m
ð4:36Þ
4.2.3 The Recurrence Formula
As already mentioned, the optimum strategy for most simply finding the values of I1 ð0; n; a; bÞ is given by applying the recurrence (4.8). The same pertains to the
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distribution I1 ðm; n; a; bÞ. The corresponding recurrence may be derived by using (4.25) and (4.28). Indeed, starting from the relation (4.29), we first determine the nth ðm þ 1Þ ðzÞ for z ¼ 0 as derivative of C1 n nk 2 n k X X d d d ðm þ 1Þ ðmÞ ðm þ 1Þ C1 ð0Þ=n! ¼ ai ð0Þ dz dz dz i¼0 k¼0 ! ðmiÞ
C1
ð0Þ=k!ðnkÞ!
ð4:37Þ
and substitute the result in (4.25). After collecting terms containing the same factor d k ðmÞ ai ð0Þ=k!, this yields dz d ðmÞ ðmÞ ðm þ 1Þ I1 ðm þ 1; nÞ ¼ a0 ð0Þ I1 ðm; nÞ þ a ð0Þ I1 ðm; n1Þ dz 0 1 d 2 ðmÞ þ a0 ð0Þ I1 ðm; n2Þ þ 2! dz þ
1 d n ðmÞ ðmÞ a0 ð0Þ I1 ðm; 0Þ þ a1 ð0Þ I1 ðm1; nÞ n! dz
þ
d ðmÞ 1 d 2 a1 ð0ÞI1 ðm1; n1Þ þ dz 2! dz ðmÞ
a1 ð0Þ I1 ðm1; n2Þ þ þ
1 d n ðmÞ a1 ð0Þ n! dz
d ðmÞ a ð0Þ dz 2
ðmÞ I1 ðm1; 0Þ þ a2 ð0Þ I1 ðm2; nÞ þ
I1 ðm2; n1Þ þ
þ þ
1 d 2 ðmÞ a2 ð0Þ I1 ðm2; n2Þ 2! dz
1 d n ðmÞ a2 ð0Þ I1 ðm2; 0Þ; n! dz
ð4:38Þ
d k ðmÞ ai ð0Þ=k!, dz ði ¼ 0; 1; 2Þ are given explicitly in Ref. [109]. Equation 4.38 enables us to determine I1 ðm; nÞ completely for all values m and n, provided that the values of I1 ð0; nÞ are already available.
where we have assumed I1 ðm; n; a; bÞ ¼ I1 ðm; nÞ. The coefficients
4.2 The Distributions I1(m, n; a, b)
4.2.4 Case b ¼ 0
When b ¼ 0; a special case of the formulas of the preceding section exists. In this case, the problem simplifies considerably, since an n!
I1 ð0; n; a; 0Þ ¼ exp ðaÞ
ð4:39Þ
reduces to the Poisson distribution of probability theory with mean a. In comparison with the latter, I1 ðm; n; a; bÞ gives skew line shapes, with a skewness to lower n or to higher n values, depending on whether b < 0 or b > 0 (see Figure 4.2). We can use the exact expression (4.23), but for b ¼ 0 ðmÞ
C1 ðz; a; 0Þ ¼ zm þ þ
m m
m 1
a ð1zÞ2 zm1 þ 1!
m 2
a2 ð1zÞ4 zm2 þ 2!
am ð1zÞ2m ; m!
ð4:40Þ
x þ k1 x for x > 0. ¼ ð1Þk k k Differentiating in respect to z and substituting z ¼ 0, we have
where use has been made of the fact that
1 d n ðmÞ 2 m a C1 ð0; a; 0Þ ¼ ð1Þnm þ 1 þð1Þnm þ 2 nm þ 1 1 1! n! dz
4 nm þ2
m a2 2m2 þ þð1Þn1 2 2! n1
m1 m a m m a 2m þ ð1Þn þ dmn ; m1 ðm1Þ! m m! n
n
ð4:41Þ
d ðmÞ C1 ð0; a;0Þ are given in dz Ref. [109] for several of the values of m in terms of polynomials of a. It may be where dmn is the Kronecker delta. The derivatives n!1
seen that the right side of Equation 4.41 is symmetrically distributed with respect ðmÞ to n ¼ m (where n denotes the nth derivative of C1 ðz;a:0Þ) and the sum over all derivatives for a given m equals 1, as Equation 4.26 clearly shows. Moreover, the ðmÞ number of the derivatives of C1 ðz; a;0Þ for each m is finite (see also Table 1 in Ref. [109]). Substitution of (4.39) and (4.41) into (4.25) leads after rearrangement to n! mn mn 2 I1 ðm; n; a;0Þ ¼ exp ðaÞ Ln ðaÞ ; a m!
ð4:42Þ
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where Lan ðaÞ ¼
n X Cða þ n þ 1Þ ðaÞl ; Cðaþ l þ 1Þ l!ðnlÞ! l¼0
a > 1
ð4:43Þ
is the Laguerre polynomial.1) In expression (4.42), it is assumed that m n. If n > m, simply exchange m and n. 4.2.5 Case b 6¼ 0
As with the result (4.42), an explicit representation of I1 ðm; n; a; bÞ is obtained for the general case b 6¼ 0. The result is by similar arguments leading to Equation 4.42 " ½m=2 ½n=2 m!n! X X ð1Þi bi þ r 2 1=2 I1 ðm; n; a; bÞ ¼ ð1b Þ exp ðaÞ m þ n ðm2iÞ!i!ðn2rÞ!r! 2 i¼0 r¼0 #2 mn2ðirÞ n2r mn2ðirÞ C Ln2r ðaÞ ; ðn2rÞ!A
ð4:44aÞ
where _ 1=2 ¼ ½2að1 þ bÞ1=2 ¼ ð2a Þ ; A
¼ ½2að1bÞ1=2 ¼ ð2 B aÞ1=2 ;
C ¼ 2½ð1bÞð1 þ bÞ1=2
ð4:45Þ
mn2ðirÞ Ln2r ðaÞ
and are again Laguerre polynomials. This is computationally useful formula. As before, in deriving expression (4.44a), it is assumed that m n and m2i n2r (there is a case in which one can have m2i < n2r for one or finitely limited values of i). In this case, replace the corresponding factor(s) on the right side of (4.44a) ð*Þ
mn2ðirÞ
ðn2rÞ!A
mn2ðirÞ
C n2r Ln2r
ðaÞ
by ðm2iÞ!B
nm2ðriÞ
nm2ðriÞ
Cm2i Lm2i
ðaÞ:
Analogously if m < n, 2 1=2
I1 ðm; n; a; bÞ ¼ ð1b Þ
m!n! exp ðaÞ m þ n 2
" ½m=2 ½n=2 XX i¼0 r¼0
ð1Þi bi þ r ðm2iÞ!i!ðn2rÞ!r! #2
nm2ðriÞ
ðm2iÞ!B
nm2ðriÞ Cm2i Lm2i ðaÞ
ð4:44bÞ
provided n2r m2i holds for all nonnegative integers i and r. Otherwise, perform an exchange of the appropriate factors appearing in (4.44b) according to R1 1) It is easily to verify from Equation 4.42 that I1 ðm; n; a 0Þda ¼ 1. 0
4.2 The Distributions I1(m, n; a, b)
( ), but in the reverse order. The terms within the square brackets in (4.44) are polynomials in a, the coefficients of which are polynomials of b. We have thus shown m is a square that each member of the sequence of I1 ðm; n; a; bÞ for different integers m!n! 1=2 of a polynomial multiplied by a positive factor ð1b2 Þ exp ðaÞ m þ n . As 2 mentioned earlier, the result (4.44)is a generalization of Equation 4.42, to which it reduces if we set b equal to zero. The properties (4.27) and (4.44) satisfy the requirements for a definition of I1 ðm; n; a; bÞ. 4.2.6 Numerical Results
Finally, we illustrate the role of the parameters a (or D2 ) and b (or b) on the distribution I1 ðm; n; a; bÞ in the following figures. We remark that I1 ðm; n; a; bÞ is an integer-valued function, but it is often convenient to have a representation of I1 ðm; n; a; bÞ transcribed to the form appropriate when n is continuous. This can be carried out by analytical continuation. Thus, the graphic presentation of I1 ðm; n; a; bÞ in such continuous form for preselected m levels and a large a parameter looks as shown in Figure 4.1. The curves are smooth functions of the variable n and exhibit m þ 1 peaks along the n-axis. This behavior is usual for the case of strongly coupled states, that is, those states with a large difference in their geometrical equilibrium positions a. The b (or b) dependence is very slight. The b parameter solely influences the skewness of the curves (see Figure 4.2). The situation for weakly coupled states, where the displacement parameter a is small, that is, a < 1, is quite different. If we plot I1 ðm; n; a; bÞ versus n, we find the result shown in Figure 4.3. The distribution I1 ðm; n; a; bÞ varies from a value of nearly one by a factor of 1010 or more, as n increases from zero to n ¼ 10 and the analytical continuation of I1 ðm; n; a; bÞ exhibits discontinuities (jumbs) at even integrals n. The surprise comes in Figure 4.4, which indicates that the effect of b (or b) on the distribution I1 ðm; n; a; bÞ is quite remarkable. The distribution I1 ð0; n; a; bÞ is relative to the Poisson distribution I1 ð0; n; a; 0Þ typically 10 000 times (ore more) greater, when the parameter a continuously drops. Moreover, the quotient between these distributions becomes greater still as the frequency parameter b ¼ vs =vl drops or deviates from unity to a slight extend. This of course should come as no surprise and may be seen in somewhat greater detail as follow. Since the a (or D) and b (or b) parameters are related to the linear and quadratic interaction terms of the accepting mode that is active in the electronic transition, this means that with a large linear interaction term the influence of the quadratic term is only slight. On the other hand, the latter frequency effect becomes very strong for weakly coupled states having a small a parameter. Considerable insight has been obtained into the properties of the IDs in Figures 4.5–4.8, where the multidimensional distribution Ii ðm; n; a; bÞ of i accepting modes is represented, respectively, for the cases of moderately strong-coupled states ! i X aj and weakly coupled states with a ¼ 0:3. The i vibrational having a ¼ 2 a ¼ j¼0
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Figure 4.1 The intramolecular distribution I1 ðm; n; a; bÞ as function of n for preselected levels m of the electronic excited state (strongly coupled states a ¼ 12; b ¼ 0:05).
modes belong either to an i-fold degenerate mode or to modes of different frequencies, but having the same frequency factor b ðbÞ. In the first case of i-fold degenerate mode, the norm, Equation from the fact that the degeneracy of the mth 4.36, results i þ m1 vibrational level is just . The enormous rise of the area under the curves m in Figures 4.7 and 4.8 is confirmed by the fact that the norm of the ID and hence the density of states increases with i. Thus, the multidimensional ID expresses the interplay of vibrational overlap and density of states. This, in turn, reflects the dependence of the multidimensionless ID on the density of (vibrational) states. This behavior is essential for our calculations; it simplifies the discussion about the irreversibility. The multidimensional distribution Ii ðm; n; a; bÞ for weakly coupled electronic states will also increase with deviating b from zero (or when b deviates from unity), but this effect (typically described by a power law) is quite overwhelmed by the more rapid increase in the density of states with increasing i.
4.3 Calculation of the Multidimensional Distribution
Figure 4.2 The intramolecular distribution for the lowest m levels ðm ¼ 0; 1; 2Þ and a value of a ¼ 12:5. When the parameter a is large, the b-dependence of I1 ðm; n; a; bÞ is weak.
4.3 Calculation of the Multidimensional Distribution 0 1 ð2Þ b1 b2 m1 ; m2 Dð1Þ 12 D12 A ; I2 @ n1 ; n2 Dð12Þ Dð12Þ b12 b21 1 2 4.3.1 Preliminary Consideration
The multidimensional distribution IN ðm; n; a; bÞ, which we described in the previous section, is appropriate for a set of separable modes nm , especially for components of a degenerate vibration. Here nm represents the set of choices of the occupation numbers n1 ; n2 ; . . . ; nN , (and correspondingly for the excited state), where each nm can assume all integer values between zero and n, and for which n1 þ n2 þ þ nN ¼ n. The individual nm can be treated as the occupation number of the mth
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Figure 4.3 Same as Figure 4.1, for weakly coupled states ða ¼ 0:15; b ¼ 0:025Þ.
separate vibrational mode. The characteristic behavior of such multidimensional distributions is that they arise via a convolution of one-dimensional distributions, each of which is associated with an individual vibrational mode. Quite often we are dealing with systems involving many mixed (nonseparable) vibrational components, with these components in a state vector characterized by a set of choices of n1 ; n2 ; . . . ; nN , where each nm can take all integral values 0. The formalism just outlined is applied to this case, where many ðNÞ vibrational modes of a molecule are not separable modes from each other in the sense that some or all of them are connected by a linear relationship, that is, by the Duschinsky rotation. The multidimensional distributions of this kind differ in an essential manner from those of separable vibrational modes. The latter are highly complex compared to those for separable modes. This results, as we have seen, from the increasing number of parameters appearing in the generating function and, as mentioned above, the parameters becoming dependent. Therefore, in this case, we cannot hope to obtain solutions in closed form for a large number of vibrational degrees of freedom as in the one-dimensional case and it is necessary to develop suitable methods. These can be formulated in terms of recurrence equations (there is one for each occupation
4.3 Calculation of the Multidimensional Distribution
Figure 4.4 The ratio I1 ð0; n; a; bÞ=I1 ð0; n; a; 0Þ (of the distribution (4.7b) to the Poisson distribution (4.39)) versus displacement parameter D at b ¼ 0:18; 0:11; 0:05 for a preselected levels n ¼ 10. Note the strong
dependence of I1 ð0; n; a; bÞ on the frequency 1b vl vs for weakly coupled change b ¼ ¼ l 1 þ b v þ vs b states, when the shift D or a ¼ D2 is small. 1þb
Figure 4.5 The multidimensional distribution Ii ð0; n; a; bÞ (in the parallel-mode approximation) for moderately strongly coupled states a ¼ 2; b ¼ 0:2 and different orders of degeneracy i.
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Figure 4.6 Same as Figure 4.5 for weakly coupled electronic states a ¼ 0:045 and b ¼ 0:025.
number nm and correspondingly mm ). This and the related problems will be discussed in the next section for the case of N ¼ 2 [123]. In the last section, the result of Section 4.3 will be extended to the case of N-vibrational components, where N is any integral value [123].
Figure 4.7 The multidimensional distribution Ii ð1; n; a; bÞ in the parallel-mode approximation for moderately strongly coupled electronic states a ¼ 2 and b ¼ 0:2. Note how the degeneracy i of the modes influences the distribution extensively.
4.3 Calculation of the Multidimensional Distribution
Figure 4.8 Same as Figure 4.7, for weakly coupled states a ¼ 0:045 and b ¼ 0:025. For even numbers n the analytical continuation of the ID has a discontinuity (jumb in Ii , as n crosses an even integer).
4.3.2 Derivation of Recurrence Equations
We begin by recalling the two-dimensional generating function of two nonseparable accepting modes given by Equations 3.31–3.37 namely, G2
ð1Þ ! ð2Þ D 12 D12 b1 b2 w1 ; w2 ; z1 ; z2 ; Dð12Þ Dð2Þ b12 b21 1 12
1=2 1=2
¼ 4b1 b2
Aðw1 ; w2 ; z1 ; z2 Þ exp B1 ðw1 ; w2 ; z1 ; z2 Þ ½B1 ðw1 ; w2 ; z1 ; z2 Þ B2 ðw1 ; w2 ; z1 ; z2 Þ1=2
;
ð4:45Þ
and consider a function of four complex variables w1 ; w2 ; z1 ; z2 and the eight real parameters written explicitly on the left side of Equation 4.45. Based on this equation and the following Equations 3.32–3.37 in Chapter 3, we try to obtain a solution of our problem in terms of recurrence equations. If we differentiate Equation 4.45 with
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respect to one of the four complex variables, for example, w1 , we obtain
qG2 qB1 qA q 2 2B1 B2 ¼ G2 2AB2 2B1 B2 B1 ðB1 B2 Þ : qw1 qw1 qw1 qw1
ð4:46Þ
We proceed with an expansion in powers of w1 w2 z1 z2 of the functions contained in Equation 4.46 and find (see Appendix B) 3 X
j
cij;kl w1i w2 zk1 zl2 ;
ð4:47Þ
2 X 3 X q ð1Þ j ðB1 B2 Þ ¼ gij;kl w1i w2 zk1 zl2 ; qw1 i¼0 j;k;l¼0
ð4:48Þ
B21 B2 ¼
i;j;k;l¼0
B1
and AB2
1 X 3 X qB1 qA ð1Þ j B1 B2 ¼ dij;kl w1i w2 zk1 zl2 : qw1 qw1 i¼0 j;k;l¼0
ð4:49Þ
Substituting Equation 4.47 through (4.49) and the expansion of the GF G2 (see Equation 3.43) into Equation 4.46 and equating terms of the same power in w1 w2 z1 z2 , we obtain the following equation: ( 3 3 X X m1 þ 1; m2 j m1 ; m2 j ð1Þ ð1Þ ð2doj;kl g0j;kl Þ I2 2ðm1 þ 1Þ c0j;kl I2 ¼ n1 k; n2 l n1 k; n2 l j;k;l¼0 j;k;l¼0 2m1 c1j;kl I2
m1 ; m2 j n1 k; n2 l
2ðm1 1Þc2j;kl I2
ð1Þ
ð1Þ
þ ð2d1j;kl g1j;kl Þ I2
m1 1; m2 j n1 k; n2 l
) m1 1; m2 j m1 2; m2 j ; 2ðm1 1Þc3j;kl I2 n1 k; n2 l n1 k; n2 l
ð4:50Þ
where in the last row, the identity g2j;kl ¼ 2c3j;kl has been used (see Appendix B). For simplicity of notation, we have set I2
m1 ;
m2
n1 ;
n2
! ¼ I2
! ð2Þ b1 b2 m1 ; m2 Dð1Þ 12 D12 : ; n1 ; n2 Dð12Þ Dð12Þ b12 b21 2 1
For computational convenience, we have arranged the term in Equation 4.50 by m1 þ 1; m02 , then those that contain collecting together all those that contain I2 n01 ; n02 0 m1 ; m 2 , and so on. Equation 4.50 constitutes a four-term recurrence relation I1 n01 ; n02 (in each of the quantum numbers m1 ; m2 ; n1 ; n2 ), that is, it allows one to express the m1 ; m2 0; m2 j arbitrary value I2 in terms of all preceding values I2 n1 ; n2 n1 k; n2 l
4.3 Calculation of the Multidimensional Distribution
where j; k; l ¼ 0; 1; 2, and 3. Therefore, in order to solve the problem fully, three additional recurrence equations are necessary. In particular, we need a recurrence equation that raises the number m2 to m2 þ 1. In order to derive the latter equation, we can proceed as we did previously with the exception that the GF (4.45), as well as its expansion, must be differentiated with respect to w2 . Alternatively, it is simpler to recall the invariance of I2 with respect to the interchange of modes discussed in Section 3.2.5 and the symmetry properties of the coefficients involved in Equation 4.50 (see Appendix B). In view of these symmetries, the desired recurrence equation can be obtained directly from Equation 4.50 as follows: i. Apply the operation F (flip) to both sides of Equation 4.50 taking consideration of the properties of the coefficients appearing in Equation 4.50 (see Appendix B); ii. Invoking the symmetry of I2 , reverse the order of the integer variables there and ð2Þ ð1Þ ð12Þ ð12Þ simultaneously change D12 to D12 ; D2 to D1 and b2 to b1 , and so on iii. Finally, replace m1 by m2 ; n1 by n2 ; i by j; k by l, and vice versa. Thus, ! ! ( 3 3 X X m1 i; m2 þ 1 m1 i; m2 ð2Þ ð2Þ ¼ ð2di0;kl gi0;kl ÞI2 2ðm2 þ 1Þ ci0;kl I2 n1 k; n2 l n1 k; n2 l i;k;l¼0 i;k;l¼0 ! ! m1 i; m2 m1 i; m2 1 ð2Þ ð2Þ 2m2 ci1;kl I2 þ ð2di1;kl gi1;kl ÞI2 n1 k; n2 l n1 k; n2 l ! m1 i; m2 1 2ðm2 1Þci2;kl I2 n1 k; n2 l !) m1 i; m2 2 ð4:51Þ 2ðm2 1Þci3;kl I2 n1 k; n2 l m 1 ; m2 Equations 4.50 and 4.51 allow us to determine I2 for all occupation n1 ; n2 0; 0 are already available. In numbers m1 ; m2 ; n1 ; n2 , provided the values of I2 n1 ; n2 this manner, we have reached the point in our procedure where only values of I2 for quantum numbers m1 ¼ m2 ¼ 0 remain to be calculated. Physically, such a situation is realized, for example, at low temperatures, where only the vibrationless level m1 ¼ m2 ¼ 0 of the initial electronic state is populated. In this limit, the GF (4.45) can be rewritten (by taking w1 ¼ w2 ¼ 0) in a more explicit manner (see Equation 3.42) d00;00 þ d00;10 z1 þ d00;01 z2 þ d00;11 z1 z2 exp a00;00 þ a00;10 z1 þ a00;01 z2 þ d00;11 z1 z2 ð0Þ 1=2 1=2 G2 ¼ 4b1 b2 h ð4:52Þ i1=2 : ða00;00 þ a00;11 z1 z2 Þ2 ða00;10 z1 þ a00;01 z2 Þ2 Consequently, Equation 3.43 reduces to ! ð2Þ X b1 b2 0; 0 Dð1Þ ð0Þ 12 D12 zn11 zn22 zm 1 ðm ¼ 1; 2Þ: G2 ¼ I2 ð12Þ ð12Þ ; b b n1 ; n 2 D D 12 21 n ;n ¼0 1
2
1
2
ð4:53Þ
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In Equation 4.53, we note the presence of dm1 m2 ;n1 n2 and am1 m2 ;n1 n2 coefficients for which the first two indices m1 and m2 are zero. This greatly simplifies the calculation effort, since the multiple sums that appear in the recurrence Equations 4.50 and 4.51 reduce to only one. Differentiating both sides of Equation 4.53 with respect to z1 , and proceeding as before, we obtain 3 3 n X X ð1Þ ð1Þ 2ðn1 þ 1Þ c00;0l I2 ðn1 þ 1; n2 lÞ ¼ ð2d00;0l g00;0l Þ I2 ðn1 ; n2 lÞ l¼0
l¼0
ð1Þ ð1Þ 2n1 c00;1l I2 ðn1 ; n2 lÞ þ ð2d00;1l g00;1l Þ I2 ðn1 1; n2 lÞ
o 2ðn1 1Þc00;2l I2 ðn1 1; n2 lÞ2ðn1 1Þc00;3l I2 ðn1 2; n2 lÞ ;
ð4:54Þ
where again for notational convenience, we have set ! ð2Þ b1 b2 0; 0 Dð1Þ 12 D12 : I2 ðn1 ; n2 Þ ¼ I2 ; n1 ; n2 Dð12Þ Dð12Þ b12 b21 1
2
The last recurrence equation that we need to complete our procedure can be obtained from Equation 4.54 by applying the operation F and invoking the symmetry of I2 in respect to the interchange n1 , n2 . This yields 2ðn2 þ 1Þ
3 3 n X X ð2Þ ð2Þ c00;k0 I2 ðn1 k; n2 þ 1Þ ¼ ð2d00;k0 g00;k0 Þ I2 ðn1 k; n2 Þ k¼0
k¼0
ð2Þ ð2Þ 2n2 c00;k1 I2 ðn1 k; n2 Þ þ 2d00;k1 g00;k1 I2 ðn1 k; n2 1Þ o 2ðn2 1Þ c00;k2 I2 ðn1 k; n2 1Þ2ðn2 1Þc00;k3 I2 ðn1 k; n2 2Þ :
ð4:55Þ
Equations 4.54 and 4.55 have the same analytic structure as the corresponding Equations 4.50 and 4.51. Both are four-term recurrence equations that express the arbitrary element I2 ðn1 ; n2 Þ in terms of I2 ðn1 k; n2 lÞ, where k; l ¼ 0; 1; 2; 3; k þ l > 0. Similarly, the coefficients contained in Equations 4.54 and 4.55 have their counterparts in Equations 4.50 and 4.51 (see Appendix B). 4.3.3 The Calculation Procedure
m1 ; m 2 As may be seen from the preceding section, the calculation of I2 n1 ; n2 0; 0 necessarily requires two steps. In the first step, we calculate I2 for all n1 ; n2 pairs ðn1 ; n2 Þ by successive use of Equations 4.54 and 4.55. Knowledge of 0; 0 I2 then permits us, by using the two remaining Equations 4.50 and 4.51 n1 ; n2 m1 ; m2 for all numbers m1 ; m2 ; n1 and n2 of in a second step, to obtain I2 n1 ; n2
4.3 Calculation of the Multidimensional Distribution
vibrational quanta. In detail, the procedure is as follows: We start with the initial value I2
0; 0 0; 0
! ¼ G2
ð1Þ ! ð2Þ 1=2 1=2 D 4b b d00;00 12 D12 b1 b2 ¼ 1 2 exp 0; 0; 0; 0 ; Dð12Þ Dð12Þ b12 b21 a00;00 a00;00 2 1
ð4:56Þ 0; 0 and calculate in the first step the sequence I2 , n1 ¼ 0; 1; 2; . . . by successive n1 ; 0 utilizations of Equation 4.54 n1 times. After the evaluation of these quantities, it is possible to progress from any ðn1 ; 0Þ to any finite ðn1 ; n2 Þ by n2 repeated utilization of Equation 4.55. Should one of the integer numbers n1 k or n2 l become negative, the corresponding values of I2 ðn1 k; n2 lÞ contained in Equation 4.54 or 4.55 are set to zero. After obtaining all values of I2 ðn1 ; n2 Þ, we are in position to raise the numbers m1 and m2 , employing Equations 4.50 and 4.51 (second step). Here, the procedure is precisely the same as that applied before: We calculate first the sequence m1 ; 0 I2 , m1 ¼ 1; 2; 3; . . . applying Equation 4.50 m1 times, and subsequently, n1 ; n2 taking these as our initial values, we repeat this procedure m2 times with the help of Equation 4.51.
4.3.3.1 Some Numerical Results With the aid of the recurrence procedure described in the previous section, the w ð12Þ dependence of I2 incorporated in the interactive displacement parameters D1 and ð12Þ D2 as well as in the cross-frequency parameters b12 and b21 has been investigated. Note that if w 6¼ 0, the two vibrational components are interdependent, which is manifested in an unusual behavior of the distribution I 2 . This is illustrated in m1 ; m2 Figure 4.9a–c, which represent relief plots of I2 over the plane ðn1 ; n2 Þ n1 ; n2 ð1Þ ð2Þ for various pairs ðm1 ; m2 Þ and moderately large parameters D12 ¼ D12 ¼ 4. In the patterns shown in Figure 4.9a for m1 ¼ 1; m2 ¼ 0, the distribution I2 is bell shaped ð1Þ ð2Þ and exhibits two maxima. One can verify that when the parameters D12 and D12 are sufficiently large, then the number of maxima increases as m1 þ m2 increases (see Figure 4.9b–c). Generally, m1 and m2 coincide with the number of valleys, which for w ¼ 0 run, respectively, perpendicularly to the n1 or the n2 axis. Furthermore, if the angle w changes, a renormalization among the modes occurs and the maximum (maxima) of I2 moves in the ðn1 ; n2 Þ plane, running, for special values of w, close to the n1 axis or close to the n2 axis. In these special cases (i.e., w ¼ 30 and w ¼ 120 in Figure 4.9), the distribution I2 becomes more complex and behaves as a onedimensional distribution with a remarkably complicated course. Finally, note that I2 is periodic in w with the period p. These effects on the spectroscopy will be discussed in chapter 7. ð1Þ ð2Þ ðmÞ When D12 and D12 are small ðD12 1Þ, I2 is not so simply described graphically, since I2 decreases nearly exponentially as the numbers n1 and n2 increase. In this case, the maximum of I2 lies in the vicinity of n1 ¼ m1 ; n2 ¼ m2 . As the angle w
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Figure 4.9 (a) Relief plot of ! ð2Þ b b m1 ; m2 Dð1Þ 12 D12 for m1 ¼ 1; I2 ; 1 2 ð12Þ n1 ; n2 D Dð12Þ b12 b21 1 2 m2 ¼ 0. The spectroscopic parameters are ð1Þ ð2Þ D12 ¼ D12 ¼ 4 and b1 ¼ 0:9; b2 ¼ 1:18;
b12 ¼ 0:53 and b21 ¼ 2:0. The values of the angle of rotation j are indicated in the figure. (b) Same as (a) but for m1 ¼ 0; m2 ¼ 1. (c) Same as (a) but for m1 ¼ 2; m2 ¼ 0. (d) Same as (a) but for m1 ¼ 0; m2 ¼ 2.
4.3 Calculation of the Multidimensional Distribution
Figure 4.9 (Continued ).
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varies, this maximum displaces, as before, toward the n1 axis, then from the n1 axis to the n2 axis, returning at w ¼ 180 to the initial position for w ¼ 0 .
4.4 General Case of N-Coupled Modes 4.4.1 The Generating Function GN
With this machinery in hand, we look at the general Nd problem, where N may be identified with some or all molecular modes. Since the molecule in the sth electronic state generally does not share the symmetries of the lth state, we must consider the largest subgroup common to both the s and l state conformations to classify the molecular normal modes. As we have already noted the mass-weighted normal coordinates of the l electronic state manifold and of an arbitrary secondary manifold s are linearly related ð1Þ s w11 w12 w1N q1 ql1 k12...N s l w21 w22 w2N q kð2Þ q2 2 12...N ¼ þ ð4:57Þ ; qs ql kðNÞ w N w w N N1
N2
NN
12...N
where W is a rotation matrix defined in Section 1.3. If the molecule has elements of symmetry, the matrix W will be block diagonal and Equation 4.57 decomposes into a set of several simultaneous equations for the irreducible representations of the point ðmÞ group under consideration. k12...N of Equation 4.57 is the component of a vector k12...N , which describes the difference of the equilibrium positions of the s and the l electronic states in a coordinate system with base vectors qlm . Of these components, only those that belong to the totally symmetric modes in the largest subgroup common to both the s and l state are nonzero. In the notation of Section 3.2.1, the multidimensional GF associated with the s ! l transition is given by Z Z GN ðtÞ ¼
1
1
Z Y N m¼1
N
N
rs ðqsm ; qsm ; wm Þrl ðqlm ; qlm ; zm Þdql dql ;
ð4:58Þ
where rs and rl are the trace functions defined by (3.17) (3.18). Here, wm and zm and are complex variables lying in the polydisc D2N ð0; 1Þ wm 1; zm 1; m ¼ 1; 2; . . . N . The overlap integral, Equation 4.58, may be evaluated according to the procedure used in Section 3.2. The only difference in the treatment in this section is that the generating function has a higher dimension and depends on the above 2N complex variables wm and zm ðm ¼ 1; 2; . . . NÞ. As before, to facilitate integration we define a new set of coordinates qm and q0m
4.4 General Case of N-Coupled Modes
qm ¼ 21=2 ðqlm þ qlm Þ; qm ¼ 21=2 ðqlm qlm Þ;
j83
ð4:59Þ
m ¼ 1; 2; . . . N
and correspondingly for the s state q0m ¼ 21=2 ðqsm þ qsm Þ; q0m ¼ 21=2 ðqsm qm Þ;
ð4:60Þ
m ¼ 1; 2; . . . N
Equations 4.59 and 4.60 guarantee that the transformation from qm to q0m and from qm to q0m are of the same form as the transformation (4.57) from qlm to qsm . The only distinction is that the displacement vector in this transformation is 21=2 k12 N and 0, respectively (see, for example, Equation 3.23). On substitution of Equations 4.59 and 4.60 into Equation 4.58 and considering the transformation between qm and q0m (and also between qm and q0m ) discussed above, we obtain 0 1 Z þ1 Z N ðbsm blm Þ1=2 1 BY C GN ¼ N @ h dq1 dq1 dq2 dq2 ...dqN dqN i1=2 A p 1 m¼1 ð1z2 Þð1w 2 Þ m m 8 N X X X > > l s s 2 s > w b þb ; w w b ; ; w w b w z w w > m 1 m1 m2 m m1 mN m m1 m 1 m m > > > m m m¼1 > > N > > X > X X < 1 s l s 2 s w w z w w w b ; w b þb ; ; w w b m2 m1 m m 2 m2 mN m m2 m m 2 m exp kq1 ;q2 ;...;qN k m m > m¼1 2 > > > > > N > > X X X > > s s s l 2 > w w b ; w w b ; w b þb w w w z > mN m1 m m mN m2 m m mN m m N N : m¼1 m m q1 q2 1 kq1 ;q2 ; qN k 2 qN N X X X 2 s 1 m þbs1 z1 1 1 wm1 bm w wm1 wm2 bsm w ; wm1 wmN bsm w 1 ; m ; m ; m¼1 m m X X X s 1 l 1 s 1 2 s 1 m ; m þb2 z2 ; ; m ; wm2 wm1 bm w wm2 bm w wm2 wmN bm w m m m X N X X s 1 s 1 s 1 l 1 2 m ; m ; ; m þbN zN ; wmN wm1 bm w wmN wm2 bm w wmN bm w m¼1
m
m
)
q1 q1 q2 q2 X X N N N X 2 ðmÞ ðmÞ m ;...; m bsm kðmÞ m ; 21=2 wm1 bsm k12N w wmN bsm k12N w 12N w m¼1 m¼1 m¼1 qN q N
ð4:61Þ
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1
2
N
where m ¼ w
1wm 1zm ; zm ¼ ; m ¼ 1;2;...;N: 1þwm 1þzm
ð4:62Þ
This result should be compared with Equation 3.24. It is a natural extension of the integral (3.24) to N dimensions. As before, it is a product of the two multiple Gaussian integrals, one over q1 ; q2 ; . . . ; qN and the other over q1 ; q2 ; . . . ; qN as variables, respectively. Each of these integrals can be evaluated explicitly by carrying out the integration using (cf. Equation 3.25) Z
1
1
Z
1 t 1 1 N=2 1=2 t exp q xq þ y q dq1 dq2 . . . dqN ¼ ð2pÞ ðdet xÞ exp yx y ; 2 2 ð4:63Þ
where q and y are N-dimensional column vectors and x stands for the N N matrix in Equation 4.61. Without repeating the details, we follow once the steps that led to Equation 3.31 and after a lot of algebra, we obtain n on o ði i2 ...ip Þ s l ; b GN w1 ;w2 ;...;wN ;z1 ;z2 ;...zN kj1 1j2 ...j ;b m m q A1 ðw1 ;w2 ;...;wN ;z1 ;z2 ;...;zN Þ exp N Y B1 ðw1 ;w2 ;...;wN ;z1 ;z2 ;...;zN Þ ¼ 2N ðbsm blm Þ1=2 ½B1 ðw1 ;w2 ;...;wN ;z1 ;z2 ;...;zN ÞB2 ðw1 ;w2 ;...;wN ;z1 ;z2 ;...;zN Þ1=2 m¼1 ð4:64Þ
where A1 ðw1 ;w2 ;...;wN ;z1 ;z2 ;...;zN Þ ¼
1 X
1 X
m1 ;m2 ;...;mN ¼0 n1 n2 ...nN ¼0
m
m
m
dm1 m2 ...mN ;n1 n2 ...nN w1 1 w2 2 ...wNN zn11 zn22 ...znNN ;
ð4:65Þ
B1 ðw1 ;w2 ;...;wN ;z1 ;z2 ;...;zN Þ ¼
1 X
1 X
m1 ;m2 ...;mN ¼0 n1 ;n2 ;...;nN ¼0
m
m
m
ð4:66Þ
m
m
m
ð4:67Þ
am1 m2 ...mN ;n1 n2 ...nN w1 1 w2 2 ...wNN zn11 zn22 ...znNN
B2 ðw1 ;w2 ;...;wN ;z1 ;z2 ;...;zN Þ ¼
1 X
1 X
m1 ;m2 ;...;mN ¼0 n1 ;n2 ;...;nN ¼0
bm1 m2 ...mN ;n1 n2 ...nN w1 1 w2 2 ...wNN zn11 zn22 ...znNN :
With this economical notation, it will be possible to discuss this type of problem in exactly the same manner as in the two-dimensional case. The coefficient dm1 m2 ...mN ;n1 n2 ...nN ; am1 m2 ...mN ;n1 n2 ...nN and bm1 m2 ...mN ;n1 n2 ...nN , which can be regarded as elements of matrices of order 2N are real and given by
4.4 General Case of N-Coupled Modes
dm1 m2 ...mN ;n1 n2 ...nN ¼
X
j85
ð12...NÞ2
1 jp N
ð1Þm1 þ m2 þ mN þ njp bs1 bs2 . . . bsN bljp kjp X
X
þ
ð1Þmi1 þ mi2 ...miN1 þ njp þ njq
1i1 hi2 ...iN1 N 1 jp h jq N ði i ...i
Þ2
bsi1 bsi2 . . . bsiN1 bljp bljq kip 1jq2 N1 X ði1 Þ2 þ þ ð1Þmi1 þ n1 þ n2 þ nN bsi1 bl1 bl2 . . . blN k12...N ; 1i1 N
ð4:68Þ
where i1 hi2 h. . . hir form a complete system of r indices as do j1 h j2 h. . . h js , both taken from among indices 1; 2; . . . ; N and where r þ s ¼ N þ 1. For convenience of ði i ...i Þ notation, we use here the dimensioned quantities kj1 1j22...jqp and bsm and blm instead ði1 i2 ...ip Þ of dimensionless Dj1 j2 ...jq and bm and bmn of the preceding section. In Section 8.1, it ði i2 ...ip Þ will often be convenient to justify our notation. For example, the parameters kj1 1j2 ...j q and those of the frequency factors bm and bmn can be normalized to dimensionless ði i ...i Þ ones in a condensed form. The interactive parameters kj1 1j22...jqp appearing in (4.68) are given by ! ! ! 23...N ð1Þ 13...N ð2Þ 12...N1 ðNÞ ð12...NÞ N þ1 k12...N W k12...N þð1Þ k12...N ; k1 ¼W W 23...N 23...N 23...N ! ! ! 23...N ð1Þ 13...N ð2Þ 12...N1 ðNÞ ð12...NÞ N þ2 k2 ¼W k12...N þW k12...N þð1Þ W k12...N ; 13...N 13...N 13...N .. . ð12...NÞ kN ¼ð1ÞN þ1 W
23...N
! ð1Þ k12...N þð1Þ2N W
12...N1
12...N1 12...N1
! ðNÞ
k12...N : ð4:69aÞ
ði i ...i Þ k121 2 N1 ¼W
i2 i3 ...iN1
!
34...N
þð1ÞN W ði i ...i Þ k131 2 N1 ¼W
þð1Þ
i1 i2 ...iN2
24...N W
ði
i1 i2 ...iN2
Þ
i1 i3 ...iN1 24...N
! ði
! ði Þ
2 k12...N
Þ
N1 ; k12...N
.. . ði1 i2 ...iN1 Þ ¼ðÞ1=2NðN1Þ W kN1;N
ði Þ
2 k12...N
N1 ; k12...N
ði1 Þ k12...N þW
24...N
!
34...N
!
34...N !
i2 i3 ...iN1
N þ1
i1 i3 ...iN1
ði1 Þ W k12...N
i2 i3 ...iN1 12...N2
! ði2 Þ þ ðÞ1=2NðN þ1Þ W k12...N
i1 i2 ...iN2 12...N2
! ði
Þ
N1 : k12...N
ð4:69bÞ
j 4 Calculational Methods for Intramolecular Distributions I , I , and I
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1
2
N
for all combinations of N1, indices 1i1 hi2 h...hiN1 N selected from among the indices 1;2;...;N and arranged in lexicographic order, and finally ði1 i2 Þ k12...N1 ¼W
i2 N
! ði1 Þ k12...N W
!
i2
ði i Þ
1 2 k1...N2;N ¼W
ði Þ
N1
.. . ði1 i2 Þ ¼ð1ÞN þ1 W k23...N
i2 1
i1
!
N
1 k12...N þW
ði Þ
2 k12...N ;
i1 N1
! ði1 Þ k12...N þð1ÞN W
! ði Þ
2 k12...N ;
i1 1
ð4:69cÞ
! ði Þ
2 k12...N ð1i1 hi2 NÞ:
i 1 i2 . . . i p are minors of order p of the N-dimensional orthogonal j1 j2 . . . j p i1 i 2 . . . i p refer to the rows and the subindices to matrix W. The upper indices of W j1 j2 . . . j i the column of the matrix W. As can be seen, the construction of the scheme (4.69) for ði i2 ...ip Þ due to mixing of components is simple. These the interactive parameters kj1 1j2 ...j q parameters are derivable from the components of the displacement vector k12...N in combination with minors of W of decreasing order. Moreover, as the order of the minors is decreased, the number of the components of k12...N on the right side of Equations 4.69 is successively diminished by 1. In the language of matrix theory [124], the coefficients in the system of (4.69a) are, apart from the sign , elements of the ðN1Þth compound matrix of W. Those of the system (4.69b) are elements of the ðN2Þth compound matrix and so on, until the first compounds matrix (Equation 4.69c) is achieved. Next, we observe that the upper and lower indices of Here, W
ði i ...i Þ
kj1 1j22...jqp in (4.69) have a close relationship with the indices of the minors i 1 i2 . . . i p W . Thus, the additional parameters on the left side of (4.69) are j 1 j 2 . . . jp uniquely determined by the properties of the matrix W and the vector k12...N. The N X N N , which evidently intotal number of these parameters is k Nk þ 1 k¼1 creases rapidly with the number of components N. From the viewpoint of the parallelmode approximation this is quite a surprising result, for we are describing the ðmÞ displacements of the normal modes m in terms of k12...N only. From the relation (4.69), it can also be inferred that a reversion of the vector k12...N ! k12...N leaves the ðmÞ by the GF (4.64) invariant, since all components k12...N , as well asthose generated i1 i 2 . . . ip effect of W enter the expression (4.68) as squares. Since W are minors j1 j2 . . . j p of an orthogonal matrix, relation (4.69a) can be written more compactly as kð12...NÞ ¼ W1 k12...N :
Equation 4.70 is a generalization of (3.30) to N dimensions.
ð4:70Þ
4.4 General Case of N-Coupled Modes
Similarly, we have m1 þ m2 þ þ mN
am1 m2 ...mN ;n1 n2 ...nN ¼ ð1Þ
X
þ
W X
12 . . . N 12 . . . N
þ
bs1 bs2 . . . bsN
ð1Þmi1 þ mi2 þ þ miN1 þ njp
1i1 hi2 h...hiN1 N 1 jp N
W
!2
i1 i2 . . . iN1 j1 . . . jp1 jp þ 1 . . . jN X X
!2 bsi1 bsi2 . . . bsiN1 bljp ð1Þm1 þ m2 þ mN2 þ njp þ njq
1i1 hi2 h...hiN2 N 1 jp h jq N
W
i1 i2 . . . iN2
!2
j1 . . . jp1 jp þ 1 . . . jq1 jq þ 1 . . . jN
bsi1 bsi2 . . . bsiN2 bljp bljq
þ þ ð1Þn1 þ n2 þ þ nN bl1 bl2 . . . blN ; ð4:71Þ
and finally bm1 m2 ...mN ;n1 n2 ...nN ¼ ð1Þm1 þ m2 þ mN þ n1 þ n2 þ þ nN am1 m2 . . .mN ;n1 n2 ...nN :
ð4:72Þ
4.4.2 Properties of dm ,n , am ,n , and bm ,n
Representing the expression (4.65) in a bilinear form, analogously to Equation (3.61), we have 2N A1 ðw1 ; w2 ; . . . ; wN ; z1 ; . . . ; zN Þ ¼ wt dm;n 1 z; ð4:73Þ where the first subscript m ¼ ðm1 ; m2 ; . . . ; mN Þ denotes the row and the second subscript n ¼ ðn1 ; n2 ; . . . ; nN Þ the column of the matrix element dm;n . It is convenient here to consider w and z as column symbols with the elements arranged in some definite, for example, lexicographic order 1 1 z 1 w1 : : : z N wN z z 1 2 w w 1 2 ; z ¼ : w¼ : : : wN1 wN zN1 zN w1 w2 w3 z 1 z2 z 3 : : : w1 w2 . . . wN z 1 z2 . . . zN
j87
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1
2
N
2N In this representation, the matrix dm;n 1 behaves like a magic square, since the sum of elements in each row and column and any main diagonal is the same, namely, zero 1 X n1 ;n2 ;...;nN ¼0
dm1 m2 ...mN ;n1 ;n2 ...nN ¼ 0;
ð4:74aÞ
for each row with the subscript m ¼ ðm1 ; m2 ; . . . mN Þ and 1 X m1;m2 ;...;mN ¼0
dm1 m2 ...mN ;n1 n2 ...nN ¼ 0;
ð4:74bÞ
for each column with the subscript n ¼ ðn1 ; n2 ; . . . nN Þ. The properties (4.74) follow directly from (4.68)and are 2N analogous to the relation (3.39). Note that the explicit matrix realization of dm;n 1 is effected by a matrix of 2N rows and columns; consequently, w and z have 2N components. Now, with the same treatment regarding the form 2N B1 ðw1 ; w2 ; . . . ; wN Þ ¼ wt am;n 1 z;
ð4:75Þ 2 N we establish some properties of the matrix am;n . Starting from the fundamental 1
formula (4.71), we have for the sum of the elements of the row with the subscript m ¼ ðm1; m2 ; . . . ; mN Þ 1 X n1 ;n2 ;...;nN ¼0
am1 m2 ...mN ;n1 n2 ...nN ¼ ð1Þm1 þ m2 þ m3 þ þ mN 2N bs1 bs2 . . . bsN
ð4:76aÞ
am1 m2 ...mN ;n1 n2 ...nN ¼ ð1Þn1 þ n2 þ ... þ nN 2N bl1 bl2 . . . blN ;
ð4:76bÞ
and analogously 1 X m1;m2 ;...;mN ¼0
for the sum of elements of the column with the subscript n ¼ ðn1 ; n2 ; . . . ; nN Þ. To complete the development thus far we attained, we write 2N B2 ðw1 ; w2 ; . . . ; wN Þ ¼ wt bm;n 1 z:
ð4:77Þ
On the basis of formulas (4.71) and (4.72), we find that 1 X n1 ;n2 ;...;nN ¼0
bm1 m2 ...mN ;n1 n2 ...nN ¼ ð1Þm1 þ m2 þ þ mN 2N bl1 bl2 . . . blN ;
ð4:78aÞ
where m ¼ ðm1 ; m2 ; . . . ; mN Þ denotes the subscript of the row being considered and 1 X m1 ;m2 ;...;mN ¼0
bm1 m2 ;...mN ;n1 n2 ...nN ¼ ð1Þn1 þ n2 þ þ nN 2N bs1 bs2 . . . bsN ;
where n ¼ ðn1 ; n2 ; . . . ; nN Þ; denotes the subscript of the selected column.
ð4:78bÞ
4.4 General Case of N-Coupled Modes
4.4.3 m1 ; m2 ; . . . ; mN The Distribution IN and its Properties n1 ; n2 ; . . . ; nN
The sum rules Before proceeding, we note that the generating function (4.64) is holomorphic in the polydisc D2N ð0; 1Þ and can be developed in following power series 1 X
GN ðw1 ; w2 ; . . . ; wN ; z1 ; z2 ; . . . ; zN Þ ¼ IN
m1 ; m2 ; . . . ; mN n1 ; n2 ; . . . ; nN
!
1 X
m1 ;m2 ;...;mN ¼0 n1 ;n2 ;...;nN ¼0
w1m1 w2m2 . . . wNmN zn11 zn22 . . . znNN
ð4:79Þ
where IN in (4.79) is, as will be shown, for each choice of integers ðm1 ; m2 ; . . . ; mN Þ, an N-dimensional probability distribution of n1 ; n2 ; . . . ; nN and vice versa. We will show that the distribution so obtained obeys conditions similar to those of (3.46) and (3.53) but generalized to 2N integer variables. Simultaneously, we show how the symmetry properties of the distribution, analogously to Equation 3.65 for N ¼ 2, can be extended to the general case of 2N arguments. In the rest of this section, m1 ; m2 ; . . . ; mN and n1 ; n2 ; . . . ; nN signify any integers 0. With the help of the expressions (4.73), (4.75) and (4.77), we can establish the following theorem. Theorem 4.1 For each choice of integers ðm1 ; m2 ; . . . ; mN Þ 1 X n1 ;n2 ;...nN ¼0
IN
m1 ; m2 ; . . . ; mN n1 ; n2 ; . . . ; nN
¼ 1:
ð4:80Þ
Proof The proof of this remarkable theorem offers no difficulty, since it closely follows the lines of the proof of the corresponding identity for N ¼ 2. By direct substitution in (4.73), (4.75), and (4.77) z1 ¼ z2 ¼ ¼ zN ¼ 1, we have, according to (4.74a), (4.76a), and (4.78a) A1 ðw1 ; w2 ;. . .; wN ; 1; 1;. . .; 1Þ¼ 0; B1 ðw1 ; w2 ; .. . ;wN ;1;1; .. . ;1Þ¼ 2N bs1 bs2 .. .bsN
1 X m1;m2 ;...;mN ¼0
m
m
m
m
m
m
ð1Þm1 þm2 þ þmN w1 1 w2 2 . .. wNN
¼ 2N bs1 bs2 .. .bsN ð1w1 Þð1w2 Þ . .. ð1wN Þ; and B2 ðw1 ; w2 ; .. . ;wN ;1;1; .. . ;1Þ ¼ 2N bl1 bl2 .. .blN
1 X m1 ;m2 ;...;mN ¼0
ð1Þm1 þ m2 þ þmN w1 1 w2 2 . . .wNN
¼ 2N bl1 bl2 .. .blN ð1w1 Þð1w2 Þ . .. ð1wN Þ:
ð4:81Þ
j89
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90
1
2
N
Substituting these expressions in (4.64), we obtain GN ðw1 ; w2 ; . . . ; wN ; 1; 1; . . . ; 1Þ ¼
N 1 Y X 1 w1m1 w2m2 . . . wNmN : ¼ 1w m m¼1 m1 ;m2 ;...;mN ¼0 ð4:82Þ
while, according to (4.79), 1 X
GN ðw1 ; w2 ; . . . ; wN ; 1; 1; . . . ; 1Þ ¼
1 X
IN
n1 ;n2 ;...;nN ¼0
m1 ;m2 ;...;mN ¼0
m1 ; m2 ; . . . ; mN
!
n 1 ; n 2 ; . . . ; nN
w1m1 w2m2 . . . wNmN ;
ð4:83Þ
which proves the theorem. Equation 4.80 appears as natural generalization of the corresponding Equation 3.46. 2N ð0; 1Þ wm 1; zm < 1; Regarding the function (4.64) in the polydisc D m ¼ 1; 2; . . . ; N, the same procedure as before enables us to prove the following supplementary Theorem 4.2 1 X m1 ;m2 ;...;mN ¼0
IN
m1 ; m2 ; . . . ; mN n1 ; n2 ; . . . ; nN
¼ 1;
ð4:84Þ
which is valid for each choice of integers ðn1 ; n2 ; . . . ; nN Þ. Proof The deduction is precisely like that of theorem 1. Based on (4.73), (4.75), and (4.77) and relations (4.74b), (4.76b), and (4.78b), we have after direct substitution of w1 ¼ w2 ¼ ¼ w N ¼ 1 A1 ð1; 1; . . . ; 1; z1 ; z2 ; . . . ; zN Þ ¼ 0 B1 ð1; 1; . . . ; 1; z1 ; z2 ; . . . ; zN Þ ¼ 2N bl1 bl2 . . . blN
1 X n1 ;n2 ;...;nN ¼0
ð1Þn1 þ n2 þ þ nN zn11 zn22 . . . znNN
¼ 2N bl1 bl2 . . . blN ð1z1 Þð1z2 Þ . . . ð1zN Þ; 1 X ð1Þn1 þ n2 þ þ nN zn11 zn22 . . . znNN B2 ð1; 1; . . . ; 1; z1 ; z2 ; . . . ; zN Þ ¼ 2N bs1 bs2 . . . bsN ¼
n1 ;n2 ;...;nN ¼0 s N s s 2 b1 b2 . . . bN ð1z1 Þð1z2 Þ . . . ð1zN Þ:
ð4:85Þ
Substituting these expressions in (4.64), we obtain N 1 Y X 1 GN ð1; 1; . . . ; 1; z1 ; z2 ; . . . ; zN Þ ¼ zn11 zn22 . . . znNN : ¼ 1zn n¼1 n1 ;n2 ;...;nN ¼0 ð4:86Þ
4.4 General Case of N-Coupled Modes
On the other hand, (4.79) gives GN ð1; 1; . . . ; 1; z1 ; z2 ; . . . ; zN Þ ¼
1 X n1 ;n2 ;...;nN ¼0
1 X
IN
m1 ;m2 ;...;mN ¼0
m1 ; m2 ; . . . ; mN
!!
n1 ; n2 ; . . . ; nN
zn11 zn22 . . . znNN ;
ð4:87Þ
which leads to (4.84). 4.4.3.1 Symmetry Property of IN
m1 ; m2 ; . . . ; mN n1 ; n2 ; . . . ; ; nN
In a manner similar to the treatment in Section 3.2.5, we investigate the invariance of IN under the exchange of parameters below bsm $ blm ;
m ¼ 1; 2; . . . ; N ð4:88Þ
and ð12...NÞ
k12...N $ k
:
First, we note that the replacement k12...N by kð12...NÞ requires, according to relation (4.70), that W ! W1 . Thus, starting with the vector kð12...NÞ and the inverse matrix W 1 instead of k12...N and W, we have the following lemma [109]: Lemma 4.1 If we replace the vector k12...N by kð12...N Þ and the orthogonal matrix W by its inverse W1 in Equations , the interactive displacement parameters convert into ði i ...i Þ kj1 1j22...jqp
!
ð j j2 ...jq Þ ki1 i12 ...i : p
1
i1 hi2 h. . . hip j1 h j2 h. . . h jq
! N
ð4:89Þ
In other words, the transformation (4.89) consists of exchanging the lower and ði i ...i Þ upper indices of kj1 1j22...jqp with each other. The proof of this lemma is provided in detail in Ref. [109]. The relation (4.89) can be transferred to the expression of the matrix elements dm;n , which, with the exchange of parameters (4.88) transforms into dn;m , or more precisely N N dm;n 2 ! dn;m 2 : 1 1
ð4:90aÞ
In the same manner, we find for the remaining coefficient matrices appearing in the GF N N am;n 2 ! an;m 2 1 1
ð4:90bÞ
2N 2N bm;n ! bn;m : 1 1
ð4:90cÞ
and
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92
1
2
N
Finally, if we simultaneously exchange the role of the dummy variables zm $ wm ; ðm ¼ 1; 2; . . . ; NÞ, as in the Section 3.2.5, we write zt dn;m w ¼ wt dm;n z ¼ A1 ðw1 ; w2 ; . . . ; wN ; z1 ; . . . ; zN Þ and similarly for the expressions B1 and B2 . This, of course, implies that GN ðw1 ; . . . ; wN ; z1 ; . . . ; zN
hn
ði i ...i Þ
2 p kj1 1j2 ...j q
o n oi ; bsm ; blm
n o n o ð j j2 ...jq Þ ; blm ; bsm ¼ GN z1 ; . . . ; zN ; w1 ; . . . ; wN ki1 i12 ...i p
ð4:91Þ
and after expanding both sides of (4.91) in power series in the polydisc D2N ð0; 1Þ and mN 1 m2 equating terms of w1m1 w2m2 . . . wNmN zm 1 z2 . . . zN , our conclusions are embodied in the following Theorem 4.3 The distribution IN is left invariant by the exchange of parameters (4.88), provided the integer variables mm and nm ðm ¼ 1; 2: . . . ; NÞ are simultaneously exchanged mm $ nm IN
n n on o on o m1 ;m2 ;...;mN ði1 i2 ...ip Þ n1 ;n2 ;...;nN ðj1 j2 ...jq Þ s l ¼ IN kj1 j2 ...jq ; bm ;bm ki1 i2 ...ip ; blm ;bsm : n1 ;n2 ;...;nN m1 ;m2 ;...;mN ð4:92Þ
Equation 4.92 appears as natural generalization of the corresponding Equation 3.65 to an arbitrarily number of vibrational modes. 4.4.4 A Special Case
We have derived all of the general properties of the multidimensional distributions that have been noted in Sections 3.2.4 and 3.2.5 (for the case N ¼ 2), except that of the special case N W ¼ dij 1 ;
ð4:93Þ
where dij is the Kronecker delta. In this case, all minors in the system of Equations 4.69 and 4.71 vanish, except those of the principal minors, which are 1. Hence, the system of Equations 4.69 simplifies considerably, since k12...N ¼ k12...N ð4:94Þ
and ði i ...i ...i Þ ki11j22...jqr p
¼
ðir Þ k12...N
4.4 General Case of N-Coupled Modes
if j1 ; j2 ; . . . ; jq completed by i1 ; i2 ; . . . ; ip form a complete sequence 1; 2; . . . ; N and where ir ¼ (rest of is), or ði i ;...ip Þ
2 kj1 1j2 ...j q
¼ 0;
otherwise:
From this, it follows that 2
ðmÞ N X bsm blm k12...N ð1wm Þð1zm Þ A1 ðw1 ; w2 ; . . . wN ; z1 ; . . . ; zN Þ ¼ s l B1 ðw1 ; w2 ; . . . ; wN ; z1 ; . . . ; zN Þ m¼1 bm ð1wm Þð1 þ zm Þ þ bm ð1 þ wm Þð1zm Þ
B1 ðw1 ; w2 ; . . . ; wN ; z1 ; . . . ; zN Þ ¼
N h Y m¼1
B2 ðw1 ; w2 ; . . . ; wN ; z1 ; . . . ; zN Þ ¼
N h Y m¼1
i
bsm ð1wm Þð1 þ zm Þ þ blm ð1 þ wm Þð1zm Þ
i
bsm ð1 þ wm Þð1zm Þ þ blm ð1wm Þð1 þ zm Þ
and lastly GN ðw1 ; w2 ; . . . ; wN ; z1 ; . . . ; zN Þ ¼
N Y
G1 ðwm ; zm Þ;
ð4:95Þ
m¼1
where G1 ðw:zÞ is again the one-dimensional GF considered in Sections 3.2 and 4.1. Thus, we have the following Theorem 4.4 If the matrix (4.93) is a unit matrix, the multidimensional GF GN factors into a simple product of N one-dimensional GF, each of which depends on variables and parameters of one vibrational component only. In addition, if the parameters bsm =blm ¼ bm for all components m are equal, the corresponding distribution IN generated by (4.95) coincides with formula (4.35). 4.4.5 Concluding Remarks and Examples
The explicit separation of vibrations in the multidimensional GF of Theorem 4.4 allows an effective reduction of the number of degrees of freedom and facilitates the calculation of transition rates. In this regard, it cannot be too strongly emphasized that the calculation of transition rates in the parallel-mode approximation has a fundamental inadequacy that is evident from the derivation above. The defect emerges, if we return to the case of N-vibrational modes some of which are not parallel to each other. This situation occurs if the latter have the same symmetry, especially if they are totally symmetric in the molecular group. In this case, the complexity introduced by the reciprocal (4.69a) and interactive displacement parameters (Equations 4.69b and 4.69c) is considerable and this fact cannot be overlooked in any parallel-mode estimate of the transition probability. Even with considerable effort, it is impossible to factor the exact GF into a product of one-dimensional GF.
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1
2
N
Note that the interactive displacement parameters are not quantities with physical significance. They merely represent the error incurred in making a crude approximation, assuming that all modes are parallel. Another remarkable feature of mode mixing is the dependence of the transition rate on the cross-frequency parameters (see Equation 4.71). (Note that in the parallel-mode approximation the transition rate depends solely upon km and bm ¼ vsm =vlm per mode). Both of these findings are manifested in the molecular spectra: (i) A striking energy narrowing or broadening of the absorption and fluorescence spectra does occur [123] and (ii) regularly structured emission bands (in form of single-mode progressions) occur only at special values of w, especially when the (orthogonal) matrix W is a unit matrix. Under all other conditions, vibrational components in the spectra are more or less scrambled and irregularly distributed. 4.4.6 Recurrence Relations
We raise the important question of finding the values of the MID. Based on our analysis pertaining to the one-and two-dimensional IDs, this problem will again be solved by constructing 2N four-term recurrence equations. There is one relation for each of the vibrational quantum numbers m1 ; m2 ; . . . ; mN ; n1 ; n2 ; . . ., nN contained in IN . Invoking the methods used above in Section 4.3.1, the recurrence equations are obtained by differentiating the GF (4.64) with respect to wi ði ¼ 1; 2; . . . ; NÞ and by substituting the series solution (4.79) for GN in this equation. Using the notation introduced in Section 4.3.2 and extending it to N dimension, we get 3 X
2ðmi þ1Þ
cm1 ...mi1 0miþ1 ...mN ;n1 ...nN IN
m1 ;...;mi1 ;miþ1 ;...;mN ¼0
...;mi þ1;...
!
...;ni ni ;...
n1 ;n2 ;...;nN ¼0 3 X
¼
(
ðiÞ ðiÞ 2dm1 ...mi1 0miþ1 ...mN ;n1 ...nN gm1 m2 ...mi1 0miþ1 ...mN ;n1 ...nN
m1 ;...;mi1 ;miþ1 ;...;mN ¼0 n1 ;n2 ;...;nN ¼0
2mi cm1 ...mi1 1miþ1 ...mN ;n1 ...nN IN ðiÞ
...;mi ;...
þð2dm1 ...mi1 1miþ1 ...mN n1 ...nN gm1 ...mi1 1miþ1 ...mN n1 ...nN ÞIN 2ðmi 1Þcm1 ...mi1 2miþ1 ...mN ;n1 ...nN IN 2ðmi 1Þcm1 ...mi1 3miþ1 ...mN ;n1 ...nN IN ði ¼ 1;2;...;NÞ;
IN
...;mi ;...
!
...;ni ni ;...
!
...;ni ni ;...
ðiÞ
...;mi 1;...
!
...;ni ni ;... ! ...;mi 1;...
...;ni ni ... !) ...;mi 2;... ; ...;ni ni ;... ð4:96Þ
j95
4.4 General Case of N-Coupled Modes
where IN
...;mi þr;...
!
...;ni ni ;...
¼ IN
m1 m1 ; ...; mi1 mi1 ; mi þr; miþ1 miþ1 ; ...; mN mN n1 n1 ; ... ...;
ni ni ; ...
!
...; nN nN
ðr ¼ 1;0;1;2Þ:
To obtain the second set of equations, we insert w1 ¼ w2 ¼ wN ¼ 0 into Equations 4.64 and 4.79 and m1 ¼ m2 ¼ mN ¼ 0 in the latter. We proceed in the above manner with the exception that the GF as well as its expansion must be differentiated with respect to zi . This gives ! 3 0:; . . . ; 0 X 2ðni þ 1Þ c0...0;n1 ...ni1 0ni þ 1 ...nN IN . . . ; ni þ 1; . . . n1 ;...;ni1 ;ni þ 1 ;...;nN ¼0 ( ! 3 0:; . . . ; 0 X ðiÞ ðiÞ ð2d0...0;n1 ...ni1 0ni þ 1 ...nN g0...0;n1 ...ni1 0ni þ 1 ...nN ÞIN ¼ ni n1 ;...;ni1 ;ni þ 1 ;...;nN ¼0 ! 0:; . . . ; 0 ðiÞ ðiÞ 2ni c0...0;n1 ...ni1 1ni þ 1 ...nN IN þ ð2d0...0;n1 ...ni1 1ni þ 1 ...nN g0...0;n1 ...ni1 1ni þ 1 ...nN Þ . . . ; ni ; . . . ! ! 0:; . . . ; 0 0; . . . ; 0 IN 2ðni 1Þc0...0;n1 ...ni1 2ni þ 1 ...nN IN . . . ; ni 1; . . . . . . ; ni 1; . . . !) 0; . . . ; 0 ; 2ðni 1Þc0...0;n1 ...ni1 3ni þ 1 ...nN IN . . . ; ni 2; . . . i ¼ 1; 2; . . . ; N:
ð4:97Þ
In both sets of equations, our notation suppresses the parametric dependence of IN on the spectroscopic parameters. The coefficients cm;n ; gm;n , and dm;n appearing in these equations are given in the Appendix C. Notice the upper indices on dm;n and gm;n in Equations 4.96 and 4.97. These are chosen deliberately to distinguish between different dm;n and gm;n in the system of recurrence (Equations 4.96 and 4.97). In order to complete the final step in the derivation, we insert w1 ¼ w2 ¼ wN ¼ 0 and z1 ¼ z2 ¼ zN ¼ 0 into Equation 4.79 and obtain n o n o 0; . . . ; 0 ði i2 ...ip Þ ; bsm ; blm ¼ GN 0; . . . ; 0; 0; . . . ; 0 kj1 1j2 ...j IN q 0; . . . ; 0 ; ð4:98Þ N Y d0...0;0...0 a0...0;0...0 ¼ 2N ðbsm blm Þ1=2 exp a0...0;0...0 m¼1 which is the starting point in our recurrence procedure. Equations 4.96 and 4.97 are four-term recurrenceequations and solving them is equivalent to the evaluation of m 1 ; m2 ; . . . ; m N IN for different values of the vibrational quantum numbers n1 ; n2 ; . . . ; nN m1 ; m2 ; . . . ; mN and n1 ; n2 ; . . . ; nN . This procedure offers a very convenient and efficient manner of calculating the MIDs. The calculation proceeds as already
:
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1
2
N
described in Section 4.3.2 forN ¼ 2 in two steps. In the first step, the numerical 0; 0; . . . ; 0 for all systems ðn1 ; n2 ; . . . ; nN Þ are calculated by values of IN n1 ; n2 ; . . . ; nN successive use of the N recurrence Equation 4.97: The ith equation employed to raise the quantum number ni. Taking these values as our initial values in Equation 4.96, we proceed in a similar manner as above and raise the numbers m1 ; m2 ; . . . ; mN , again by successive use of each of the Equation 4.96. 4.4.7 The Three-Dimensional Case
For illustrative purposes, we will present some results for the case N ¼ 3. In this case, we use the three Euler angles to describe the rotation matrix W in the (z,x,z) convention cos j cos ysin j cos q sin y sin j cos y þ cos j cos q sin y sin q sin y W¼ cos j sin ysin j cos q cos y sin j sin y þ cos j cos q cos y sin q cos y ; sin j sin q cos j sin q cos q
where 0 j 2p; 0 y 2p; 0 q p
and det W ¼ W
1 2 3 1 2 3
¼1
The influence of W is essentially attributable to the displacement parameters. According to Equations 4.69, there are a total of 15 parameters: Three direct ð1Þ ð2Þ ð3Þ geometrical displacements defined by the vector k123 ¼ col k123 ; k123 ; k123 , three reciprocal displacements specified in Equation 4.70 kð123Þ ¼ W1 k123 ; ð123Þ ð123Þ ð123Þ where kð123Þ ¼ col k1 ; k2 ; k3 , and nine further (interactive) displacements generated by the first compound matrix of W, Equation 4.69c: 2 ð1Þ 1 ð2Þ ð12Þ k123 W k123 k12 ¼ W 3 3 2 ð1Þ 1 ð2Þ ð12Þ k13 ¼ W k123 þ W k123 2 2 2 ð1Þ 1 ð2Þ ð12Þ k23 ¼ W k123 W k123 1 1 3 ð1Þ 1 ð3Þ ð13Þ k12 ¼ W k123 W k123 3 3
4.4 General Case of N-Coupled Modes ð13Þ
k13
ð13Þ
k23
ð23Þ
k12
ð23Þ
k13
ð23Þ
k23
3 ð1Þ 1 ð3Þ ¼ W k123 þ W k 2 2 123 3 ð1Þ 1 ð3Þ ¼ W k W k 1 123 1 123 3 ð2Þ 2 ð3Þ ¼ W k123 W k 3 3 123 3 ð2Þ 2 ð3Þ ¼ W k þW k : 2 123 2 123 3 ð2Þ 2 ð3Þ ¼ W k123 W k 1 1 123
Given values for all these displacements together with the frequencies factors bsm ¼ vsm =h and blm ¼ vlm =h ðm ¼ 1; 2; 3Þ (the latter, for instance, may be determined from spectroscopic data), the coefficients dm1 m2 m3 ;n1 n2 n and am1 m2 m3 ;n1 n2 n3 (see Equations 4.68 and 4.71) of the homogeneous functions A1 ðw1 ; w2 ; w3 ; z1 ; z2 ; z3 Þ and B1 ðw1 ; w2 ; w3 ; z1 ; z2 ; z3 Þ, respectively, can be calculated. This may be performed ðmÞ either in dimensioned quantities of k123 ; bsm ; and blm or in dimensionless quantities: i1 i2 ...ip ðmÞ D123 and aj1 j2 ...jq , normalized according to the procedure given in Section 8.1 (see Equations 8.14 and 8.15. The latter quantities are quite convenient because the numerical values have an order of magnitude of 1. Next, starting from dm;n and am;n , we obtain cm;n ; gm;n ; and dm;n via Equations C1–C8. With all of these coefficients and the initial value of I3 , Equation 4.98, the system of recurrence Equations 4.96 and 4.97 may be solved. 4.4.8 Some Numerical Results
We present results of such calculations to illustrate some of the effects of normalmode mixing. There are obviously a large number of possible examples and a few of them will be included here. The calculations are performed for m1 ¼ m2 ¼ m3 ¼ 0, that is, for the transition from the lowest vibrational level of the optically excited initial s state into the vibrational manifold of the lower electronic state (the zero-temperature limit). The results that we shall display are the final-state vibrational distribution (as given by the multidimensional surface of I3 ) and the relative nonradiative decay probability, both represented as functions of the normal coordinate rotation. Since the multidimensional surface of IN for dimensions N > 2 is hard to visualize, Figure 4.10 represents cross sections of I3 as functions of the lower-state occupation numbers n1 ; n2 at n3 ¼ 10. These cross sections are displayed for various values of the first Euler angle j in order to illustrate the influence of some mixed quadratic interaction terms of the excited-state force field on the vibrational distribution. In all of the examples presented in Figure 4.10, the geometry distortions along ð1Þ ð2Þ the first and second coordinates qs1 and qs2 ; k123 and k123 , have been chosen to be ð3Þ strong, whereas the remaining displacement k123 was moderately strong. In this figure, some of the effects of normal-mode mixing and of the interactions responsible
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Figure spatial variation of 4.10 Characteristic 0 0 0 with the Euler angle j I3 n1 n2 n3 depicted for a high sheet of I3 at n3 ¼ 10. The values of the Euler angle j are indicated in the figure. The remaining angles are constant and equal q ¼ y ¼ 30 . The dimensionless normal-
2
N
ð1Þ
ð2Þ
mode displacements are D123 ¼ D123 ¼ 4:0,
ð3Þ D123
¼ 1:0 and the normal-mode frequencies of the excited initial state s and the final states l are vs1 ¼ 200; vl1 ¼ 240; vs2 ¼ 400; vl2 ¼ 600; vs3 ¼ 900 and vl3 ¼ 800 cm1 .
for them become apparent. If the angle j varies (while keeping the remaining angles q and y constant), the coordinate system ðqs1 ; qs2 ; qs3 Þ rotates about the ql3 axis (or in general, about an axis that is parallel to the ql3 ). When the above rotation is carried out for any fixed value of the occupation number n3, the surface of I3 moves in the ðn1 ; n2 Þ
4.4 General Case of N-Coupled Modes
plane toward the n2 axis. This is demonstrated in Figure 4.10 for the highest cross section occurring (for any value of j) at n3 ¼ 10. As can be seen, for an angle of j ffi 30 the ID is distributed practically in the ðn2 ; n3 Þ plane (assuming in the remaining space spanned by the n1 ; n2 , and n3 axes approximate values of zero). If the angle j is further increased, the surface of I3 moves away from the n2 axis, running at approximately j ¼ 120 close to the n1 axis. Clearly, these special values of j are affected by the values of spectroscopic parameters. However, they are primarily ðmÞ dependent on the normal coordinate displacements k12...N ðm ¼ 1; 2; . . . ; NÞ. At l j ¼ p, that is, after a C2 ðq3 Þ rotation, the surface again reaches the initial position for j ¼ 0 . Therefore, the period of j is p. In this context, the three-dimensional and two-dimensional IDs behave similarly. The variation of I3 with q and y is more complicated and cannot be fully represented by one cross section as above. Another interesting feature of mode mixing, not shown in Figure 4.10, is the variation of the distribution along the n3 axis. Since the distortion along the third ð3Þ acceptor mode was chosen to be moderately strong, D123 ¼ 1, only low vibrational l levels of the q3 normal mode should be occupied (cf. Figure 4.3). However, from Figure 4.10, we conclude that this effect does not generally occur. The ql3 mode can be highly occupied if the coordinate axes are rotated due to mode mixing. Thus, the maximum decay in the examples illustrated in Figure 4.10 takes place at n3 ¼ 10. This unusual spread in the population of vibrational levels, which has no counterpart in the parallel-mode approximation ðj ¼ q ¼ y ¼ 0Þ,is attributed solely to mode mixing. As reported previously, due to normal coordinate rotation the direct ðmÞ displacements k12...N measured along the base vectors qlm are inadequate to describe ðmÞ spectral line broadening or narrowing. More suitable than the k12...N are the dm;n coefficients, which according to Equations 4.68 and 4.69 are complicated functions of ðmÞ the k12...N ; bsm ; blm ðm ¼ 1; 2; . . . ; NÞ and the coefficients of the rotation matrix W (or the Euler angles). Certainly, the dm;n coefficients may be large even though all ðmÞ k12...N ðm ¼ 1; 2; . . . ; NÞ are small. This behavior of the ID is directly related to experimental data such as optical spectra of polyatomic molecules or nonradiative decay rates. For example, the spectral line shape of a spectrum may be deduced by convoluting the ID with Lorentzian functions centered around Vvg n1 vl1 n2 vl2 n3 vl3 , where V corresponds to the energy gap between the two molecular (electronic) states and vlm are the vibrational frequencies of the final state. This point will be addressed in greater detail in Chapter 7. Here, we merely note that the effect shown in Figure 4.10 leads to a certain mode selection. If the angle j is equal to 30 , or lies within a certain range 0; 0; 0 ffi 0 for all occupation numbers n1 6¼ 0. The spectroaround 30 , I3 n1 ; n2 ; n3 scopic consequence is an increase in the intensities for the vibronically assisted (electronic) transitions involving the vl2 and vl3 vibrations at the expense of the vl1 vibration, the latter being completely eliminated. The same holds at j ¼ 120 with regard to the second vibration. Mode selection can also occur (in our case of three accepting modes) with the complete elimination of two modes and the dominance of the third remaining mode. Such situation arises if the molecular geometry change upon electronic excitation l ! s locates the initial-state coordinate axes ðqs1 ; qs2 ; qs3 Þ
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2
N
relative to the axes ðql1 ; ql2 ; ql3 Þ in a position as described by the displacement vector ðmÞ k123 (or D123 ) and the three Euler angle j; q; and y using the values given in the caption of Figure 4.11. It should be emphasized that such extreme cases occur at those values of j; q, and y which lie in certain finite interval, determined by the spectroscopic constants. In each of the three extreme cases depicted in Figure 4.11, the three-dimensional ID behaves one-dimensionally, being distributed along one of the n1 ; n2 , or n3 axes, respectively. This implies that instead of a level density typical of a polyatomic molecular system, a discrete level structure in the form of a single-mode progression can be resolved from the vibronically assisted molecular spectra. The net result is a proportionate increase in the intensity of these resolved levels with respect to those remaining. The line shape of such spectra or their envelopes are directly given by the IDs. The shape of the plots shown in Figure 4.11, although being functions of one quantum number nm only, are far more complicated than those expressed by one-dimensional IDs. The main difference is that in the latter the
Figure 4.11 Selective properties of I3 showing the reduction of the three-dimensional ID into one-dimensional IDs: (a) distributed along the n1 axis if j ¼ 60 ; q ¼ 30 and y ¼ 270 ; (b) distributed along the n2 axis if j ¼ 30 ;
q ¼ 30 and y ¼ 210 ; and (c) distributed along the n3 axis if j ¼ 30 ; q ¼ 60 and y ¼ 60 . The normal-mode displacements are ð1Þ ð2Þ ð3Þ D123 ¼ D123 ¼ D123 ¼ 3:0 and the vibrational frequencies are the same as in Figure 4.10.
4.4 General Case of N-Coupled Modes ðmÞ
number of progressional members is related to the electronic origin shift k123 upon the electronic excitation, whereas in the former it is governed by the dm;n coefficients ðmÞ which are complicated functions of the k123 and the Euler angles, as mentioned above. Therefore, single-mode progressions such as in Figure 4.11 are either very short (Figure 4.11a) or can be much longer (Figure 4.11b and c) than in the case of a onedimensional ID. These model examples reflect the spectroscopic implications of mode mixing and indicate that in practice special care must be exercised in the analysis of spectral line shapes. Fitting calculated to observed spectral intensities, although conceptually simple, can be difficult to perform, since for every particular molecular system one must find the appropriate coordinate transformation (4.57) between the normal coordinates of the states in question. This requires extensive input information on configurational and frequency changes for all molecular normal modes or the knowledge of the potential energy surfaces of both the states s and l [45]. Let us next investigate the role of normal-mode rotations on the nonradiative decay probability. To do this, one can ordinarily evaluate the quotient wnr ðj; q; yÞ=wnr ð0; 0; 0Þ, using Equation 3.75 together with Equation 3.77 for the nonradiative decay rate, but extended to N ¼ 3 accepting modes. Furthermore, we assume that the initial electronic state s is vibrationless, that is, has mm ¼ 0 quanta in all the normal modes. In this case, the sum in Equation 3.77 extends over all possible final states lnm i whose energies do not differ from the initial energy by more than c, Vvg n1 vl1 n2 vl2 n3 vl3 < c. For the width, we have assumed that ~ N is the largest common integer divider of all frequencies vm . ~ N , where v c v Such a situation is encountered in the nonradiative decay of (nearly degenerate) levels in a small molecule embedded in a medium. Under these circumstances the probability per unit time wnr is proportional to c1 [111] (see Equation 3.80) and the quotient wnr ðj; q; yÞ=wnr ð0; 0; 0Þ becomes independent of c. In the other limit ~ N , which is not considered here, the probability wnr is not dependent on c. This c v situation corresponds to the statistical limit. The results of such model calculations, some of which are portrayed in Figure 4.12, show a considerable change of wnr ðj; q; yÞ on increase of j; q, and y. The increase (decrease) of the transition probability due to rotation is a consequence of the increase (decrease) of the vibrational overlap when the overall shape of I3 moves in the space spanned by the occupation numbers n1 ; n2 and n3 . Note that the electronic coupling factor cancel in the expression wnr ðj; q; yÞ=wnr ð0; 0; 0Þ (if there is a single-promoting mode). Due to variation of the Euler angles the position of the maximum of I3 displaces in the direction of those occupation numbers nm having higher energy vibrations vm , thus leading to an increase of the nonradiative transition probability. On the contrary, if the peak in I3 moves toward an occupation number associated with a low-frequency vibration, wnr decreases. This is clearly seen from the curve for q ¼ y ¼ 0 , where the shift of the peak in I3 from the position ð0; 4; 0Þ to ð2; 0; 0Þ changes wnr by five orders of magnitude. Note that in this example vl2 > vl1 . The selectivity of I3 at different positions ðn1 ; n2 ; n3 Þ (see Figure 4.11) also comes into play here. A selection due to rotation of a progression in a high (or low)-frequency mode results almost always in an increase (decrease) of nonradiative transition probability. Such a selection
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Figure 4.12 Relative nonradiative decay probability as function of the rotational angles j; q, and y for a model molecule characterized ð1Þ by three accepting modes with D123 ¼ 2:0;
ð2Þ
2
N
ð3Þ
D123 ¼ 1:5; D123 ¼ 0:8 and a single-promoting mode. The effective energy gap V was taken to be 6000 cm1 and the normal-mode frequencies are the same as in Figure 4.10.
becomes apparent in the curve for q ¼ y ¼ 30 , where the third vibration with the highest frequency chosen is involved. The magnitude and type of the variation of wnr thus depend on the spectroscopic constants describing the effect of frequency distortion and potential surface displacement.
4.5 Displaced Potential Surfaces 4.5.1 The Strong Coupling Limit
In this section, we provide an alternative derivation of the nonradiative decay rate for a statistically large molecule under the simplifying assumption that the normal modes are parallel and their frequencies are the same in the two electronic states
4.5 Displaced Potential Surfaces
j103
under consideration, except for displacements in the origins of the normal coordiðmÞ nates k12...N in the two electronic states under consideration [125–127]. For this case, we can set vsm ¼ vlm or bm ¼ 1 ðbm ¼ 0Þ for all the normal modes m and the singlemode generating function (4.1) simplifies to " # D2m ð1wm Þð1zm Þ exp 2ð1wm zm Þ ðmÞ G1 ðwm ; zm ; am ; 0Þ ¼ : ð4:99Þ 1wm zm Taking into account Equation 4.99 becomes
zm ¼ eivm t
that
and
wm ¼ ebhvm ivm t ðb ¼ 1=kB TÞ,
(
) D2m ivm t ivm t G1 ðwm ; zm ; am ; 0Þ ¼ Zm exp nm e ð nm þ 1Þe coth ðb hvm =2Þ ; 2 ð4:100Þ
m ¼ ðebhvm 1Þ1 corresponds to the number of where Zm ¼ ð1ebhvm Þ1 and n excited vibrations with frequency vm at thermal equilibrium. We then see that (on using the above substitution for the variables wm and zm ) the generating function becomes temperature dependent. The multidimensional generating function for all N1 accepting modes is obtained as product of terms (4.100) ( ) N1 Y X D2m GN1 ðtÞ ¼ Zm exp ð4:101Þ coth ðb hvm =2Þ þ g ðtÞ þ g þ ðtÞ ; 2 m m¼1 where for convenience we have introduced the relation g þ ðtÞ ¼
1X 2 D ð nm þ 1Þeivm t ; 2 m m
ð4:102Þ
g ðtÞ ¼
1X 2 m eivm t : D n 2 m m
ð4:103Þ
Taking the explicit expression (3.75) for the single-promoting mode generating function, the expression for the nonradiative decay rate in the simple displaced potential surface model can be written as ( Z1 v g g 2 hwnr iT ¼ Rsl dt coth ðb hvg =2Þ þ 1 4h 1 " # 1X 2 exp itðVvg Þ D coth ðb hvm =2Þ þ g þ ðtÞ þ g ðtÞ 2 m m " #) Z1 X 1 hvg =2Þ1 dt exp itðV þ vg Þ D2 coth ðb hvm =2Þ þ g þ ðtÞ þ g ðtÞ þ cothðb 2 m m 1
ð4:104Þ
j 4 Calculational Methods for Intramolecular Distributions I , I , and I
104
1
2
N
Under conditions that will be given later, Equation 4.104 is essentially independent of the vibrational relaxation width c and therefore valid when c ¼ 0. Therefore, in writing Equation 4.104 we have made use of the integral representation of the d-function (3.78) to insure conservation of energy. As follows, we will treat Equation 4.101 in the strong coupling limit gð0Þ ¼ g þ ð0Þ þ g ð0Þ 1
ð4:105Þ
that is, the displacements Dm of the origins between the two electronic states considerably exceed the root mean square vibrational displacements ðh=vm Þ1=2 , for at least some vibrational modes. This strong coupling limit is generally found for spin-allowed transitions in transition metal ion systems and several organic molecules. The weak coupling limit, which is encountered when gð0Þ 1, behaves differently than the strong coupling limit, so that the relative displacement for each normal mode is small. When gð0Þ 1, the functions g þ ðtÞ and g ðtÞ in Equations 4.102 and 4.103 can be expanded in a power series of t around t ¼ 0 retaining only terms up to t2,2) 1 X 2 1 gðtÞ ¼ g þ ðtÞ þ g ðtÞ ¼ gð0Þ þ it D vm D2 t2 þ Oðt3 Þ; 2 m m 2
ð4:106Þ
where D2 ¼
1X 2 2 v D ð2 nm þ 1Þ; 2 m m m
ð4:107Þ
and gð0Þ ¼
1X 2 1X 2 Dm ð2 nm þ 1Þ ¼ D coth ðb hvm =2Þ: 2 m 2 m m
ð4:108Þ
1 m ¼ ehvm =kB T 1 The quantity n in Equations 4.107 and 4.108 is the thermal equilibrium vibrational occupation number. Introducing the so-called molecular rearrangement energy in the excited state, EM ¼
1X hvm D2m ; 2 m
ð4:109Þ
which corresponds half of the Stokes shift of the two electronic states under consideration, Equation 4.104 can be written as 2) If g þ ðtÞ þ g ðtÞ is large, the integrand in function (4.104) fall off roughly as exp ðgð0Þ hvi2 t2 =2Þ, so that at sufficient large time t, exp ðgð0Þ hvi2 t2 =2Þ is already small that the decay is for practical purposes completed before the truncated power expansion of g þ ðtÞ þ g ðtÞ becomes invalid.
4.5 Displaced Potential Surfaces
Z1 v 1 22 g g 2 hwnr iT ¼ coth ðb hv =2Þ þ 1 dt exp it ðVv ÞE = h t D R g g M sl 2 4 h 1
þ coth ðb hvg =2Þ1
Z1
dt exp it ðV þ vg ÞEM
= h
1
1 22 D t 2
: ð4:110Þ
Subsequent integration over t leads to the following result 2 pffiffiffiffiffiffi ( g 2 ) Rsl vg 2p hðVvg ÞEM hwnr iT ¼ cothðb hv =2Þ þ 1 exp g hD 4 2D2 h2 ( 2 ) hðV þ vg ÞEM ; ð4:111Þ þ cothðb hvg =2Þ1 exp 2D2 h2 which exhibits a Gaussian dependence on the energy parameter hðV vg ÞEM. Using a kind of coarse graining of the vibrational frequencies permits further simplification of Equation 4.111. Introducing an average frequency hvi, we can write (see Equation 4.107) h2 D 2
ffi h hvi EM coth ð hhvi=2kB T Þ 2EM kB T ;
where T is an effective temperature defined by [128] kB T ¼
1 h hvi coth hvg =2kB T : 2
ð4:112Þ
We next assume that the promoting-mode frequencies are small enough to be neglected in the exponents (4.111) and introduce an activation energy EA, given by the height of the point intersection of the two potential surfaces as measured from the bottom of the upper surface [125] E A ¼ ð hVEM Þ2 =4EM :
ð4:113Þ
The expression (4.111) for the decay rate assumes the form hwnr iT ¼
rffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi g 2 p R vg coth ð hvg =2kB TÞexp ðEA =kB T Þ; 4EM kB T sl
ð4:114Þ
At high temperatures, T coincides with the ambient temperature T, whereas at energy. In the lowlow temperatures kB T hhvi=2, the mean zero point motion temperature limit bhvg 1 and therefore coth b hvg =2 1. This permits us to rewrite Equation 4.111 in a form ( ) ffi v rffiffiffiffiffi ðVvg vs Þ2 2p g g 2 exp ; ð4:115Þ hwnr i ¼ Rsl 2h 2s2 s2
j105
j 4 Calculational Methods for Intramolecular Distributions I , I , and I
106
1
2
N
where vs ¼
1X 2 D vm ; 2 m m
ð4:116Þ
s2 ¼
1X 2 2 D v ; 2 m m m
ð4:117Þ
and
which is in agreement with the result of [129] as was derived previously by an alternative way, using in a formal sense lim
c
c ! 0 ðEa Ea0 Þ2
þ c2
¼ pd ðEa Ea0 Þ;
which has meaning when the quantity appears under an integral sign. A quite general feature of the result obtained in the displaced potential energy surfaces approximation is the relation between the nonradiative transition rate and the energy gap. If the energy gap hV is small, the exponential functions in Equation 4.115 are correspondingly large. As a rule of thumb, the less the energy gap, the larger the transition probability; conversely, the transition probability decreases exponentially as the energy gap is continuously increased. This results in the well-known exponential energy gap law that is common to several different types of multiphonon radiationless and vibrational relaxation processes. 4.5.2 The Weak Coupling Limit
The weak coupling limit is encountered as we have stated above, when
X m
D2m 1 or
EM hhvi. Thus, the relative displacement for each mode is small. This complicates the discussion of the correctness of our procedure. It merely confirms our earlier observation that if the displacement parameters are small, than the effect of the frequency distortion bm ¼ vsm =vlm on the values of the ID is appreciable. This conclusion can also be reached by a seemingly different argument recalling that the displacement parameters Dm refer to linear interaction terms (which produce a horizontal shift of the B–O potential energy surfaces), whereas the change of the vibrational frequencies bm refer to the quadratic interaction terms (the latter are derivable from the curvature of the potential energy surfaces). Thus, when Dm becomes large, the effect of bm is small and conversely, at small Dm along the qm coordinate, the effect of bm dominates.3) Therefore, there is no point in providing a derivation of the expression for the nonradiative decay rate in the weak coupling limit in the approximation of displaced potential surface model. Instead, in the weak coupling limit, the result of Section 4.3 is correct and must be used. 3) In fact, even if the linear coupling is weak, it is not correct to assume that the quadratic coupling is also weak.
4.6 The Contribution of Medium Modes
4.6 The Contribution of Medium Modes
Before leaving the subject of radiationless processes in an isolated molecule, we mention briefly the role of vibrational relaxation involved in the electronic relaxation process of a small molecule in a medium. To describe the influence of the medium, we shall use an approximate method involving the introduction of a so-called supermolecule [111] with a single intramolecular promoting mode and a single accepting mode and N intermolecular modes characterized by frequencies va and ðaÞ reduced displacements D12...N ; a ¼ 1:2; . . . ; N. We shall accept the experimental ðaÞ fact that the molecule medium coupling is weak and defined by the parameters D12...N and that the frequency vm considerably exceeds the medium frequencies va .4) The intramolecular modes are specified by the frequencies vg and vm , respectively, ðmÞ ðgÞ and the reduced displacement D1 and D1 ¼ 0. Treating the intermolecular vibrations analogously to the intramolecular vibrations, the physical situation is reminiscent of a statistical limit (whereupon the nonradiative decay rate is independent of the relaxation width c). Separating the intramolecular and the intermolecular contributions and using Equations 4.100–4.104 for moderately low temperatures bhv 1; coth ðbhv=2Þ 1, the transition probability takes the form wnr
" # v 1 ðmÞ2 1 X ðaÞ2 g g 2 ¼ Rsl exp D1 D 2 2 a 12...N 2h Z1 1
! 1 ðmÞ2 ivm t 1 X ðaÞ2 iva t dt exp itðVvg Þ exp D1 e D e exp : 2 2 a 12...N ð4:118Þ
Equation 4.118 can be expressed in terms of separate contributions of the intramolecular high-frequency mode and intermolecular low-frequency modes. Using the expansion exp
n X ðmÞ2 1 ðmÞ2 ivm t ðD1 =2Þ exp ðinvm tÞ; ¼ D1 e 2 n! n
ð4:119Þ
Equation 4.118 can be reformulated as ðmÞ2 n o v X 1 ðmÞ2 ðD1 =2Þn ~ g g 2 ðaÞ wnr ¼ Rsl exp D1 GN Vvg nvm ; D12...N ; 2 2h n! n ð4:120Þ 4) To pursue this matter a little further, we remark that we may define a model Hamiltonian X for ðaÞ vibrational relaxation of the molecule in a dense medium in the form Hm ¼ Cqm exp D12...N qa a [130].
j107
j 4 Calculational Methods for Intramolecular Distributions I , I , and I
108
1
2
N
where
~ N Vvg nvm ; G Z1 1
n
ðaÞ D12...N
o
1 X ðaÞ2 ¼ exp D 2 a 12...N
!
1 X ðaÞ2 iva t dt exp itðVvg nvm Þ exp D e 2 a 12...N
! ð4:121Þ
plays the role of the medium line shape function. Its appearance here does not, of course, violate energy conservation since the energy gap hV is bridged by intramolecular vibrations and as will be shown below by medium induced Stokes shift. Proceeding as in Section 4.5, expression (4.121) can be simplified further in the limit of strong coupling to the medium modes (phonons) X ðaÞ2 ðD12...N =2Þ 1 ð4:122Þ a
writing ( 2 ) n o 2p 1=2 ðVvg nvm ÞEM = h ðaÞ ~ ¼ ; exp GN Vvg nvm ; D12...N D2M 2D2M ð4:123Þ
where D2M ¼
1 X 2 ðaÞ2 v D ; 2 a a 12...N
ð4:124Þ
is responsible for the medium broadening, while EM ¼
1X ðaÞ2 hva D12...N ; 2 a
ð4:125Þ
is responsible for the Stokes shift due to the medium modes. We substitute Equation 4.121 into Equation 4.118 to obtain
n DðmÞ2 =2 p 1=2 v X 2 1 1 ðmÞ g Rg 2 wnr ¼ exp D1 sl hDM n! 2 2 n " # ðVvg nvm EM = hÞ2 : exp 2 2DM
ð4:126Þ
Equation 4.126 describes the nonradiative decay of a small molecule strongly coupled to the medium in terms of a superposition of an intramolecular (Poisson) distribution and Gaussian. The summation over the occupation numbers n of the intramolecular accepting mode in the final electronic state is implied in Equation 6.126. The contribution of the medium modes in terms of the parameters ðmÞ2 EM and DM is contained in the Gaussian distribution. For D1 =2 1, it may happen
4.6 The Contribution of Medium Modes
that the largest contribution to this decay rate will occur from low-lying off-resonance levels in the final manifold, which contribute via the tails of the distributions. The methods we have described for studying electronic relaxation and decay of electronic states may be applied to a variety of problems. These include, for example, the study of vibrational relaxations (VR) which will be illustrated with a simple application to the decay of an initially prepared harmonic molecular oscillator state Q Q ji >¼ j1; a na > of a macroscopic system to the final state jf >¼ j0; a n0a >. The system is supposed to contain a guest, represented by a harmonic molecular oscillator of frequency v, coupled to a very large number of medium (phonon) states jfna g > of considerable lower frequencies va . Then, for the VR rate wvr , we have [130] XXY 2p h wvr ¼ hvÞ Za1 expðb hna va Þ ½1 expðb h 2v 0 fn g fn g a a
a
Y Y 2 X 0 0 n jFðfq gÞj n d ðn n Þ hv hv a a a a a a a
a
a
ð4:127Þ
where the coupling of the guest molecule to the medium phonons is given by the Hamiltonian
X Hm ¼ Cq exp a Da ðva = hÞ1=2 qa ¼ q Fðfqa gÞ; ð4:128Þ P
which involves the Debye-Waller factor exp a Da ðva =hÞ1=2 qa due to the thermal vibrations of the medium modes about the equilibrium positions. In one of the case of greatest physical interest, the coupling varies linearly with the normal coordinate of the molecular oscillator q. We might calculate wvr directly. It is simpler, however, to evaluate it using the generating function technique of Chapter 3. By following the same steps that led to representation (4.99) one can represent the generating function of eq. (4.127) in the form XX exp½na ðit va þ b hva Þ expðitn0a va Þ fna g fn0a g
Y X Y 2 na exp Da ðva = hÞ1=2 qa n0a a
a
a
Y 1X 2 ¼ Ga1 wa ; za ; Da ; 0 2 a a
ð4:129aÞ
where h 2 i ð1þwa Þð1þza Þ exp D a 2ð1wa za Þ 1 2 Ga1 wa ; za ; Da ; 0 ¼ 1wa za 2 1 2 ¼ Za exp Da ð2na þ 1Þ þ gþa ðtÞ þ ga ðtÞ : 2
ð4:129bÞ
j109
j 4 Calculational Methods for Intramolecular Distributions I , I , and I
110
1
2
N
Eq. (4.129b) has the form of the expression (4.99) for the generating functions for electronic relaxation between two vertically displaced potential surfaces, except with wm 2 replaced by wa, zm by za and D2m by Da and exhibits the same t dependence as the 2 latter. We emphasize, however, that the effect of replacing the D2m by Da changes the temperature dependence of wvr manifested through na dramatically in comparison to the expected for electronic relaxation processes [130]. Now, expression (4.129a) is expanded in terms of the associated MID for different vibrational occupation numbers n1 ; n2 ; . . . ; nN ; n01 ; n02 ; . . . ; n0N according to (4.79). This may be substituted into eq. (4.127), to give an expression for the rate constant wvr which has the form of a Fourier integral Z1 wvr ¼ D 1 Z1
¼D
Y X dt exp ivt a ca jtj Ga ðtÞ a 1
X X dt exp it v þ ðna va n0a va Þ ca jtj a
1
XX
X 0 0 0 ð1Þn1 þn2 ...þnN þn1 þn2 þ...þnN exp b h na va
fna g fn0a g
Y
a
1 2 0 I n ; n ; D ; 0 1 a a a 2 a
a
ð4:130Þ
Q where D ¼ ð2hvÞ1 C 2 ½1 expðbhvÞ a Za1 . In obtaining this result we have taken proper account of the conservation of energy P P manifested through the delta function dðv þ a na va a n0a va Þ. If we wish the rate at which phonons are emitted into frequency range of the lattice including resonance and local impurity modes, we adopt the validity of the limit of fast P vibrational relaxation, defined in terms of the relation a ca t 1 with t being the time scale. The method
of carrying out the calculation of (4.130) and the MID Q 1 2 0 I n ; n ; D ; 0 has been described before quite explicitly. a a a 1 2 a
j111
5 The Nuclear Coordinate Dependence of Matrix Elements With the conclusion of Chapter 4 we have completed our formal development of electronic relaxation processes in polyatomic molecules and the remaining portion of the book will be largely devoted to applying the results thus far obtained to special situations. We will also consider the nuclear coordinate dependence of electronic matrix elements that occurs in the rate expression for the nonradiative transitions. Besides, topics such as radiative decaying states, excitation energy transfer in molecular crystals, and other applications will also be taken up subsequently. Section 5.1 deals with the nuclear dependence of the electronic matrix elements for radiationless transitions by the use of a q-centroid approximation. The latter is obtained as an average in which the density of states is weighted by means of vibrational overlap factor using the ID procedure developed in earlier chapters. Such studies considerably enhance the understanding and accuracy of transition probability calculation and also underscore previous warnings as to the enormous errors incurred by using the Condon approximation for the nuclear coordinate-dependent energy denominators that appear in the electronic matrix elements.
5.1 The q-Centroid Approximation
As remarked in Chapter 3, simply formulating the non-Born–Oppenheimer (BO) coupling element Vsm;ln ¼ ðhjs ðr; qÞxsm ðqÞjH 0 BO jjl ðr; q Þxln ðq ÞiÞ i 1 2 P h ¼ h2 js xsm qjl =qqg qxln =qqg þ xsm js q =qq2g jl xln 2 g ð5:1Þ
as a product of an electronic transition matrix element and a density of states weighted vibrational overlap factor results in an enormous simplification of the actual problem of calculating nonradiative transitions between the electronic states s and l: In this chapter, we shall specify the nuclear configuration q0 at which the integration
j 5 The Nuclear Coordinate Dependence of Matrix Elements
112
over the electronic coordinates r of the integral in (5.1) is evaluated. From this, it consequently follows that the matrix element (5.1) for calculation of the thermally averaged internal conversion rates is written as a product of electronic factor and vibrational factor. As one should expect from the terminology, the earliest application of the q-centroid, strictly speaking, the r-centroid method was made in diatomic spectroscopy [131], although in a completely different physical sense. The q-centroid approximation presents a nontrivial generalization of the r-centroid approach of diatomic spectroscopy to the case of the nonradiative decay of polyatomic molecules. The importance of studying the q-dependence of the nonadiabatic coupling element was emphasized by Freed and Gelbart [132] and Freed and Lin [27]. The customary approach to (5.1) involves the expansion of the electronic wavefunctions appearing in (5.1) in a Taylor series about some reference configuration q0 [133, 134]. Often this reference configuration is chosen as the equilibrium configuration qe of either the ground electronic state or the excited electronic state. This is the approach that is almost universally used in the case of radiation transitions and corresponds to using the crude BO wavefunctions. In the case of nonradiative transitions when using adiabatic electronic wavefunctions, considerable errors are incurred, which are incorrect by orders of magnitude if the usual Condon approximation is invoked [136, 137]. On the other hand, the choice of q0 is purely ad hoc, since nothing has singled out q0 as natural, so there is no unique choice of q0 . If, for instance, terms in all orders in the Taylor expansion of the electronic wavefunction about q0 are retained, then any reasonable choice of q0 , which makes the series converge, is adequate. However, this is not necessarily true if only some leading terms in the expansion are retained. Thus, it is necessary to find an optimal q0 to ensure the best rapid convergence of the expansion. In Section 3.3, we saw that the energy conservation imposes a stringent selection rule on nonradiative transition. However, the energy conservation is often quite unfavorable with the vibrational overlap factor and this favors a q-centroid, which may considerably differ from that of the equilibrium position of either of the two electronic states. Therefore, Freed and Lin have shown that the proper treatment of this problem is obtained from a thermally averaged decay rate with density of states weighted vibrational overlap factor. This average is not restricted to geometries near the equilibrium positions of the electronic states under consideration [27]. The basic idea of the q-centroid approach rests on the following assumption. The vibrational overlap factor, as we saw in Chapter 4, is a sharply peaked function of nuclear coordinates, while the electronic matrix element (apart from particular instances) is often a slowly varying function of q. Thus, we assume that it is reasonable to expand the electronic matrix element about a point in the vicinity of the peak of the vibrational overlap factor. An optimal expansion point is chosen to guarantee the most rapid convergence of series expansion or as that that makes the leading correction term for the thermally averaged nonradiative decay rate vanish. This point is called the q-centroid and corresponds to a nuclear configuration very often of lower symmetry than the equilibrium configuration.
5.1 The q-Centroid Approximation
In this chapter, we shall extend the description given in Ref. [27]. This will include the effect of Duschinsky mixing for some (totally symmetric) modes. We shall also give an extensive discussion of the dependence of the electronic matrix element on the nuclear coordinates. In this section, we will justify the use of such favored nuclear configuration by means of which the electronic matrix element should be determined. We shall do this by considering the expansion of the electronic wavefunctions js and jl derived in Section 1.3: ð0Þ
ð1Þ
ð2Þ
ð0Þ
ð1Þ
ð2Þ
js ¼ js þ ljs þ l2 js þ jl ¼ jl þ ljl þ l2 jl þ ;
ð5:2Þ
where the order of perturbation have now been displaced explicitly in terms of ðiÞ ðiÞ a parameter l.1) The functions js and ðjl Þ in (5.2) are corrections of ith orders, obtained through the Rayleigh–Schr€odinger expansion of the adiabatic wavefunction js ðjl Þ in terms of crude BO wavefunctions about arbitrary reference values q0 . The latter may be determined by the generalized average q-centroid approximation. If we take ðqU=qqm Þ0 to be of the first order, ðq2 U=qqm qqg Þ0 of the second order, and so ð1Þ ð2Þ on, the functions jb ðb ¼ s; lÞ are linear in qm , jb are quadratic in qm , and so on. Substituting the expansion (5.2) of electronic wavefunction js and jl into the matrix element (5.1) and collecting terms of the same order in l after squaring the matrix element, we obtain D ED E ð1Þ ð0Þ ð1Þ 0 Vsm;ln 2 ¼l2 jð0Þ jl xln jH0 BO jjs xsm s xsm jH BO jjl xln D ED E D E ð0Þ ð1Þ ð0Þ ð2Þ ð1Þ ð1Þ jl xln jH0 BO jjs xsm þ jl xln jH 0 BO jjs xsm þl3 js xsm jH 0 BO jjl xln D E D ED E ð0Þ ð2Þ ð1Þ ð1Þ ð0Þ ð1Þ jl xln jH 0 BO jjs xsm þl3 js xsm jH 0 BO jjl xln þ js xsm jH 0 BO jjl xln ð2Þ
ð3Þ
¼Csmln þCsm;ln ; ð5:3Þ
where we have truncated the expansion after the third-order term of jVsm;ln j2 (in the expressions Csm;ln , we have set l¼1). Using the expansion (5.2), the electronic matrix elements appearing in (5.3) can be evaluated to give in lowest order of perturbation, D E * + ð0Þ ð0Þ q js ðqU=qqlg Þ0 jl ð1Þ g ; ð5:4aÞ ¼ i h Rsl ¼ h jð0Þ j s i qqlg l El ðq0 ÞEs ðq0 Þ D E + ð0Þ s ð0Þ q j ðqU=qq Þ j s g 0 l ð0Þ ; ¼ i h ¼h jl i s jð1Þ qqg s Es ðq0 ÞEl ðq0 Þ *
g
Rsl
ð5:4bÞ
1) The purpose of introducing the parameter l is simply to identify the various orders in the perturbation. The parameter l is then set equal to 1 when this identification has been made.
j113
j 5 The Nuclear Coordinate Dependence of Matrix Elements
114
and in the next (third) order of perturbation 0 1 * + 2 ð0Þ q Uðr; qÞ ð0Þ @ A * + " jl qqs qqs js n g X ð0Þ q ð2Þ 0 ¼ ih ðqsn q0n Þ h jl i s js ðq ÞE ðq Þ E s l qqg 0 0 n þ
D ED ð0Þ E ð0Þ ð0Þ ð0Þ jc ðqU=qqsn Þ0 js X jl ðqU=qqsg Þ0 jc c6¼s
þ
D E ð0Þ ED ð0Þ ð0Þ ð0Þ jc ðqU=qqsg Þ0 js X jl ðqU=qqsn Þ0 jc c6¼s
¼
ðEs ðq0 ÞEl ðq0 ÞÞðEs ðq0 ÞEc ðq0 ÞÞ
X n
ðEs ðq0 ÞEl ðq0 ÞÞðEs ðq0 ÞEc ðq0 ÞÞ
ðqsn q0n Þ # ðqsn q0n Þ
Mgn ðslÞðqsn q0n Þ;
ð5:5aÞ
D ED E + ð0Þ ð0Þ l ð0Þ s ð0Þ j j j ðqU=qq Þ ðqU=qq Þ X X c c n 0 g 0 js l ð1Þ q ð1Þ ¼ i h ðqln q0n Þ h jl i s js ðq ÞE ðq ÞÞðE ðq ÞE ðq ÞÞ ðE s c c l qqg 0 0 0 0 n c6¼s X ¼ Lgn ðslÞðqln q0n Þ; ð5:6aÞ *
n
where the summation over n in Equations 5.5 and 5.6 includes all (promoting and accepting) modes and * 2 h
E 2D ð0Þ + 2 ð0Þ jl ð1=2Þðq2 U=qqsg Þ0 js q2 ð2Þ j ¼ 2h2 4 s2 s Es ðq0 ÞEl ðq0 Þ qqg
ð0Þ jl
D ED E ð0Þ ð0Þ 3 ð0Þ ð0Þ jc ðqU=qqsg Þ0 js X jl ðqU=qqsg Þ0 jc 5: þ ðEs ðq0 ÞEl ðq0 ÞÞðEs ðq0 ÞEc ðq0 ÞÞ c6¼s
ð5:7Þ
In Equations 5.4–5.7, the energy of the zero-order states, Eb ðq0 Þ ðb ¼ s; l; cÞ, is taken at the q0 -centroid. The third-order (in l) electronic matrix elements appearing on the left-hand (bra) side of (5.3) are obtained from the derivations (5.5a), (5.6a), and (5.7) with indices s and l interchanged: * + X ð0Þ q ð2Þ ¼ h js i l jl Mgn ðlsÞðqln q0n Þ ð5:5bÞ qqg n and * h
+ q X ð1Þ ¼ Lgn ðlsÞðqsn q0n Þ: jl l qqg n
jð1Þ s i
ð5:6bÞ
5.1 The q-Centroid Approximation
j115
With these expressions we have given a complete set of matrix elements to evaluate the thermally averaged rate constants for the radiationless decay between states s and l [138 –143] in successive order of approximation with respect to l. Following the concept of Section 3.3, we have in second order 2p X 1 C ð2Þ hwnr iT ¼ pðm; TÞCsm;ln ¼ w ð2Þ ðslÞc þ wð2Þ ðslÞcc ; h fm g;fn g p ðEsm Eln Þ2 þ C2 m m ð5:8Þ
where wð2Þ ðslÞc represents just the expression (3.75) for the nonradiative decay rate considered in Section 3.3. The second term wð2Þ ðslÞcc in Equation 5.8 contains mixedtype single promoting mode generating functions Ig ðtÞ and Ig0 ðtÞ (see Equations 3.10 and 3.74) and vanish, if the promoting modes are nontotally symmetric, as in this case kg ¼ kg0 ¼ 0. The q-centroid is introduced at the next level of approximation. Taking first the third-order terms occurring on the right (ket) side of (5.3), we have w ð3Þ ðslÞ ¼ w ð3Þ ðslÞ1 þ w ð3Þ ðslÞ2 ;
ð5:9Þ
where
0 1 q 2p X X ð2Þ @ g s l w ðslÞ1 ¼ pðm; TÞRsl Rsl xsm ð q Þi h l xln ð q ÞA xln ðql Þjxsm ðqs ÞÞ h g;g0 fm g;fn g qqg ð3Þ
n
1 C ; p ðEsm Eln Þ2 þ C2
with ð2Þ Rsl
n
2 h ¼ 2
*
ð5:10aÞ
+ q2 ð2Þ ; 2 j qqsg0 s
ð0Þ jl
ð5:11Þ
and 1 0 XX X 2p q g ð3Þ @ w ðslÞ2 ¼ pðm; TÞRsl xsm ih l xln A h g;g0 m fm g;fn g q q g n
n
1 0 13 s qx qx C A þLg0 m ðslÞ@xln ðql q0m Þi A5 1 h sm : 4Mg0 m ðslÞ@xln ðqm q0m Þih sm m s s qq qq p ðEsm Eln Þ2 þ C2 g0 g0 2
0
ð5:12Þ
Introducing integral representation of the Lorentzian function (see Equation 3.9) into (5.10) and proceeding as in Section 3.3, we obtain w ð3Þ ðslÞ1 ¼ ðh2 ÞZ 1
X g;g0
g
ð2Þ
1 ð
Rsl Rsl
dt exp½iVcjtjIg ðtÞGN1 ðtÞ; 1
ð5:10bÞ
j 5 The Nuclear Coordinate Dependence of Matrix Elements
116
where Equations 3.12, 3.15 and 3.74 have been used. Notice that wð3Þ ðslÞ1 ¼ 0, if the promoting modes g are nontotally symmetric. To continue, we consider w ð3Þ ðslÞ2. The appearance of qsm (and qlm ) coordinates in the expression of (5.12) must be considered in detail, because the summation over m covers normal modes that have nonvanishing normal coordinate displacements ðmÞ k23;...;N and mix under a perturbation of the full symmetry of the molecular group with corresponding partners of identically transforming symmetry representation. Thus, the modes constitute a block separated from the remaining (promoting) modes discussed so far (see the shaded area in the matrix W of Section 1.2). If for convenience in order to clearly portray the physical situation, we regard the presence of only two accepting modes, this may be done using Equation 3.21. Although our discussion deals with the case of two accepting modes, the principal results obtained can easily be generalized. To represent Equation 5.12 in a particular transparent manner, it is convenient to decompose (split) it into classes or prototype parts, depending on the nature of the triple indices g; g0 ; and m representing modes of different symmetries, w ð3Þ ðslÞ2 ¼ w ð3Þ ðslÞ21 þ w ð3Þ ðslÞ22 þ wð3Þ ðslÞ23 þ w ð3Þ ðslÞ24 þ w ð3Þ ðslÞ25 þ w ð3Þ ðslÞ26 ; ð5:13Þ
where the individual components are obtained directly from Equation 5.12. These are as under: 1( 0 X X 2p qx g ln w ð3Þ ðslÞ21 ¼ pðm; TÞRsl @xsm i h l A Mgg ðslÞ þ Lgg ðslÞ h g fm g;fn g qqg n
n
1 0 19 = l qx qx sm A A þ kg Mgg ðslÞ@xln i dðEsm Eln Þ; h @xln ðqg q0g Þih sm s qqsg qqg ; 0
ð5:14Þ
where for the promoting mode, we write qsg ¼ qlg þ kg . For convenience, we have reinserted in Equation 5.14 the energy conserving d-function in place of the Lorentzian distribution of Equations 5.10 or 5.12 (but with the understanding that smooth representations of the Dirac delta function are to be taken). For the second term in Equation 5.13, we may write w ð3Þ ðslÞ22
1( 0 xln 2p X X X g@ ¼ pðm; TÞRsl xsm i h l A Mgm ðslÞ h g m6¼g fm g;fn g qqg n
n
1 0 19 = s qx qx sm A A þ Lgm ðslÞ@xln ðql q0m Þi dðEsm Eln Þ: @xln ðqm q0m Þih sm h m qqsg qqsg ; 0
ð5:15Þ
The relationship here between the totally symmetry coordinates qsm and qlm ðm ¼ 1; 2Þ are given by Equation 3.21. Similarly,
5.1 The q-Centroid Approximation ð3Þ
w ðslÞ23
1( 0 qxln 2p X X X g@ ¼ pðm; TÞRsl xsm i h l A Mmg ðslÞ þ Lmg ðslÞ h g m6¼g fm g;fn g qqg n
n
1 0 19 l qxsm = qx sm @xln ðqg q0g Þih s A þ kg Mmg ðslÞ@xln i h s A dðEsm Eln Þ; qqm qqm ; 0
ð5:16Þ
where the summation over m covers totally symmetric modes. In the following expressions, g and g0 refer to promoting modes that are distinct: 1( 0 qxln 2p X X X g@ ð3Þ w ðslÞ24 ¼ pðm; TÞRsl xsm ih l A Mg0 g0 ðslÞ þ Lg0 g0 ðslÞ h g g0 6¼g fm g;fn g qqg n n m
1 0 19 l qxsm = qx sm @xln ðqg0 q0g0 Þih s Aþ kg0 Mg0 g0 ðslÞ@xln i h s A dðEsm Eln Þ; qqg0 qqg0 ; 0
ð3Þ
w ðslÞ25
ð5:17Þ
1( 0 qxln 2p X X X g@ ¼ pðm; TÞRsl xsm ih l A Mg0 m ðslÞ h g6¼g0 m6¼g fm g;fn g qqg n
n
1 0 19 = s l qx x sm sm h s A dðEsm Eln Þ: @xln ðqm q0m Þih s A þ Lg0 m ðslÞ@xln ðqm q0m Þi qqg0 qqg0 ; 0
ð5:18Þ
Finally, we consider ð3Þ
w ðslÞ26
1( 0 qxln 2p X X X g@ ¼ pðm; TÞRsl xsm ih l A Mgg0 ðslÞ þ Lgg0 ðslÞ h g g0 6¼g fm g;fn g qqg n
n
1 0 19 l qxsm = qx sm @xln ðqg0 q0g0 Þih s A þ kg0 Mgg0 ðslÞ@xln i h s A dðEsm Eln Þ: qqg qqg ; 0
ð5:19Þ
This last expression may be regarded as a supplement to the expression w ð3Þ ðslÞ21 , if g and g0 are assigned to distinct promoting modes. For further discussion of these equations, it is useful to transform the w ð3Þ ðslÞ2i of Equations 5.14–5.19 into a more convenient form. Proceeding as in Chapter 3, the expression for w ð3Þ ðslÞ21 can be written as w ð3Þ ðslÞ21 ¼ ðh2 ÞZ1
X g
g
1 ð
Rsl
dt exp½iVtcjtj 1
f½Mgg ðslÞ þ Lgg ðslÞ½Jgð0Þ ðtÞq0g Kgð0Þ ðtÞ þ kg Mgg ðslÞKgð0Þ ðtÞgGN ðtÞ;
ð5:20Þ
where Kg ðtÞ corresponds to the single-mode generating function (which involves the nuclear momentum operator for the promoting mode qg ) defined in Equation 3.72,
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118
and Jg ðtÞ is defined by X Jg ðtÞ ¼ exp½mg ðit vsg þ hvsg =kB TÞexpðitng vlg Þ mg ;ng
1 ð
h2
ð
qxlng ðblg qlg Þ 1=2
dqlg dqlg qlg xsmg ðbsg qsg Þi 1=2
qqlg
1
¼ h2
ÐÐ
qxsmg ðbsg qsg Þ 1=2
xlng ðblg qlg Þi 1=2
qqsg
q s s s q r ðq ; q ; wg Þi l rlg ðqlg ; qlg ; zg Þ: qqsg g g g qqg
dqlg dqlg qlg i
ð5:21Þ
Jg ðtÞ is calculated in the Appendix D and can be expressed as 0 1 2 g bsg kg 2bsg blg k2g w g w h2 s l A @ 4 Jg ðtÞ ¼ bg bg 3 s 2 s l s l 1 1 1 2 g þ bg zg Þ ðbg zg þ bg w g Þ 1 ðbg w ðbg zg þ blg w g Þ þ
#
z1 g
g
g
G1 ðtÞ ¼ Jgð0Þ ðtÞG1 ðtÞ:
l 1 1 zg Þ ðbsg w g þ bg
ð5:22Þ
ð0Þ
The part of w ð3Þ ðslÞ21 involving Jg ðtÞ and kg vanishes if the promoting mode g is nontotally symmetric. Similarly, after a sequence of steps, the next expression can be brought to the form wð3Þ ðslÞ22 ¼ ðh2 ÞZ1
XX g
m6¼g
g
1 ð
Rsl
h ð0Þ ðtÞq0m dt exp½itVcjtj Mgm ðslÞ H m
1
i þ Lgm ðslÞ Hmð0Þ ðtÞq0m Kgð0Þ ðtÞGN ðtÞ
ð5:23Þ
where ð Hm ðtÞ ¼
1 ð
dql1 dql2 dql1 dql2 qlm rs1 ðqs1 ; qs1 ; w1 Þrs2 ðqs2 ; qs2 ; w2 Þrl1 ðql1 ; ql1 ; z1 Þrl2 ðql2 ; ql2 ; z2 Þ;
1
ð5:24Þ
and correspondingly ðm ¼ 1:2Þ m ðtÞ ¼ H
ð
ð1
dql1 dql2 dql1 dql2 qsm rs1 ðqs1 ; qs1 ; w1 Þrs2 ðqs2 ; qs2 ; w2 Þrl1 ðql1 ; ql1 ; z1 Þrl2 ðql2 ; ql2 ; z2 Þ;
1
ð5:25Þ
with qsm and qlm given by Equation 3.21. The straightforward, but somewhat tedious, evaluation of these integrals is made in Appendix D. The results are Hm ðtÞ ¼ Hmð0Þ ðtÞG2 ðtÞ;
m ¼ 1; 2;
ð5:26Þ
5.1 The q-Centroid Approximation
with ð0Þ
H1 ðtÞ ¼
n o 1 ð12Þ 1w 2 þ w11 b1 kð1Þ 1 z2 þ w21 b21 kð2Þ 2 z2 ; b1 b2 k1 w 12 w 12 w B1 ðw1 ; w2 ; z1 ; z2 Þ ð5:27Þ
and ð0Þ
H2 ðtÞ ¼
n o 1 ð12Þ 1w 2 þ w12 b12 kð1Þ 1 z1 þ w22 b2 kð2Þ 2 z1 : b1 b2 k2 w 12 w 12 w B1 ðw1 ; w2 ; z1 ; z2 Þ ð5:28Þ
The quantity B1 was previously derived and given by Equation 3.27: 2 2 1w 2 þ w11 1 z2 þ w12 1 z1 B1 ðw1 ; w2 ; z1 ; z2 Þ ¼ b1 b2 w b1 w b12 w 2 2 2 z2 þ w22 2 z1 þ z1 z2 : þ w21 b21 w b2 w
ð5:29Þ
Without repeating the details, we follow once again the steps that led to Equations 5.26–5.28. With somewhat greater effort and upon the results given in Appendix D, we find ð0Þ ðtÞG2 ðtÞ; m ðtÞ ¼ H H m
m ¼ 1; 2;
ð5:30Þ
with ð0Þ H 1 ðtÞ ¼
n o 1 ð12Þ 2 z2 þ w22 b2 kð12Þ 2 z1 þ kð1Þ w21 b21 k2 w z1 z2 ; 1 w 12 B1 ðw1 ; w2 ; z1 ; z2 Þ ð5:31Þ
and ð0Þ ðtÞ ¼ H 2
n o 1 ð12Þ 1 z1 þ w11 b1 kð12Þ 1 z2 þ kð2Þ w12 b12 k1 w z1 z2 : 2 w 12 B1 ðw1 ; w2 ; z1 ; z2 Þ ð5:32Þ
The complexity introduced by the normal coordinate mixing (3.21) is considerable. ð1Þ ð2Þ Apart from the displacements k12 and k12 (referred to as the direct terms) and frequency parameters b1 and b2 of the individual modes, expressions 5.27–5.32 ð12Þ ð12Þ involve reciprocal displacements k1 and k2 as well as cross-frequency parameters b12 and b21 . This implication will be subsequently overcome by approximations that make the problem more manageable. Let us now focus our attention on w ð3Þ ðslÞ23 . It is worth noting that the summation over m in (5.16) covers totally symmetric modes that have nonvanishing normal coordinate displacements. These modes are supposed to be mixed with each other as we have already shown above and separated from the remaining nontotally symmetric vibrational modes. Then in terms of Fourier integral, we may obviously
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rewrite Equation 5.16 as wð3Þ ðslÞ23 ¼ ðh2 ÞZ1
XX g
m6¼g
g
1 ð
dt exp½itVcjtj ½Mmg ðslÞ
Rsl 1
ð0Þ
ð0Þ ð0Þ þ Lmg ðslÞ½Dð0Þ g ðtÞq0g Ig ðtÞ þ kg Mmg ðslÞIg ðtÞgN m ðtÞGN ðtÞ;
ð5:33Þ
where again qsg ¼ qlg þ kg have been set. The function Dg ðtÞ for the promoting mode is defined by 1 ð
ð
Dg ðtÞ ¼ h 1
q dqlg dqlg qlg rsg qsg ; qsg ; wg i l rlg qlg ; qlg ; zg ; qqg
ð0Þ
ð5:34Þ
ð0Þ
m ðtÞ ðm ¼ 1; 2Þ are related to H m ðtÞ (Equation 5.25), with qsm being replaced and N there by the nuclear momentum operator i hq=qqsm. Then (see Appendix D), # 2
" z1 2bsg k2g z1 zg 1 g g g l s s G1 ðtÞ Dg ðtÞ ¼ ihbg s 1 l 1 l l 1 2 1 2 ðbg w g þ bg zg Þ ðbg w g þ bg zg Þ ðbg zg þ bg w g Þ g
¼ Dð0Þ g ðtÞG1 ðtÞ
ð5:35Þ
and ð0Þ ð0Þ mH N hbsm w m ðtÞ ¼ i m ðtÞ;
m ¼ 1; 2:
ð5:36Þ
ð0Þ
By retaining only the dominating term of Dg ðtÞ when vsg ¼ vlg and kg ¼ 0, we then find Dð0Þ g ðtÞ ¼
ih zg wg ih g expðit vg þ ¼ n hvg =kB TÞexpðitvg Þ ; 2 1wg zg 2
ð5:37Þ
g ¼ ðebhvg 1Þ1 is the number of excited vibrations of the promoting mode where n at thermal equilibrium. Likewise, w ð3Þ ðslÞ24 is rewritten as 2
ð3Þ
w ðslÞ24 ¼ ðh ÞZ
1
P P
g g0 6¼g Rsl
g
1 ð
dt exp½itVcjtjf½Mg0 g0 ðslÞ 1
ð0Þ
ð0Þ
ð0Þ
þ Lg0 g0 ðslÞ½Bg0 ðtÞ þ q0g0 Ig0 ðtÞ þ kg0 Mg0 g0 ðslÞIg0 ðtÞgIgð0Þ ðtÞGN ðtÞ; ð5:38Þ
where 1 ð
Bg0 ðtÞ ¼ h 1
ð
dqlg0 dqlg0 qlg0 i
q s s s r 0 ðq 0 ; q 0 ; wg0 Þrlg0 ðqlg0 ; qlg0 ; zg0 Þ: qqsg0 g g g
ð5:39Þ
5.1 The q-Centroid Approximation
Analogous to Dg ðtÞ, this is found to be 2
1 w g0 w 1 g0 þ Bg0 ðtÞ ¼ ihbsg0 4 s l s 1 2 g0 þ bg0 zg0 g0 þ blg0 z1 bg0 w bg0 w g0 # 2bsg blg0 k2g0 z1 g0 ð0Þ g0 g0 2 G1 ðtÞ ¼ Bg0 ðtÞG1 ðtÞ s 1 l 1 g0 bg0 zg0 þ bg0 w
ð5:40Þ
If the promoting modes g are nontotally symmetric, then w ð3Þ ðslÞ24 vanishes. Let us now return to Equation 5.18. Remembering that the summation over m covers nonseparable totally symmetric modes, we have, similar to as in the case of Equation 5.23, w ð3Þ ðslÞ25 ¼ ðh2 ÞZ 1
1 ð 2 n XXX g ð0Þ ðtÞq0m Rsl dt exp½itVcjtj Mg0 m ðslÞ H m g g0 6¼g m¼1
1
o ð0Þ Igð0Þ ðtÞIg0 ðtÞGN ðtÞ; þ Lg0 m ðslÞ Hmð0Þ ðtÞq0m
ð5:41Þ
from which follows that wð3Þ ðslÞ25 vanishes if the promoting modes g are nontotally symmetric. On completing the evaluation of Equation 5.19, we verify that w ð3Þ ðslÞ26 ¼ ðh2 ÞZ1
XX g g0 6¼g
g
1 ð
Rsl
dt exp½itVcjtjf½Mgg0 ðslÞ 1
ð0Þ
þ Lgg0 ðslÞðCg0 ðtÞq0g0 Þ þ kg0 Mgg0 ðslÞg Kgð0Þ ðtÞGN ðtÞ;
ð5:42Þ
with 1 ð
Cg0 ðtÞ ¼
ð
dqlg0 dqlg0 qlg0 rsg0 ðqsg0 ; qsg0 ; wg0 Þrlg0 ðqlg0 ; qlg0 ; zg0 Þ ¼
1
g0 bsg0 kg0 w g0 ðbsg0 w
þ blg0 zg0 Þ
g0
G1 ðtÞ: ð5:43Þ ð0Þ
For g0 being a promoting mode, only the part of (5.42) that contains q0g0 Kg ðtÞ contributes to the q-centroid. A discussion similar to that carried out above leads for the second part of the squared matrix elements (5.3), which comes from the left (bra) position, to further nonvanishing nonradiative rate constants. These are ð3Þ ðslÞ21 ¼ ðh2 ÞZ 1 w
X
ð0Þ
g
g
1 ð
dt exp½itVcjtjf½Mgg ðlsÞ
Rsl
1
þ Lgg ðlsÞ½ J g ðtÞq0g Kgð0Þ kg Mgg ðlsÞKgð0Þ ðtÞgGN ðtÞ;
ð5:44Þ
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j 5 The Nuclear Coordinate Dependence of Matrix Elements
122
ð0Þ
where Kg ðtÞ is given by Equation 3.72 and the single-mode generating function J g ðtÞ is now defined by ðð q q J ðtÞ ¼ h2 d qlg dqlg qsg i s rsg ðqsg ; qsg ; wg Þi l rlg ðqlg ; qlg ; zg Þ: ð5:45Þ g qqg qqg Without repeating the details, we follow once again the steps that led to Equation 5.22 ð0Þ g and obtain J g ðtÞ ¼ J g ðtÞG1 ðtÞ, where "
2 blg kg 2bsg blg k2g zg h ð0Þ s l J ðtÞ ¼ bg bg g l 1 2 2 g þ blg zg Þ ðbsg z1 g Þ ðbsg w g þ bg w 3
zg ðbsg z1 g
1 þ blg w g Þ
þ
1 w g 1 ðbsg w g
þ blg z1 g Þ
:
ð5:46Þ
We may also arrive at this result by considering the symmetry of the originally derived generating function Jg ðtÞ, interchanging bsg by blg and simultaneously wg by zg. Note g that incidentally the single-mode generating functions Kg ðtÞ and G1 ðtÞ are invariant under such transformation. We recall that the interchange s , l relates also the electronic matrix elements Mgg ðlsÞ and Lgg ðlsÞ appearing in (5.44) to those given in ð3Þ ðslÞ21 Equations 5.5a and 5.6a. As a closing remark, we note that the part of w ð0Þ involving J g ðtÞ and kg vanishes if the promoting modes g are nontotally symmetric. In precisely the same manner as we have done above, the reader can verify by elementary method that 2
ð3Þ
w ðslÞ22 ¼ ðh ÞZ þ Lgm ðlsÞ
1
XX g
m6¼g
g Rsl
ð0Þ H m ðtÞq0m
1 ð
h dt exp½itVcjtj Mgm ðlsÞ Hmð0Þ ðtÞq0m
1 i Kgð0Þ ðtÞGN ðtÞ;
ð5:47Þ
ð0Þ ð0Þ ðtÞ ðm ¼ 1; 2Þ are where the two-dimensional generating functions Hm ðtÞ and H m given by Equations 5.27–5.32. Without repeating the details, we follow once again the steps that led to Equation 5.33 and may write
ð3Þ ðslÞ23 ¼ ðh2 ÞZ1 w
XX g
m6¼g
g
1 ð
Rsl
dt exp½itVcjtjf½Mmg ðlsÞ 1
ð0Þ ð0Þ ð0Þ ð0Þ þ Lmg ðlsÞ½D g ðtÞq0g Ig ðtÞkg Mmg ðlsÞIg ðtÞgNm ðtÞGN ðtÞ;
ð5:48Þ
where m covers nonseparable totally symmetric modes. The single-mode generating function appearing in Equation 5.48 is defined as g ðtÞ ¼ h D
1 ð
ð
dqlg dqlg qsg i
q s s s r ðq ; q ; wg Þrlg ðqlg ; qlg ; zg Þ qqsg g g g
01 12 3 2 1 1 2blg k2g w w w 1 g g g s 5Gg ðtÞ s s ¼ @ ihbg A4 s 1 l 1 l 1 þ bl w 1 Þ2 2 1 z w z z ðbg w þ b Þ ðb þ b Þ ðb g g g g g g g g g g g ð0Þ
ðtÞG ðtÞ: ¼D g 1 g
ð5:49Þ
5.2 Determination of the q-Centroid ð0Þ
g ðtÞ Again, the interchange bsg , blg and wg , zg relates the generating function D ð0Þ ð0Þ ðtÞ is to Dg ðtÞ. The dominating term of D g ð0Þ ðtÞ ffi D g
ih wg zg ih g expðitvg þ ¼ hvg =kB TÞexpðitvg Þ : n 2 1wg zg 2 ð5:50Þ ð0Þ
The functions Nm ðtÞ appearing in Equation 5.48 are Nmð0Þ ðtÞ ¼ ihblm zm Hmð0Þ ðtÞ;
m ¼ 1; 2:
ð5:51Þ
ð0Þ
ð0Þ
ð3Þ ðslÞ23 involving Ig ðtÞ and Since Ig ðtÞ ¼ 0 if qg is a promoting mode, the part of w ð3Þ ðslÞ24 ; w ð3Þ ðslÞ25 ; and that that correkg vanishes. The remaining expressions w ð3Þ sponds to w ðslÞ1 do not contribute to the derivation of the q-centroid (as do w ð3Þ ðslÞ24 ; w ð3Þ ðslÞ25 , and w ð3Þ ðslÞ1 above) and are not given here. Finally, analogous to Equation 5.42, we obtain the expression ð3Þ ðslÞ26 ¼ ðh2 ÞZ1 w
XX g g0 6¼g
g
Rsl
1 ð
n dt exp½itVcjtj ½Mgg0 ðlsÞ
1 o ð0Þ þ Lgg0 ðlsÞ Cg0 ðtÞq0g0 kg0 Mgg0 ðslÞ Kgð0Þ ðtÞGN ðtÞ;
ð5:52Þ
where ð0Þ C g0 ðtÞ ¼
blg0 kg0 zg0 g0 þ blg0 zg0 Þ ðbsg0 w
:
ð5:53Þ
5.2 Determination of the q-Centroid
Our discussion up to this point has been restricted to determination of the decay rates of nonradiative transitions up to third order of perturbation theory. We have established how the transition probabilities may be reduced by the knowledge of the average of the density of states weighted vibrational overlap factor and its symmetry properties. Assuming that the promoting modes are nontotally symmetric (ns) and separated from the totally symmetric accepting modes (ts), we have found that ð3Þ ðslÞ1 ¼ w ð3Þ ðslÞ24 ¼ w ð3Þ ðslÞ24 ¼ w ð3Þ ðslÞ25 ¼ w ð3Þ ðslÞ25 ¼ 0: w ð2Þ ðslÞcc ¼ w ð3Þ ðslÞ1 ¼ w ð5:54Þ
The nonradiative decay rate constant becomes hwnr iT ¼ w ð2Þ ðslÞc þ
3 X ð3Þ ðsl Þ2i þ w ð3Þ ðsl Þ26 þ w ð3Þ ðsl Þ26 ; w ð3Þ ðsl Þ2i þ w i¼1
ð5:55Þ
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124
where w ð2Þ ðslÞc , the leading term, is given by (5.8) and w ð3Þ ðslÞ21 ; w ð3Þ ðslÞ22 ;w ð3Þ ðslÞ23 ; and w ð3Þ ðslÞ26 are given by the following: 2
ð3Þ
w ðslÞ21 ¼ ðh ÞZ
1
X g
Rgsl
1 ð
dt exp½iVtcjtj½Mgg ðslÞ þ Lgg ðslÞKgð0Þ ðtÞGN ðtÞðq0g Þ;
1
ð5:56aÞ
wð3Þ ðslÞ22 ¼ ðh2 ÞZ1 þ Lgm ðslÞ
XX g
m6¼g
XX g
h ð0Þ ðtÞq0m dt exp½itVcjtj Mgm ðslÞ H m
1
Hmð0Þ ðtÞq0m
w ð3Þ ðslÞ23 ¼ ðh2 ÞZ1
1 ð
g
Rsl
m6¼g
i
g
Kgð0Þ ðtÞGN ðtÞ; 1 ð
ð5:57aÞ
dt exp½itVcjtj Mmg ðslÞ
Rsl 1
ð0Þ þ Lmg ðtÞ Dð0Þ g ðtÞN m ðtÞGN ðtÞ;
m ¼ 1; 2;
ð5:58aÞ
and w ð3Þ ðslÞ26 ¼ ðh2 ÞZ1
XX
1 ð
g
g g0 6¼g
Rsl
dt exp½itVcjtj½Mgg0 ðslÞ 1
þ Lgg0 ðslÞKgð0Þ ðtÞGN ðtÞðq0g0 Þ:
ð5:59aÞ
Similarly, we find ð3Þ
2
ðslÞ21 ¼ ðh ÞZ w
1
X g
Rg sl
1 ð
dt exp itVcjtj Mgg ðlsÞ
1
þ Lgg ðlsÞ Kgð0Þ ðtÞGN ðtÞðq0g Þ;
ð3Þ ðslÞ22 ¼ ðh2 ÞZ1 w þ Lgm ðlsÞ
XX g
m6¼g
ð0Þ ðtÞq0m H m
ð3Þ ðslÞ23 ¼ ðh2 ÞZ1 w
XX g
m6¼g
1 ð
g
Rsl
ð5:56bÞ
h dt exp½itVcjtj Mgm ðlsÞ Hmð0Þ ðtÞq0m
1
Kgð0Þ ðtÞGN ðtÞ;
g
ð5:57bÞ
1 ð
Rsl
dt exp½itVcjtj½Mmg ðlsÞ 1
ð0Þ ð0Þ þ Lmg ðlsÞD g Nm ðtÞGN ðtÞ;
ð5:58bÞ
5.2 Determination of the q-Centroid
and finally, ð3Þ ðslÞ26 ¼ ðh2 ÞZ1 w þ Lgg0 ðlsÞ
XX
g
Rsl
1 ð
j125
dt exp itVcjtj Mgg0 ðlsÞ
g g0 6¼g 1 ð0Þ Kg ðtÞGN ðtÞðq0g0 Þ:
ð5:59bÞ
After these preparations, the q-centroid may now be determined by those q0g and q0m appearing in (5.56)–(5.59), which likewise cause the sum in (5.55) to vanish. First, we considerthenontotallysymmetric (ns)vibrations. SinceEquations 5.56 and5.59 contain directly the nontotally symmetric mode q0g and Equations 5.58 are nonzero if g is ns and m is totally symmetric (ts), the q-centroid condition for the ns modes is given by 8 1 ð X <X g0 ð0Þ Rsl ½Mg0 g ðslÞ þ Lg0 g ðslÞ dt exp itVcjtj Kg0 ðtÞGN ðtÞ : 0 g g 1 ) 1 ð ð0Þ 0 g þ Rsl ½Mg0 g ðlsÞ þ Lg0 g ðlsÞ dt exp itVcjtj Kg0 ðtÞGN ðtÞ ðq0g Þ þ
8 X <X g
:
m
1 1 ð
g
ð0Þ dt exp itVcjtj Dð0Þ g ðtÞN m ðtÞGN ðtÞ
Rsl ½Mmg ðslÞ þ Lmg ðslÞ
g þ Rsl ½Mmg ðlsÞ þ Lmg ðlsÞ
1 1 ð
ð0Þ g ðtÞNmð0Þ ðtÞGN ðtÞ dt exp itVcjtj D
) ¼ 0;
1
ð5:60Þ
where we have combined Equations 5.56 and 5.59 and rewritten in a compact form. Then, g
Rsl
ð1 X ð0Þ ½Mmg ðslÞ þ Lmg ðslÞ dt exp itVcjtj Dð0Þ g ðtÞN m ðtÞGN ðtÞ m
g þ Rst
1
X m
½Mmg ðlsÞ þ Lmg ðlsÞ
ð1 1
ð0Þ ðtÞN ð0Þ ðtÞGN ðtÞ dt exp itVcjtj D m g
; q0g ¼ X n o ð1 ð0Þ g0 g0 Rsl ½Mg0 g ðslÞ þ Lg0 g ðslÞ þ Rsl ½Mg0 g ðlsÞ þ Lg0 g ðlsÞ dt exp itVcjtj Kg0 ðtÞGN ðtÞ 1
g0
g ¼ ns; m ¼ ts: ð5:61Þ
For totally symmetric vibrations, we need only Equations 5.57. The q-centroid is then ð3Þ ðslÞ22 ¼ 0. This gives determined by setting w ð3Þ ðslÞ22 þ w ð1 X g ð0Þ g m ðtÞKgð0Þ ðtÞGN ðtÞ ½Rsl Mgm ðslÞ þ Rsl Lgm ðlsÞ dt exp itVcjtj H 1
g
ð1 X g ½Rsl Lgm ðslÞ þ Rg M ðlsÞ dt exp itVcjtj Hmð0Þ ðtÞKgð0Þ ðtÞGN ðtÞ þ gm sl g
1
q0m ¼ X n ; o ð1 g g Rsl ½Mgm ðslÞ þ Lgm ðslÞ þ Rsl ½Mgm ðlsÞ þ Lgm ðlsÞ dt exp½itVcjtjKgð0Þ ðtÞGN ðtÞ g
1
m ¼ ts: ð5:62Þ
j 5 The Nuclear Coordinate Dependence of Matrix Elements
126
Several features of Equations 5.61 and 5.62 deserve comment: Equations 5.61 and 5.62 are quite general and have a clear physical significance. They provide us with the correct expression for the q-centroid configuration. Equation 5.61 as well as Equation 5.62 may be understood as an existential theorem, or more correctly, as a fix point theorem, since it may be written in the form q0 ¼ Jðq0 Þ, where the function J is given by the righthand side of Equation 5.61 or 5.62. The calculation of both Equations 5.61 and 5.62 then requires (i) knowledge of this function over the region of nuclear coordinates between the equilibrium position and the q-centroid and (ii) the density of states weighted vibrational overlap factor, which involves all vibrational (promoting and accepting) modes contributing to the radiationless decay rate. The evaluation of the former requires the knowledge of electronic matrix elements appearing in Equations 5.61 and 5.62, generally an involved numerical task. The latter is usually beyond our ability to accurately calculate. To further pursue this matter, we note that the q-centroid is temperature dependent. The latter is extracted by making the change of variables wm ¼ expðivsm tÞexpðhvsm =kB TÞ as seen in Section 3.3. Later we will see from the discussion below that the q-centroid depends on the rotation of the normal coordinates upon electronic excitation. Let us now return to the basic relations (5.27) through (5.32), which play the role of generalized displacement parameters. To gain some insight into the significant feature of these quantities, we consider the zero-temperature limit. We assume that only the vibrationless level of the electronic excited state is occupied with an m ¼ 1 ðm ¼ 1; 2Þ. appreciable probability in thermal equilibrium, and therefore w Furthermore, we make the special assumption by setting vsm ¼ vlm . Under these circumstances, Equation 5.27 reduces to the simpler form ð0Þ H1 ðtÞ
¼
1 ð0Þ
B1
(
h i h ð1Þ ð2Þ ð1Þ ðw11 þ w22 Þk12 þ ðw21 b21 w12 Þk12 þ ðw11 þ w22 Þk12
i ð2Þ ð2Þ þ ðw21 b21 w12 Þk12 expðiv1 tÞðw21 b21 þ w12 Þk12 expðiv2 tÞ ) ð2Þ ðw21 b21 w12 Þk12 exp½iðv1
þ v2 Þt ;
ð5:63Þ
where ð0Þ
2 2 2 2 B1 ¼ 2 þ w11 þ w22 þ w12 b12 þ w21 b21 :
ð5:64Þ
In deducing this result we have used Equation 3.30 to express the reciprocal ð12Þ ð12Þ ð1Þ ð2Þ parameters k1 and k2 by k12 and k12 and by setting z1 ¼ expðiv1 tÞ and ð0Þ z2 ¼ expðiv2 tÞ. Furthermore, the z-dependence of the denominator of H1 ðtÞ has been ignored, since it consists of oscillations about zero with an amplitude considerably smaller than the leading term (5.64). This approximation is made entirely for practical reasons to render a difficult computational problem more manageable. The ð0Þ corresponding expression H2 ðtÞ is obtained from Equation 5.63 by interchanging 1 , 2 (see Equations 5.27 and 5.28).
j127
5.2 Determination of the q-Centroid ð0Þ
ð0Þ
1 ðtÞ ðm ¼ 1; 2Þ. In complete analogy with H ðtÞ, To continue, we consider next H 1 we may recast Equation 5.31 into the form ( h i h 1 ð0Þ ð12Þ ð12Þ ð12Þ 1 ðtÞ ¼ ðw11 þ w22 Þk1 þ ðw12 w21 b21 Þk2 ðw11 þ w22 Þk1 H ð0Þ B1 ð12Þ
þ ðw12 þ w21 b21 Þk2
i
ð12Þ
expðiv1 tÞðw12 w21 b21 Þk2 expðiv2 tÞ )
ð12Þ þ ðw12 þ w21 b21 Þk2 exp½iðv1
þ v2 Þt :
ð5:65Þ
ð0Þ ðtÞ is obtained from (5.65) by interchanging the indices 1 , 2. Similar to above, H 2 ð 0Þ We recall that w11 ¼ w22 ¼ cosj and w12 ¼ w21 ¼ sinj. Consequently, Hm ðtÞ and ð0Þ m ðtÞ ðm ¼ 1; 2Þ become strongly j dependent, even for attainable changes of j. H This is among other things due to the presence of the cross-frequency parameters b12 and b21 that can differ appreciably from unity for different accepting modes. Thus, the entire integrand in Equation 5.62 is j dependent (recall that GN ðtÞ is also a function of j). For parallel accepting modes ðj ¼ 0Þ, Equations 5.63 and 5.65 reveal ðmÞ ð0Þ ð0Þ ðtÞ reduce to that they depend only on k12 , that is, Hm and H m 1 ðmÞ ð0Þ Hm ðtÞ ¼ k12 1 þ expðivm tÞ 2 1 ðmÞ 1 ð12Þ ð0Þ 1expðivm tÞ ¼ k12 1expðivm tÞ ; H m ðtÞ ¼ km 2 2
ð5:66Þ
m ¼ 1; 2:
ð0Þ ð0Þ ðtÞ, we are faced with the Having extracted the significant features of Hm ðtÞ and H m problem of evaluating the Fourier integrals appearing in Equation 5.62 for the q0m -centroid. Formally, this problem can be solved by the same steps that led to Equations 3.75 and 3.77 for the nonradiative transition probability. A very general g analysis of how many promoting modes of nonvanishing coupling terms Rsl occur in Equation 5.62 is fairly complex due to our ignorance of molecular interstate coupling terms. For further discussion of this equation, let us now examine how the q-centroid ð0Þ ð0Þ ðtÞ. It may first be is affected by the several contributions appearing in Hm ðtÞ and H m ð0Þ expected that the q-centroid arises from the constant (nonoscillatory) terms of Hm ðtÞ ð0Þ ð0Þ ð0Þ ð0Þ) either directly or less directly through the electronic ðtÞ (say Hm ð0Þ; H and H m m coupling terms. Indeed, to a first-order approximation, we can write
ð1 X g g ð0Þ ð0Þ þ ½Rg Lgm ðslÞ þ Rg Mgm ðlsÞH ð0Þ ð0Þg f½Rsl Mgm ðslÞ þ Rsl Lgm ðlsÞH dtð Þ m m sl sl q0m
g
X g
g g fRsl ½Lgm ðslÞ þ Mgm ðslÞ þ Rsl ½Lgm ðlsÞ þ Mgm ðlsÞg
ð1 1
1
;
dtð Þ ð5:67Þ
where the ratio of third-order electronic factors evaluated at q0 could be very large or ð0Þ ð0Þ ðtÞ (not small in given instances. The next terms in the numerator of Hm ðtÞ and H m taken into account in (5.67)) contribute among other things due to the time factors
j 5 The Nuclear Coordinate Dependence of Matrix Elements
128
expðiv1 tÞ, expðiv2 tÞ, and exp½iðv1 þ v2 Þt that decrease the energy gap of hV hv2 , and hðv1 þ v2 Þ, respectively. The appearing in Equation 5.62 by sizes of hv1 , latter can be appreciable for good accepting modes.2) Incidentally, this phenomenon is quite analogous to situation that we have already illustrated in Chapter 3 by including the function Kg ðtÞ in the expression for the nonradiative transition rate. There we concluded that the energy gap hV was modified by the energy hvg of the promoting mode. Although our estimate is very crude, it suffices to show that expression (5.67) leads to a q0m -centroid, which order of magnitude is of the ðmÞ displacement parameters k12 . The procedure in the case of nontotally symmetry modes is similar and can be handled on the same footing. The relevant displacement parameters appearing in ð0Þ ð0Þ ðtÞNmð0Þ ðtÞ and Dð0Þ Equation 5.61 are now given by the products D g ðtÞN m ðtÞ, where g (see Equation 5.51) ( i iv1 h ð0Þ ð0Þ ð1Þ ð2Þ l N1 ðtÞ ¼ iv1 z1 H1 ðtÞ ð0Þ ðw11 þ w22 Þk12 ðw12 w21 b21 Þk12 B1 ð2Þ
ð2Þ
ðw12 þ w21 b21 Þk12 expðiv2 tÞ þ 2w12 k12 exp½iðv1 þ v2 Þt ð1Þ ð1Þ ð2Þ þ ½ðw11 þ w22 Þk12 ðw12 w21 b21 Þk12 expð2iv1 tÞðw12 w21 b21 Þk12 exp½ið2v1
) þ v2 Þt : ð5:68Þ
ð0Þ N2 ðtÞ
The second component is quite comparable to the first and is obtained from ð0Þ ðtÞ ðm ¼ 1; 2Þ are them by interchanging the indices 1 , 2. The expressions N m ð0Þ ðtÞ and (in the zero-temperature limit) given by closely related to H m ð0Þ ð0Þ ð0Þ ð0Þ ðtÞ ¼ ivs H N m m m ðtÞ. The corresponding prefactors Dg ðtÞ and Dg ðtÞ reduce on ð0Þ the same level of approximation to the results Dg ðtÞ ¼ ð1=2Þi h expðivg tÞ and ð0Þ ðtÞ the ð0Þ ðtÞ ¼ ð1=2Þih expðivg tÞ and cause apart of the factors Nmð0Þ ðtÞ and N D g m energy gap of hV to decrease additionally of about hvg . A comparison of expressions ð0Þ ð0Þ ð0Þ ð0Þ 0 ð0Þ ð 0Þ ð0Þ Hm ðtÞKg ðtÞ and H m ðtÞKg ðtÞ on the one side with Dg ðtÞNm ðtÞ and Dg ðtÞN m ðtÞ on the other indicates that the nontotally symmetric q0g can be as large as those for totally symmetric modes q0m . If the q-centroid for nontotally symmetric modes is large, the molecule is distorted by displacing the ion of the skeleton from the equilibrium positions (of high symmetry) to the q-centroid at considerably lower symmetry. At this unsymmetrized and distorted q-centroid configuration, the electronic wavefunctions will be deformed as well. Consequently, the electronic coupling terms in (5.61) and (5.62) enhance in a manner that can be quite difficult to deduce with any precision. With reference to the leading contribution of the nonradiative decay rate (Equation 5.8), one can expect an appreciable enhancement of the electronic matrix element evaluated at the q-centroid compared to the customary approach at qe resulting from a small (or rapidly varying) energy denominator Es ðq0 ÞEl ðq0 Þ of the electronic matrix elements (5.4). 2) Roughly speaking, the nonradiative decay rate increases as the energy gap decreases as one might expect from formula (4.111) for nonradiative transition in the displaced potential model.
j129
6 Time-Resolved Spectroscopy We have thus far analyzed the radiationless decay of a single excited state of a polyatomic molecule into a dense manifold of Born–Oppenheimer (BO) states, corresponding to another electronic configuration. Since the prepared zero-order excited state is induced by an electromagnetic field (i.e., by a broadband excitation), the decay by radiative transition of the excited state of the molecule should also be considered. This chapter mainly deals with a unified treatment of such a decay process, which includes the radiative transition to the lower electronic state as well. In this context, we follow here the treatment of Goldberger and Watson [81], Mower [80], and Freed and Jortner [144], which is based on the Greens function formalism for the transition amplitude. In this formalism, the states of interest are selected by suitable projection operators, which we have already used in Chapter 2 in the case of nonradiative transitions, and the matrix elements can be displayed in an energy representation, which involves either the BO or the molecular eigenstate (ME) basis set. In this chapter we shall also address ourselves to a theoretical study of coherent optical effects such as optical free induction decay and photon echo from an assembly of collision-free molecules. From the mathematical point of view, many of the formal manipulations are given in Appendix A.2.
6.1 Formal Consideration
Before discussing the interaction of a molecule with an electromagnetic field in detail, it is useful to review some formal facts about electromagnetic radiation. When radiative decay processes are considered, the molecular Hamiltonian of the system molecule plus radiation field is given by H ¼ Hel þ Hrad þ Hint ;
ð6:1Þ
Hel ¼ HBO þ Hv :
ð6:2Þ
where
The operator Hel or HBO is the Hamiltonian for the internal electronic states of the molecule (which include electronic, vibrational, and rotational states). If the initial
j 6 Time-Resolved Spectroscopy
130
basis set is chosen in terms of BO wavefunctions ðysv ; ylv0 Þ, then Hv is the intramolecular perturbation, the so-called Born–Oppenheimer coupling, which promotes transitions between (see the discussion in Section 1.1) potential energy surfaces. Alternatively, if we choose the molecular eigenstate yn as basis set (see Appendix F), then Hel yn ¼ En yn
ð6:3Þ
and the perturbation consists of Hint . Hrad in Equation 6.1 is the Hamiltonian of the free radiation field (see Appendix E): þ 1X þ Hrad ¼ ðkcÞ ak^ ð6:4Þ hvk^e ¼ ðckÞ ðc ¼ 3 1010 cm=sÞ; e ak^e þ ak^e ak^e ; 2 k;^e þ where ak^e and ak^ e are the respective operators for annihilation and creation of photons in the state ðk;^eÞ. The sum on k and ^e in Equation 6.4 extends over all plane wave momentum states k, and respectively over the two allowed directions of polarization of a photon having momentum k. The eigenfunctions of (6.4) in the Dirac notation are
j ¼ jnk1^e1 ; nk2^e2 ; . . . ; nke ; . . .i;
ð6:5Þ
where nk1 ;^e1 ; nk2 ;^e2 ; . . . represent a complete set of photon numbers that specify how many photons of each type are present. Hint is the radiation–matter interaction term taken as Hint ¼
Z X e pj Aðrj Þ; mc j¼1
ð6:6Þ
where e and m are the charge and mass of an electron. The summation in (6.6) extends over the coordinates rj and momentum pj of the Z electrons in the molecule. The quantity Aðrj Þ is the vector potential of the radiation field evaluated at rj . This vector potential may be expanded in a series of plane waves [145] (see Appendix E): AðrÞ ¼
i X 2ph2 c 1=2 h þ iðkrÞ= h ^e ak;^e eiðkrÞ=h þ ak;^ : ee Vk k;^e
ð6:7Þ
The sum on k here extends over all plane wave momentum states k in the cavity of þ volume V. The only nonvanishing matrix elements of ak;^e and ak;^ e are pffiffiffiffiffiffiffi nk1 ;^e1 ; nk2^e2 ; . . . ; nk;^e 1; . . . ak;^e nk1 ;^e1 ; nk2^e2 ; . . . ; nk;^e ; . . . ¼ nk;^e pffiffiffiffiffiffiffiffiffiffiffiffiffiffi ð6:8Þ nk ;^e ; nk ^e ; . . . ; nk;^e þ 1; . . . a þ nk ;^e ; nk ^e ; . . . ; nk;^e ; . . . ¼ nk;^e þ 1: 1
1
2 2
k;^e
1
1
2 2
In discussing the electromagnetic interaction of a charged particle with the radiation field, the zero-order states are taken as eigenstates of the Hamiltonian: H0 ¼ HBO þ Hrad :
ð6:9Þ
They include the vibronic state ys ¼ jys ; vaci, the zero-order approximation of the electronically excited state, which carries oscillator strength to the ground state and the vibronic manifold fyl g ¼ fjyl ; vacig. The vibronic manifold corresponds to a lower electronic state that are quasi-degenerate with ys and does not carry oscillator
6.2 Evaluation of the Radiative Decay Probability of a Prepared State
strength to the ground state yk;^e ¼ jy0 ; k;^ei, (jvaci is the zero photon state) (we revert here to the simple notations s for ðsvÞ and l for ðlv0 Þ). Using Equations (6.6–6.8), we find 0 11=2 * + 2 D E pe pffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi 2p h c y ; vac A nk;^e þ 1 yk;^e yk;^e jHint jys ; vac ¼ e@ Vk mc s 0
11=2 2 pffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi 2p h c A nk;^e þ 1 ¼ e@ Vk 0
1 + p^e s s j ðr; q Þ xsv ðq ÞA ; @x0v0 ðq Þ j0 ðr; q Þ mc s *
0
0
ð6:10Þ
q
PZ
where nk;^e ¼ 0 and p ¼ j¼1 pj . For optically allowed transitions, the electronic matrix element hj jir in (6.10) is usually a slowly varying function of the nuclear coordinates over the range where xs x0 significantly differs from zero. Therefore, it may be removed from the inner element of the nuclear integration by using the q-centroid-type approximation. To obtain (6.10), we have assumed that the electric dipole transition is allowed for the decay from state ys to the ground state y0 and set eikrj =h ¼ 1 in Equation 6.7. This is an excellent approximation for atomic transitions, since called long-wave approximation. 6.2 Evaluation of the Radiative Decay Probability of a Prepared State
Let us now consider a system consisting of a molecule plus an electromagnetic radiation field. The molecule is prepared by optical excitation at time t ¼ 0 in a nonstationary state of H, which may be expressed as a superposition of either the BO states fys ; yl g or the molecular eigenstates yn [144]: X X yð0Þ ¼ bs ð0Þjys ; vaci þ bl ð0Þjyl : vaci ¼ an ð0Þjyn : vaci: ð6:11Þ l6¼s
n
In many cases of physical interest, the initial excited state of the system can be prepared by coherent excitation, by broadband source, or by a square light pulse [146–149] (having a pulse length chosen so that t v1 , where v ¼ ck is the photon frequency),1) whereupon an ð0Þ ¼ hys jyn i; bl ð0Þ ¼ dls . In this case, the completeness 1) It is well known that by the uncertainty principle, a finite pulse length t gives rise to an energy spread DE h=t in the incident light. In this case, it is suitable to employ a wave packet formulation to provide the correct analysis of the system. The importance of using photon wave packets to provide a physically realistic model for the excitation process has been emphasized by Jortner and Mukamel [146] and
Freed [149]. Furthermore, Jortner and Mukamel discussed how no extra molecular information can be gained by altering the nature of the incident wave packet, so the reader is referred to their work for more details. The idealized square pulse employed here omits such energy spread and its simplicity enables the elucidation of the fundamental molecular phenomena we wish to illustrate.
j131
j 6 Time-Resolved Spectroscopy
132
of the molecular basis set for the excited states and the fact that ys is the only state that carries oscillator strength immediately imply that yð0Þ ¼ jys ; vaci. When narrow-band excitation is used (i.e., by using nanosecond lasers), the bl ð0Þ are not necessarily nonzero and bs ð0Þ can be greatly reduced, so the contributions of bl ð0Þ to the radiative decay should also be considered. After a time t has evolved, the state of the system is determined by the Hamiltonian (6.1) according to the expression2) yðtÞ ¼ expðitHÞyð0Þ:
ð6:12Þ
The probability P of finding the system in the one-photon ground state yk;^e ¼ jy0 : k; ^ei is Pk;^e ðtÞ ¼ jhyk;^e jjyðtÞij2 ¼ jhyk;^e jexpðitHÞyð0Þij2 :
ð6:13Þ
Using Equation 6.11, Equation 6.13 can be written as X Pk;^e ðtÞ ¼ hyk;^e jexpðiHtÞjyj ; vacibj ð0Þhyk;^e jexpðiHtÞjyj0 ; vaci bj0 ð0Þ j;j0 ¼s;l
X ¼ hyk;^e jexpðiHtÞjyn ;vacian ð0Þhyk;^e jexpðiHtÞjyn0 ; vaci an0 ð0Þ; n;n0
ð6:14Þ
where for the case of broadband excitation, the coefficients may simply be taken as bj ð0Þ ¼ djs : Otherwise, there is possibility of interference between the different states, ys and yl , as many of them come close together and may be strongly coupled. The nonzero matrix elements of H in the basis set ðys ;yl Þ and yk;^e ¼ jy0 ;k;^ei are given by hyk;^e jH jyk0 ;^e0 i ¼ ðE0 þ kcÞdkk0 d^e^e0 ;
ð6:15aÞ
hys jHjyl i ¼ hys jHv jyl i ¼ Vsl ;
ð6:15bÞ
hyk;^e jH jys i ¼ hyk;^e jHint jys i ¼ Ws;k^e ;
ð6:15cÞ
hys jHjys i ¼ Es ;
ð6:15dÞ
hyl jHjyl0 i ¼ El dll0 ;
ð6:15eÞ
where Ws;k;^e is given by Equation 6.10 and E0 ; Es , and El are respectively the energies of y0 ; ys ; and yl in the absence of the external radiation field. Using the technique of Chapter 2 and considering for simplicity the classic case of broadband excitation for which yð0Þ ¼ jys ;vaci, we define the projection operator P ¼ jys ; vacihys ;vacj 2) In this chapter we return to our convention by which we set h ¼ 1.
ð6:16Þ
6.2 Evaluation of the Radiative Decay Probability of a Prepared State
and the projection operator on all other states separated from the state jys ;vaci Q ¼ 1P:
ð6:17Þ
Thus, to find the transition probability Pk;^e ðtÞ, we need the matrix element for the time evolution of the P ! Q excitation, hyk;^e jGðEÞjys : vaci ¼ hyk;^e jQGðEÞP jys ; vaci;
ð6:18Þ
or more explicitly the amplitude for the transition, Is;k;^e ðtÞ ¼ hyk;^e jexpðiHtÞjys ; vaci ð 1 ¼ hyk;^e jQGðEÞPjys ; vaciexpðiEtÞdE; 2pi
ð6:19Þ
c
where the contour c runs from þ ¥ to ¥ over the singularities of GðEÞ, above the real axis. As given in Equation A16b, QGðEÞP ¼ ðEQH0 QÞ1 QRðEÞP½EPH0 PPRðEÞP1 ;
ð6:20Þ
where H ¼ H0 þ V;
ð6:21aÞ
H0 ¼ HBO þ Hrad ;
ð6:21bÞ
with
and the perturbation V ¼ Hv þHint ;
ð6:21cÞ
responsible for the decay. RðEÞ in Equation 6.20 is the level shift operator given by Equation A15. Now, the electromagnetic interaction of a molecule with the radiation field is weak in the sense that virtual transitions involving the emission of photons contribute very little to the decay rates. This means that we may evaluate the matrix element in Equation 6.19 in the lowest order perturbation theory. Then according to Equation 6.20, hyk;^e jGðEÞjys ; vaci ¼ hyk;^e jQGðEÞP jys : vaci
1 1 1 ¼ ðEE0 kcÞ hyk;^e jHint jys : vaci EE s þ i ðCs ðEÞ þ Ds ðEÞÞ ; 2
ð6:22Þ
where we have set Rss ðEÞ ¼ Ds ðEÞi½CðEÞ þDs ðEÞ=2 for the matrix element of the level shift operator. The real level shifts of the matrix element Rss , which represents s, have the shift between the unperturbed energy Es and the perturbed energy E
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j 6 Time-Resolved Spectroscopy
134
s ¼ Es þDI þ DII .3) The latter represents the difference between the been included in E s s actual eigenvalues of H and the unperturbed eigenvalue Es . The term Ds ðEÞ is the damping of jys : vaci due to vibronic coupling (6.15b) with the manifold fjyl ;vacig4) and is given (see Appendix A.2) by a superposition of Lorentzians (each characterized by the strength jVsl j2 and the width Cl ) of yl : Ds ðEÞ ¼ 2
X
jVsl j2 Cl ðEÞ=2
l
ðEEl Þ2 þ ½Cl ðEÞ=22
:
ð6:23aÞ
Note that the widths Cl are very small as the levels of fyl g do not carry oscillator strength. In the statistical limit when the density rl of vibronic states fyl g is sufficiently large to exceed the reciprocal of the vibronic terms Vsl between the BO states, rl V 1, considerable configuration mixing Ð occurs. In this limit, we may P replace the sum over l by an integral using l ! dEl rl ðEl Þ. Thus, (6.23a) becomes valid in the limit of small Cl ðEÞ ! 0: ð ðCl ðEÞ=2Þ Ds ðEs Þ ¼ 2 dEl jVsl j2 rl ðEl Þ: ð6:23bÞ ðEs El Þ2 þ½Cl ðEÞ=22 Since Vsl ðEÞ and the density of states of fyl g, rl ðEl Þ, are rather slowly varying in large molecules for E ¼ Es, the width Ds ðEÞ is a smooth function of energy. Alternatively, a general condition for the smoothness of Ds ðEÞ is that the widths of successive Lorentzians considerably exceed their spacing. The term Cs in Equation 6.22 is the radiation damping associated with the decay of the initial state ys . That is, as the system radiates outgoing waves into the decay channel of yk;^e , the original state becomes depleted and this leads to a self-damping of the radiative process given by the imaginary part of the operator Rss (see Appendix A.2): Xð 2 dVk yk;^e Hint ys rph ðvph Þ; Cs ¼ 2p ð6:24Þ ^e
P Ð where rðvph Þ is the density of photon states of a given polarization ^e and ^e dVk corresponds to the integration over all propagation direction in k space directed into the solid angle Vk and summation over the two polarizations of each k. We have seen from Equation 6.22 that the matrix element of the Greens operator yk;^e jGðEÞjys ;vaci is analytic everywhere in the complex plane, except on the complex pole s i 1 ðCs þ Ds Þ; E ¼E 2
ð6:25Þ
which is situated on the second Riemann sheet Im E < 0 and along the cut extending from E0 to plus infinity on the real axis. Provided that the width ðCs ðEÞ þ Ds ðEÞÞ is a 3) The quantities DIs and DII s are numerically much smaller than Es . 4) We write the damping of the state ys due to the vibronic coupling now by Ds rather than Cs as before in chapter 2. Here Cs is the damping of ys due to the interaction with the radiation field and the remaining notation is that of the previous sections.
6.2 Evaluation of the Radiative Decay Probability of a Prepared State
smooth function of E for E ffi Es ffi E0 þkc, Equation 6.25 is the only complex pole. Making the following partial fraction decomposition 1 1 s þ iðCs þ Ds Þ=2 ¼ ½E0 þkcE s þ iðCs þ Ds Þ=2 ðEE0 kcÞ½EE 1 1 s þ iðCs þ Ds Þ=2 EE0 kc EE ð6:26Þ
and ignoring the contribution from the branch cut E > E0 , the transition amplitude is found simply by completing the contour in the lower half-plane and evaluating the integral in ð eiEt hyk;^e jHint jys ;vaci 1 Is;k;^e ðtÞ ¼ dE s þ iðCs þ Ds Þ=2 ; 2pi c ðEE0 kcÞ½EE
ð6:27aÞ
in terms of residue at the pole given by Equation 6.25. Thus, we find Is;k;^e ðtÞ ¼
s iðCs þ Ds Þ=2tg hyk;^e jHint jys ; vaci exp½iðE0 þ kcÞtexpfi½E ; s þ iðCs þ Ds Þ=2 ½E0 þ kcE ð6:27bÞ
and by taking the absolute value squared y Hint y ; vac 2 k;^e s Pk;^e ðtÞ ¼ s Þ2 þ 1 ½Cs ðEs Þ þDs ðEs Þ2 ðE0 þ kcE 4
1 s Þ t þ exp½ðCs þ Ds Þt ; 12exp ðCs þDs Þt cosðE0 þkcE 2 ð6:28Þ
where Pk;^e ðtÞ is the probability of finding the system in the state yk;^e at time t. On integrating the integral (6.27) by contour analysis, it is necessary to continue analytically the matrix element of the level shift operator Rs ðEÞ from the first Riemann sheet through the cut onto the second sheet. This may be accomplished by defining the value of the level shift operator on the second sheet as I RII s ðEieÞ ¼ Rs ðE þ ieÞ ¼ Ds ðEÞi½Cs ðEÞ þ Ds ðEÞ=2;
where the complex energy near the cut E > E0 is E ie ðe > 0Þ. The superscripts on Rs denote the sheet on which the level shift operator is to be evaluated. With this definition in mind, the matrix element of the Greens function in (6.27a) is analytic everywhere in the complex plane except on the cut along the real axis E > E0 and the pole (6.25) that is situated on the second Riemann sheet. Having performed the analytical continuation of Rs , we may now deform the contour of integration c (that
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runs from þ ¥ to ¥ above the real axis along which the singularities of RðEÞ lie) in the integral (6.27a) by bending it to the left of E0 down along the first sheet to E ¼ E0 i¥. The contour to the right of E ¼ E0 may be deformed in a similar manner, provided that we pass through the cut onto the second sheet. In addition, a small circular contour c0 encloses the poles of the singularities at E ¼ EiðC s þ Ds Þ=2 on the second sheet. The resulting expression for Is;k^e consists of two contour integrals, one about the new deformed cut c1 (extending from E0 to E ¼ E0 i¥) as well as the contour encompassing the singularities of the integrand, ð ð 1 ð ÞdE: Is;k^e ¼ þ 2pi c0 c1 Following the procedure of Goldberger and Watson (see also Mower [80]), it can be shown that the contribution of the integral around c1 is of negligible magnitude and can therefore ordinarily be neglected. Let us now return to our problem of evaluating the probability of emission. Integrating Equation 6.28 over frequencies kc, all propagation directions in k space, and summation over the polarizations ^e, we obtain [144] Pemission ðtÞ ¼
Cs ðEs Þ f1expð½Cs ðEs Þ þ Ds ðEs ÞtÞg; ½Cs ðEs Þ þ Ds ðEs Þ
where we have used the familar relations ð dðkcÞ 2p ¼ s Þ2 þ 1 ðCs þ Ds Þ2 Cs þ Ds ðE0 þ kcE 4
ð6:29Þ
ð6:30aÞ
and ð
s Þt dðkcÞcos½ðE0 þ kcE 2p 1 ¼ exp þ D Þt : ðC s s s Þ2 þ 1 ðCs þ Ds Þ2 Cs þ Ds 2 ðE0 þ kcE 4
ð6:30bÞ
The last integral is evaluated in terms of residue at the pole E0 þ kc ¼ s i=2ðCs þ Ds Þ. With the formula (6.29), we have established a relation between E the decay rate of a prepared unstable state and its lifetime in the statistical limit. Equation 6.29 describes an exponential decay with quantum yield Pð¥Þ ¼ Cs =ðCs þ Ds Þ. The lifetime of the state is the reciprocal of ðCs þ Ds Þ, which consists of independent contributions of radiative and nonradiative components. Thus, the initially prepared resonance state ys subjected to a coupling scheme represented by Figure 2.1 decays exponentially by radiative and nonradiative transihr. tions on the timescale that is appreciably shorter than the recurrence time trec The photon continuum allows the irreversible radiative decay, the states fyl g act as an effective continuum that enables irreversible decay into this manifold. The probability of finding the molecule in the fyl g manifold at time t, complementary to (6.29), is given by Pl ðtÞ ¼
Ds f1exp½ðCs þ Ds Þtg ðCs þ Ds Þ
ð6:31Þ
6.3 The Sparse Intermediate Case
and the probability that the molecule remains in its initial state jys ; vaci is 1Pemission ðtÞPl ðtÞ ¼ exp½ðCs þ Ds Þt:
ð6:32Þ
We conclude that a simple exponential decay is an adequate description of the time dependence of Pemission ðtÞ provided that coupling between all resonance levels (or optically active zero-order states) undergoing transitions may be ignored. The radiative damping matrix C is of greater importance for discussing radiative transitions and is closely related to the Fermi Golden Rule. It is defined in a manner that accounts for some type of interference effects (i.e., anticrossing-type interference effects): XXð dVk hajHint jy0 ; k; ^eihy0 ; k; ^ejHint ja0 irph ðckÞ: Caa0 ðEÞ ¼ 2p ð6:33Þ a
^e
In Equation 6.33, there is a sum over the zero-photon excited states a (after radiative decay) as well as a sum over the polarization^e and an integration over the direction Vk of the emitted photon. rph ðckÞ is the density of photon states. CðEÞ is generally nondiagonal, as will be illustrated in the next section. In the fys ; yl g representation however, it is easy to verify from Equation 6.15 that Css ¼ Cs 6¼ 0 Csl ¼ Cll0 ¼ 0
ð6:34Þ
for all l; l0 . Hence, C is diagonal in this basis. However, in another basis set, that is, a superposition of the zero-order states fys ; yl g, the C undergoes a unitary transformation and (6.33) is no longer diagonal. Molecular eigenstates (see Appendix F) provide an important illustration of this. For a single resonance, the resonance width is given by Caa. The off-diagonal matrix element of C represents coupling between the states ja; vaci via the one-photon states: ja; vaci ! jy0 ; k; ^ei ! ja0 ; vaci:
The off-diagonal contribution will be important only in the case of near-degeneracy when these terms are comparable to the energy spacing between the energy levels, that is, Caa0 jEa Ea0 j
ð6:35Þ 0
In such a case, it is known [80, 144] that the two states jai and ja i do not decay independently and the radiation coupling leads to a mixing of states.
6.3 The Sparse Intermediate Case 6.3.1 Preliminary Consideration
As we have already mentioned, in the statistical limit where the density of states is very large relative to the infrared or radiative decay width of the background states fyl g,
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Cl rl 1;
the function Ds ðEÞ is smooth and independent of the widths fCl g. In such a case, the adiabatic scheme is a good approximation for describing the bound-level structure of molecules. Large organic molecules (e.g., naphthalene, anthracene, tetracene [150], phenantren [150–152], therphenyl [154], and phentacene [155]) and a large group of inorganic transition ion complexes [156–162] fall in this category. For small molecules and also in the so-called sparse intermediate case, the vibronic coupling matrix element Vsl is sufficiently large (due to favorable Franck–Condon factor) and/or the level density rl is rather small. Consequently, the separation of the states may exceed their widths 1 jEl El0 j > ðCl Cl0 Þ 2
for adjacent levels in the fyl g manifold. In this case, DðEÞ is no longer expected to be a smooth function of energy E in the range of interest and the relevant matrix element of the Greens function may be characterized by more than a single complex pole, resulting in an extensive mixing of states. In addition, the typical recurrence times trec ¼ hrl [11] for the occurrence of relaxation processes are now very short. In such a case, due to rapid recurrence between the states ys and fyl g, the adiabatic picture is physically meaningless and the experimental timescale for the fluorescence detection considerably exceeds the conveniently called Poincare recurrence time trec tmax . The molecule may resonate many times between fyl g and ys within a timescale characterized by the recurrence time. Typical molecules in this group are SO2 ; NO2 , and CS2 . The density of vibronic states (corresponding to the ground state and the first triplet state), which are quasi-degenerate with excited singlet state, is very low, being of the order of 0:1 cm1 . It has been experimentally demonstrated that the first excited singlet of SO2 ; NO2 , and CS2 exhibit anomalously long radiative lifetimes [163, 164], which are considerably longer than those expected on the basis of integrated oscillator strength. Furthermore, it was observed that the absorption spectra of these molecules are very complex, consisting of a large number of lines that are spread out over more than 150 cm1 and that could not be assigned to the vibrational–rotational manifold of a single electronic state. It was suggested by Douglas that this situation is characteristic of intramolecular vibronic coupling in these molecules. This results in the redistribution of the intensity of a zero-order BO state (corresponding to the excited singlet) among a large number of zero-order levels. These are quasi-degenerate with the former level and do not carry oscillator strength. From the spectroscopic point of view, the redistribution of the intensity of the zero-order component ys induces the appearance of many new well-resolved lines corresponding to all the molecular eigenstates yn in the optical spectrum (Figure 6.1). With this observation in mind, in this case it is more convenient to use the molecular eigenstate basis fyn g in the following section (see also Appendix F).
6.3 The Sparse Intermediate Case
V {|l >}
|s>
hω
Radiative Coupling
{|n>}
hω
|0>
|0>
(a) BO Zero-Order States
(b) Molecular Eigenstates
Figure 6.1 The Bixon and Jortner model [11] to describe the intrastate coupling and intramolecular vibrational redistribution. The zero-order molecular levels j0i, jsi, and fjlig are BO states for intrastate dynamics. They correspond, respectively, to the ground state j0i, the (one-photon) optically accessible doorway state jsi, and the background manifold
Radiative Coupling
fjlig. The wave lines represent the intramolecular interstate and intrastate coupling. The molecular eigenstates jni diagonalize the molecular Hamiltonian and are all radiatively coupled to the ground state. They are generally unevenly spaced and exhibit irregular variation in the radiative coupling with the ground state j0i.
6.3.2 The Molecular Eigenstates
As mentioned previously for the case in which the set of coupled states is a finite small number, the projection P takes the form (in terms of diagonalized projections) X P¼ ð6:36Þ jyn : vacihyn ; vacj; n
where Hel jyn i ¼ En jyn i:
The variable n as well as its range depends on the type of problem to be considered. The projection operator on the other states is Q ¼ 1P:
ð6:37Þ
The actual matrix elements are now D E yk;^e jGðEÞjyn ; vac ¼ hy0 ; k; ^ejQGðEÞP jyn ; vaci;
ð6:38Þ
and, as previously discussed in Section 6.1, the Hamiltonian of the system being considered is H ¼ H0 þ V; where now
H0 ¼ Hel þ Hrad ;
ð6:39aÞ ð6:39bÞ
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Hel ¼ HBO þ Hv ;
with
ð6:39cÞ
and the interaction V ¼ Hint :
ð6:39dÞ
The projection QGðEÞP is again given by (6.20). However, now hy0 ; k; ^ejQRðEÞPjyn i ¼ hy0 ; k; ^ejHint jyn ; vaci ¼ hy0 ; k; ^ejHint jys ; vacihys jyn i
ð6:40Þ
and PRðEÞP iPCP=2;
ð6:41Þ
where PCP is the radiative damping matrix in the fyn g basis, which is nondiagonal as discussed above. Using Equations 6.40 and 6.41 and the expression for QGðEÞP given by Equation 6.22 leads to P hy0 ; k; ^ejQGðEÞPjyn ; vaci ðEE0 kcÞ1 n0 hy0 ; k; ^ejHint jyn0 ; vaci yn0 ; vacj½EPH0 P þ iPCP=21 yn ; vac ; ð6:42Þ P where PH0 P ¼ n jyn ; vaciEn hyn ; vacj. Note that the last term in (6.42) is the inverse of the effective Hamiltonian (EH) Heff ¼ Hel iC=2:
ð6:43Þ
In the matrix form, Equation 6.43 becomes
Heff ¼
k
E1 iC1 =2 iC12 =2 .. . .. .
k
.. .. . . .. .. E2 iC2 =2 . . .. .. . . ; .. .. . . iC12 =2
so Hel is diagonal while the damping matrix is nondiagonal. On the contrary, in the BO basis, the effective Hamiltonian is
Heff
k
Es iCs =2 Vs1 Vs2 .. ¼ .
Vs1 E1
Vs2 E2
k
:
Now Hel is off-diagonal, while the damping matrix is diagonal [165]. For the case in which the set of closely coupled states fyn g is a finite number, the matrix elements of the inverse of the operator ½EPH0 P þ ði=2ÞPCP1 may be written formally as ½EPH0 P þ iPCP=21 ¼
cofactor½EPH0 P þ iPCP=2nn0 : Det½EPH0 P þ iPCP=2
ð6:44Þ
6.3 The Sparse Intermediate Case
If the number of closely coupled states is two, then the above matrix element reduces to hy0 ; k;^ejQGðEÞP jyn ; vaci ¼
hy0 ; k;^ejHint jyn ; vaci½EEn0 þ iCn0 n0 =2 þ hy0 ; k;^ejHint jyn0 ; vaciðiCnn0 =2Þ : ðEE0 kcÞf½EEn þ iCnn =2½EEn0 þ iCn0 n0 =2 þ C2nn0 =4g ð6:45Þ
It often happens that in studying a given transition, we find a single predominant contribution. This takes place if we stipulate that the molecular eigenstates are very sparse in the sense that En En0 Cnn0 :
ð6:46aÞ
The off-diagonal parts of CðEÞ in (6.45) can then be neglected and we obtain the simple result hy0 ; k;^ejQGðEÞPjyn ; vaci ¼
hy0 ; k;^ejHint jyn ; vaci ; ðEE0 kcÞ½EEn þ iCnn =2
ð6:47Þ
and correspondingly for hy0 ; k;^ejQGðEÞPjyn0 ; vaci. In this case, the radiative decay rate of the system is characterized by a superposition of exponentials with the widths Cnn and Cn0 n0 , provided that Cnn and Cn0 n0 are slowly varying for E E0 þ kc. Furthermore, in this case, if the condition 1 En En0 ðCnn Cn0 n0 Þ 2
ð6:46bÞ
holds sufficiently, we can expect that the level crossing-type interference terms in (6.45) for ðn 6¼ n0 Þ are negligible and the molecular eigenstates decay independently with the widths Cnn and Cn0 n0 . A more general case for finite numbers n will be discussed in Section 7.5. Since the trace of the matrix C is invariant with respect to the basis set (Tr C in fys ; yl g basis ¼ Tr C in fyn g basis), the width Cs is given by Cs ¼
X n
Cnn ;
ð6:48Þ
so Cnn < Cs
for all n:
ð6:49Þ
Since the lifetime of the molecular eigenstates tn ¼ 1=Cnn , tn ¼ 1=Cnn > 1=Cs ¼ ts :
ð6:50Þ
This is the explanation for the anomalously long lifetime of small triatomic molecules observed by Douglas [163, 164]. Ordinarily, when conditions (6.46) are not satisfied
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for some of the states fyn g (for example, for closely spaced states), these states exhibit level anticrossing-type interference [166–168]. However, as shown by Bixon and Jortner [169], in the statistical limit, when the density of states rl is sufficiently high to exceed the reciprocal of the vibronic coupling term V between the zero-order BO states, that is, rl V 1, the result (6.29) is still obtained for broadband excitation even though the fyn g interfere with each other.
6.4 Radiative Decay in Internal Conversion by Introduction of Decay Rates for {c1}
In Section 6.2, we have described the decay of a single resonance that is coupled (apart from a radiation field) to a dense manifold of BO states fyl g that do not carry oscillator strength to the ground state y0 in view of spin selection rules (when the manifold fyl g is a triplet). However, when the BO states fyl g are singlets, they do carry oscillator strength to high vibrational levels of the ground electronic state yv0 . This will in general mean that we are now concerned with a situation where both ys and fyl g carry oscillator strength. Now, just as was done in Section 6.2, the initial state is taken as jys ; vaci, resulting from broadband excitation. Again, using Equation 6.18, the matrix elements of D
E D E yvk;^e jGðEÞjys ; vac ¼ yvk;^e jQGðEÞP jys ; vac
ð6:51Þ
E must be considered, since emission may also occur to yv0 , where yvk;^e ¼ yv0 ; k; ^e and P is again given as in Equation 6.16. We shall choose the label v to distinguish between transitions in the state yv0 and y0 . For the case in which fyl g form a dense manifold (see Equation 6.23), ð DðEÞ ¼ 2 dEl jVsl j2
Cl =2 ðEEl Þ2 þ ðCl =2Þ2
rl ðEl Þ;
ð6:52Þ
where rl is again the density of BO states fyl g. Cl ðEÞ are radiative widths due to the spontaneous emission given by Cl ðEÞ ¼ 2p
Xð ^e
D E2 dVk yvk;^e jHint jyl rph ðEE0v Þ;
ð6:53Þ
where it has been assumed that the damping matrix Cll0 is diagonal in the basis fyl g (see Equation 6.15). DðEÞ; Cl ðEÞ and Cs ðEÞ, as defined in Section 6.2, can all be considered to be smooth functions of E. Let us now turn to the problem of resolving the matrix element (6.51), which as in Section 6.2 can be written as D E ðEE0v kcÞ1 yvk;^e jQRðEÞP jys ; vac ðEEs þ i½Cs ðEÞ þ DðEÞ=2Þ1 :
ð6:54Þ
6.4 Radiative Decay in Internal Conversion by Introduction of Decay Rates for {y1}
But now since fyl g carry oscillator strength, the matrix element (6.54) may be decomposed into matrix elements for states jys i and jyl i: D
E v yvk;^e jHint jyl ; vac ¼ Wk;^ e ð1dv0 Þ;
ð6:55aÞ
D
E yvk;^e jHint jys ; vac ¼ Wk;^e dv0 ;
ð6:55bÞ
where dv0 is the Kronecker delta defined by dv0 ¼
0; 1;
if v 6¼ 0; if v ¼ 0:
With the aid of the identity RðEÞ ¼ V þ VQðEQHQÞ1 QV, the matrix element of QRðEÞP that describes the emission to both yv0 and y0 states may be written in compact form D
E X yvk;^e jQRðEÞP jys ; vac ¼ Wk;^e dv0 þ W v V ð1dv0 Þ½EEl þ iCl ðEÞ=21 ; l k;^e ls ð6:56Þ
where Vls ¼ hyl jHjys i. Combining Equations 6.56 and 6.54, we obtain by counterintegration (neglecting as in Section 6.2 the contribution from the branch cut E > E0 ) D
E exp½iðE0 þ kcÞtexpfi½Es iðCs þ DÞ=2tg yk;^e jexpðiHtÞjys ; vac ¼ Wk;^e E0 þ kcEs þ iðCs þ DÞ=2 ð6:57aÞ
and [144] D
E P v yvk;^e jexpðiHtÞjys ; vac ¼ l Wk;^ e Vls
exp½iðE0 þ kcÞt Es El þ iðCl Cs DÞ=2
0 1expfi½Es E0n kciðCs þ DÞ=2tg @ E0v þ kcEs þ iðCs þ DÞ=2
! 1expfi½El E0n kciCl =2tg ; E0v þ kcEl þ iCl =2
ð6:57bÞ
where Cs ; D, and Cl can all be taken as CðE0 þ kcÞ in (6.57a) and CðE0v þ kcÞ in Equation 6.57b. Equation 6.57a is, of course, exactly equivalent to Equation 6.27b. In analogy with Equation 6.31, the fluorescence probabilities are obtained from Equation 6.57, by taking the absolute value squared, integrating over all energies, all directions in the angle Vk , and polarizations ^e, giving finally P0 ðtÞ ¼
Cs 1exp½ðCs þ DÞt Cs þ D
ð6:58aÞ
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and Pv ðtÞ ¼
2 X
1exp½iðCs þ DÞt X hy jy ij2 1expðCl tÞ ij C þ hy y l l s l s l l Cs þ D 0 1 1exp½ðC þ D þ C Þt=2 þ iðE E Þt s s l l 2 A; C hyl jys ij Re@ l l ðCs þ D þ Cl Þ=2 þ iðEl Es Þ
X
þ2
ð6:58bÞ
where (compare Equation F17) jhyl jys ij2 ¼ jVsl j2 =½ðEs El Þ2 þ ðCs þ DCl Þ2 =4
ð6:59Þ
is the component of ys in the molecular eigenstate yl . An important simplification of Equation 6.58b results in the statistical limit, where Ð P ! dE r ðE Þ and if we make the simple approximation that Cl is a constant. In l l l l this case, we may use Equation 6.52 to write Equation 6.58b in the form Pv ðtÞ ¼ Cl D
1exp½ðCs þ DÞt 1expðCl tÞ 1exp½ðCs þ DÞt þD þ 2Cl D : ðCs þ DÞðCs þ DCl Þ ðCs þ DCl Þ ðCs þ DCl Þ2 ð6:60Þ
The decay probability to the lowest vibronic level of the ground electronic state is determined by the branching ratio Cs =ðCs þ DÞ and by the lifetime ðCs þ DÞ1 . The close similarity between Equations 6.58a and 6.29 should be noted. The resonance fluorescence is expected to be very weak in view of the small branching ratio Cs =ðCs þ DÞ 104 . Reference to Equation 6.58b (or to Equation 6.60) shows that the fluorescence probability to higher vibronic levels consists of three contributions that involve two direct decay terms and an interference term: (a) The first term in Equation 6.60 describes an initial decay rate (for t ! 0) that is proportional to Cl . For a long time, this term exhibits a fast decay with a lifetime of ðCs þ DÞ1 , which arises from the fact that the molecular eigenstate yn that is primarily ys and has a width ðCs þ DÞ contains some fyl g. For this long timescale, the contribution from this term is negligible and the fluorescence is expected to be of order Cl =D, as for internal conversion between singlet states Cs D and Cl D. (b) The second term in Equations 6.58b and 6.60 corresponds to the direct radiation decay of the manifold fyl g, which is determined by the lifetimes fCl g of the fyl g states. For longer times, this term dominates the direct decay term (a). The fluorescence yield to the highly vibrationally excited ground state is close to unity. (c) The third contribution to the decay probability arises from level-crossing terms, which in the statistical limit gives a small contribution that is similar in form to (a). The radiative decay of the manifold fyl g exhibits interference effects in the intermediate case, where some of the states yl in the manifold fyl g couple to ys with different efficiency [144]. Equations 6.58b, 5.59b, and 6.60 have been of considerable importance in studying the radiative decay to higher vibronic components of the ground electronic state, which do not exactly overlap the fluorescence spectrum of the first excited
6.5 Dephasing and Relaxation in Molecular Systems
singlet state. This decay is also expected to reveal the interference effects between closely spaced states fyl g. The detailed features of this interesting new effect are of course determined by the details of the excitation process (i.e., narrow versus broadband excitation).
6.5 Dephasing and Relaxation in Molecular Systems 6.5.1 Introduction
We shall see in Chapter 7 that well-resolved sharp lines spectra of molecules can be obtained by incorporating them in suitable crystals. From such spectra, information about the interactions (vibronic coupling and spin–orbit coupling) and geometries (distortion) in the excited electronic state may be obtained. The results of these studies apply generally to static properties of the molecules, though the spectra also yield some information about relaxation phenomena. New developments in studying the dynamic interactions in such systems have occurred since the mid-eighties. These were mainly due to the use of tunable dye lasers, yielding time-resolved spectra. These were specifically important in the understanding of the dephasing processes in molecular mixed crystals, in particular those occurring on an ultrafast (picosecond) timescale. It is well known that by the uncertainty principle, the time-dependent processes give rise to the finite linewidth of an optical transition [170]. This homogeneous linewidth, however, can seldom be observed since crystal strain induces a spread in resonance frequencies, which exceeds in most cases the homogeneous width. The spectral line is then inhomogeneously broadened. The relaxation processes responsible for the homogeneous linewidth can be classified into two categories (in analogy with the longitudinal and transversal relaxation in magnetic resonance spectroscopy, see below). The processes with transfer of energy from the molecule to the surroundings (the bath) are called T1 processes. Fluorescence, internal conversion, and intersystem crossing fall in this category. The other types of relaxation processes are the pure dephasing T2 processes. Here the bath induces a random fluctuation of the transition frequency, but no energy is lost or transferred. By studying T2 -type processes, information about the interaction between the molecule and its environment (e.g., the phonons and transfer of excitation energy) can be obtained and the homogeneous from the inhomogeneous contribution of the fluorescence line can be separated. Dephasing can be studied either in the time domain (photon echo PE [171, 172], optical free induction decay (OFID) [173, 174] or in the frequency domain (hole burning) [175–177]. With these techniques, the homogeneous broadening can be circumvented and the pure homogeneous width can be measured. Dephasing processes were intensively studied by investigating the dynamics of the excited S1 state of pentacene (or strictly of the S1 S0 transition of pentacene)
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in p-terphenyl and other molecular mixed crystals such as pentacene in naphthalene and zinc porphin in n-octane [178–184]. The system pentacene in p-terphenyl and pentacene in naphthalene proved to be good candidates for a detailed study, since the local phonons, responsible for the dephasing, can be observed directly in the electronic spectrum [181, 155]. 6.5.2 Interaction of a Large Molecule with a Light Pulse
As mentioned above, inhomogeneous broadening in molecular solids originates from the difference in the local crystal field acting on the molecules, while in the gas phase, differences in the velocity are responsible (Doppler effect). One of the methods for separating the homogeneous from the inhomogeneous contributions in the time domain is the OFID method. In this technique, the homogeneous broadening is removed by exciting an optically selected Born–Oppenheimer state with a laser pulse. For the optical phenomena of such type, Jortner and Kommandeur [185] have presented a theoretical study based on a generalized effective Hamiltonian (GEH) to account for the temporal characteristic of the macroscopic polarization of an assembly of isolated large molecules exposed to a short optical pulse. In the following, a brief description of this theory is given. Before describing the OFID method further, it is perhaps worth to consider a more systematic treatment for the interaction of a molecule with an electromagnetic field. The physical approximations underlying this analysis are no more rigorous or sophisticated than those used in the chapter before, merely more precisely stated. We consider a level scheme consisting of the ground state j g i ¼ j0i and a single doorway state jsi, which is coupled via nonadiabatic intramolecular interactions to a manifold of background states fjlig and where both the state jsi and the manifold fjlig are characterized by the radiative and nonradiative decay widths cs and cl , respectively (see Figure 6.2). The corresponding molecular eigenstates j ji for the problem of interest are obtained from the diagonalization of the effective Hamiltonian
Heff ¼
k
Eg 0 0 0 .. . .. .
.. . .. . Es ics =2 Vsl Vsl0 .. Vsl El icl =2 0 . .. Vsl0 0 El0 icl0 =2 . .. .. .. .. . . . . .. .. .. .. . . . . 0
0
0
.. . .. . .. . .. . .. . .. .
k
ð6:61Þ
for which the levels in Figure 6.2 are the eigenfunctions j ji. They are in general unevenly spaced and exhibit irregular variations in the radiative coupling with the ground state j g i, so at first sight it does not seem worthwhile to observe phase coherence effects in such system.
6.5 Dephasing and Relaxation in Molecular Systems
γl
γj
{|l >}
{|j >}
Vsl |s > γs
γj Radiative Coupling
γl hω
Radiative Coupling
hω Diagonalize Heff
|0>
|0>
(a) BO Zero-Order States
(b) Generalized Molecular Eigenstates
Figure 6.2 Schematic picture of the effective Hamiltonian. The zero-order states jsi and fjlig are characterized by the energies Es and fEl g, respectively, and by the decay widths cs and fcl g. Vsl represents the intramolecular coupling between the doorway state jsi and the fjlig
manifold. Diagonalization of the effective Hamiltonian results in a set of independently decaying generalized molecular eigenstates fj jig, characterized by energies fEj g and decay widths fcj g.
To consider the response of an assembly of isolated molecules to a short optical pulse of duration Dt, the Hamiltonian for the system must be modified as follows: cos vt; H ¼ Hm ~ m gs E H ¼ Hm ;
0 t Dt; t 0; t Dt;
ð6:62Þ
where Hm is the molecular Hamiltonian, ~ E is the local electromagnetic field, characterized by the frequency v, while ~ m denotes the dipole operator. The time evolution of the levels j g i; jsi, and fjlig during the pulse 0 t Dt is X g ðtÞexpðivtÞj g i þ C s ðtÞjsi þ l ðtÞjli; YðtÞ ¼ C ð6:63Þ C where
l
D E a ðtÞ ¼ ajUðt; 0ÞjYð0Þ ; C
a ¼ g; s; l:
ð6:64Þ
0Þ in Equation 6.64 is the time evolution operator during the pulse Uðt; eff tÞ; 0Þ ¼ expðiH Uðt;
ð6:65Þ
determined by the generalized effective Hamiltonian
eff ¼ H
k
Eg þ v
vR =2
0
vR =2
Es ics =2
Vsl
0
Vsl
El icl
0 .. . .. .
Vsl0 .. . .. .
0 .. . .. .
k
.. .. . . .. .. Vsl0 . . .. .. 0 . . ; . . El0 icl0 =2 .. .. .. .. .. . . . .. .. .. . . . 0
ð6:66Þ
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148
which also contains the dressed ground state characterized by the energy Eg þ v and the coupling between the ground state j g i and the doorway state jsi in terms of the m gs~ mjsi. A closed formal solution of the E, where ~ m gs ¼ hgj Rabi frequency vR ¼ ~ problem can be obtained by diagonalization of the GEH via a nonunitary transfor 0Þ in terms of the diagonalized projections: mation and by expansion of Uðt; X 0Þ ¼ Uðt; ð6:67Þ j jiexpðiEj tcj t=2Þ jj; j
eff and j ji the (complex) eigenwhere Ej icj =2 are the complex eigenvalues of H P vectors, which satisfy the relation j j ji jj ¼ 1 with ji being the vector conjugate to j ji. Readers may refer to Appendix G for more details. We may use Equation 6.67 to write the probability amplitudes (Equation 6.64) in the form E XD a ðtÞ ¼ aj j > expðiEj tcj t=2Þh jjYð0Þ ; a ¼ g; s; l; 0 t Dt; C j
ð6:68Þ
and the dipole moment induced in each molecule at t during the pulse g ðtÞexpðivtÞ þ cc: ðtÞC pðtÞ ¼ hYðtÞjmgs YðtÞi ¼ mgs C s
ð6:69Þ
Substituting Equation 6.63 into Equation 6.69 gives D E XXD 0 pðtÞ ¼ mgs Yð0Þj ji jjs hgjj0 i j jYð0Þ exp½iðEj Ej0 Þtðcj þ cj0 Þt=2: j0
j
ð6:70Þ
As the spacing of the real part of the eigenvalues ðEj Ej0 Þ is uncorrelated, one expects severe destructive interference effects for pðtÞ, when more than a single ME is driven by the field. Thus, coherent optical effects such as photon echoes or free induction decay experiments can be conducted only under special excitation conditions as follows: (a) Short-time excitation: This spans the entire congested excited spectrum of the molecule. This excitation mode, sometimes called as coherent molecular excitation [146–149, 186], corresponds to optical selection of the Born–Oppenheimer doorway state jsi. This excitation mode is specified by the condition Dt D1 sl ;
where Dsl ¼ 2p
X
jVsl j2 dðEs El Þ
ð6:71Þ
ð6:72Þ
l
is the width of the MEs. This excitation mode is feasible for an excited state that corresponds to a statistical large molecule or to a molecule with an intermediate-level structure. These assumptions are fairly justified in the case of picosecond excitation pulses as the coherent bandwidth of the pulses (typically 2--3 cm1 ) exceeds the
6.5 Dephasing and Relaxation in Molecular Systems
inhomogeneous linewidth (1 cm1 ). Under this special condition, the EH of Equation 6.61 can be considered as a scalar Heff ¼ Es Ds iðcs þ Dsl Þ=2, where Ds is the level shift. Then, the GEH that describes the interaction of the molecule with the pulse reduces to a 2 2 matrix, which represents a familiar two-level system [172],
k
k
Eg þ v vR =2 Heff ¼ vR =2 Es Ds iðc þ Dsl Þ=2 : s
If the pulse is sufficiently intense so that vR Eg þ vEs Ds iðcs þ Dsl Þ=2;
ð6:73Þ
ð6:74Þ
the time evolution during the pulse is simply 0Þ ¼ j g i cosðvR t=2Þ expðivtÞhgj þ jsi cosðvR =2Þhsj þ ij g i Uðt; sinðvR t=2Þ expðivtÞhsj þ ijsi sinðvR t=2Þhgj:
ð6:75Þ
(b) Narrow-band excitation: In the small molecule limit or in a molecule that corresponds to the intermediate-level structure, the coupling Vsl between the Born–Oppenheimer states is large while the density of states in the background manifold is low. The states jli are coarsely spaced relative to their widths and the manifold fjlig cannot act as a dissipative channel. In this case, the MEs basis j ji that diagonalizes Heff is of great utility. The level distribution of j ji is sufficiently sparse so that for the widths we have cj < r1 r1 j l and an optical excitation by a narrow-band pulse characterized by Dt < c1 j for all j;
Dt D1 sl
ð6:76Þ
will result in the selection of a single ME in each molecule (if the inhomogeneous broadening will not bring different MEs of different molecules into resonance with the narrow-band excitation source). 6.5.3 Free Induction Decay of a Large Molecule
In what follows, we consider the time evolution within a subset of discrete levels jsi of an assembly of collision-free polyatomic molecules, which interact on the timescale 0 t Dt with a short laser pulse and where the background manifolds fjlig do not carry oscillator strength to j g i. These time evolutions during the pulse 0 t Dt are eff tÞ, while after the pulse t ¼ Dt þ t are determined by ðt; 0Þ ¼ expðiH given by U the time evolution operator in the diagonalized form as X Uðt þ Dt; DtÞ ¼ j g iexpðiEg tÞhg j þ ð6:77Þ j jiexpðiEj tcj t=2Þ jj; j
where the eigenvalues of EH (Equation 6.61) are Eg and ðEj icj =2Þ, while the eigenvectors are j g i and j ji and the corresponding left eigenvectors are denoted by j . As the initial state of each molecule at t ¼ 0 is Yð0Þ ¼ j g i, the state of the
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system at time t ¼ Dt þ t can now straightforwardly be calculated by multiplication of the time evolution operators ðDt; 0Þjg i: YðtÞ ¼ Uðt þ Dt; DtÞU
ð6:78Þ
Considering the radiative coupling with a p=2 pulse, that is, vR Dt ¼ p=2, Equation 6.78 together with Equations 6.75 and 6.77 results in X YðtÞ ¼ expðivDtÞexpðiEg tÞjg i þ iCss ðtÞjsi þ i Cls ðtÞjli; ð6:79Þ l
where the probability amplitudes after the termination of the pulse are given by X Cab ðxÞ ¼ hajjihjjbiexpðiEj xcj x=2Þ; a; b ¼ s; l: ð6:80Þ j
The polarization per molecule after the pulse is obtained from Equation 6.69 is pðtÞ ¼ imgs expðivDtÞexpðiEsg tÞCss ðtÞ þ cc;
ð6:81aÞ
which may further be simplified to the form pðtÞ ¼ imgs expðivDtÞexpðiDEsg tÞf ðtÞ þ cc; where
DEsg ¼ Es Eg ;
ð6:81bÞ ð6:82Þ
mgs is the projection of the dipole operator in the direction of the field, and X f ðtÞ ¼ hsjjih jjsiexp½iðEj Es Þtcj t=2; ð6:83Þ j
with ðEj Es Þ being the detuning of a particular molecule. Since f ðtÞ is expressed in terms of the intrinsic property of a single molecule, we shall refer to f ðtÞ as the intramolecular dephasing term to distinguish it from the portion of inhomogeneous broadening. In evaluating the macroscopic polarization, we must use an appropriate distribution for the inhomogeneous broadening. The latter can be described by a Gaussian distribution of DEsg 2
ð6:84Þ WðEsg Þ ¼ ðbp1=2 Þ1 exp b2 DEsg DEsg0 ; which peaks at DEsg0 and is characterized by the width b. The macroscopic polarization PðtÞ of the molecular assembly is then ð PðtÞ ¼ N dðDEsg ÞWðDEsg ÞpðtÞ; which results in the expression o n PðtÞ ¼ Nmgs exp b2 t2 =4 sin DEsg0 t Ref ðtÞ þ cos DEsg0 t Im f ðtÞ ;
with N in Equation 6.85 being the molecular number density.
ð6:85Þ
6.5 Dephasing and Relaxation in Molecular Systems
For some application to molecular physics, we may wish to generalize (6.85) to include the reaction of the detector to determine the OFID signal. This may be obtained by squaring of Equation 6.85 and performing an optical cycle averaging ðsi n2 ðDEsg0 tÞ ¼ 1=2 . . .Þ to find IOFID ¼ A expðb2 t2 =2Þj f ðtÞj2 ;
ð6:86Þ
where the constant A refers to the time-independent parameters, such as frequency of the radiative field v, projection of the dipole operator mgs, molecular density N, and parameters of the detection system. Equation 6.86 provides us with an expression for the macroscopic polarization and the following remarks are worthy of note: 1) Inhomogeneous broadening: This contribution originates from the oversimplified assumption of light power and short-time excitation and is given by the Gaussian in Equation 6.86. 2) Intramolecular dephasing: This contribution is given by the function j f ðtÞj2 ¼ jCss ðtÞj2 . 1 For timescales relatively shorter than all genuine times c1 j , that is, t cj , Css ðtÞ ¼ expðDsl t=2ÞexpðiEs tÞ;
ð6:87Þ
so IOFID exhibits an exponential intramolecular dephasing process of the optically selected Born–Oppenheimer state with the lifetime ðDsl Þ1 . For longer times, t c1 j , destructive interference effects erode all the contributions to the double sum of jCss ðtÞj2 , where j 6¼ j0 , so jCss ðtÞj2
X hsjjihjjsi2 expðc tÞ; j
j
t c1 j ;
ð6:88Þ
and the IOFID exhibits a sum of exponentials [146–149, 186]. The decay of the OFID in such long timescale can be realized in real life for the case of the intramolecular structure, where the decay widths cj correspond to the genuine T1 relaxation rates of the (nonoverlapping) MEs. These remarks offer only the barest indication of why the following discussion has extensive practical application. 6.5.4 Photon Echoes from Large Molecules
A photon echo is a pulse of radiation emitted by the sample after irradiation with two or more coherent laser pulses, characterized by the durations Dt1 and Dt2 and separated by the time t12 . The first excitation pulse creates a macroscopic polarization in the sample, which vanishes rapidly due to differences in resonance frequency of
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the absorbing molecules (inhomogeneous dephasing). One or more subsequent pulses reverse the dephasing process, leading to a recovery of the macroscopic polarization and corresponding radiation (the echo). The photon echo is the optical analogue of the spin technique (of a spin one-half system) in magnetic resonance spectroscopy. This analogue was demonstrated by Dicke [187]. The corresponding equations for optical transitions were later derived by Feynman, Vernon, and Hellwarth [188]. The dynamics of the coherently prepared state of the system is described by a pseudo-spin vector, which during the system development with the resonant frequency of the optical transition rotates about a z-axis (the direction of the B field for magnetic transitions). In the course of this process, the z-component of this pseudo-spin describes the state of the inversion of the ensemble, while the projection in the complex x–y plane macroscopically describes the polarization p (the x-axis is the direction of an adjacent external field). Both components are subject to exponential decay. Correspondingly, both the longitudinal relaxation time T1 , which is identical with the lifetime of the excited state, and the transversal relaxation time T2 , which is also known as the total dephasing time, exist [189], since they describe the decay of the phase correlation between the excited ensemble molecules. Under certain conditions [189], the line shape is Lorentzian with a width Dnhom ¼
1 ; pT2
ð6:89Þ
where
1 1 1 ¼ þ : T2 T2 2T1
ð6:90Þ
T1 is the level depletion lifetime and T2 is the pure dephasing time associated with the phase destructive events (e.g., by phonons and intermolecular interactions). This point will be taken up in more detail in Chapter 7. Here we merely note that the pure dephasing time T2 is temperature dependent. Let us now return to the time development of the system, described in terms of the macroscopic polarization in spirit of the preceding section. In accordance with the above discussion, we shall now again consider short-time excitation conditions (6.71) and (6.74). The initial state of the system is Yð0Þ ¼ j g i, whereupon the state of the system at time t ¼ Dt1 þ t12 þ Dt2 þ t is ðDt2 þ t12 YðtÞ ¼ Uðt þ Dt2 þ t12 þ Dt1 ; Dt1 þ t12 þ Dt2 ÞU ; þ Dt1 ; t12 þ Dt1 ÞUðt12 þ Dt1 ; Dt1 ÞUðDt1 ; 0Þj g i
ð6:91Þ
during the pulses are given by Equation 6.65, where the time evolution operators U while the time evolution operators U, when the field is switched off, are given by Equation 6.77. The evaluation of Equation 6.91 is identical with that following Equations 6.63–6.69, which we need not repeat. Utilizing the conventional sequence of p=2 pulse, that is, vR Dt1 ¼ p=2, followed by a p pulse for which vR Dt2 ¼ p, the polarization per molecule at time t þ Dt2 þ t12 þ Dt1 assume the form
6.5 Dephasing and Relaxation in Molecular Systems
pðtÞ ¼ imgs fCss ðt12 ÞCss ðtÞexp½ivðDt1 Dt2 Þexp½iEg ðt12 tÞ þ ½Css ðt þ t12 ÞCss ðtÞCss ðt12 ÞexpðivDt2 ÞexpðiEg tÞg þ cc;
ð6:92Þ
where the probability amplitude Css ðxÞ for the time evolution is given by Equation 6.80. Following the discussion of the properties of this function given in the preceding section, it is apparent from Equation 6.80 that for the timescale t c1 j (for all j), the second term on the right-hand side of Equation 6.92 vanishes identically. Furthermore, it can also be shown that for longer times, this term will not contribute to the photon echo. Thus, Equation 6.92 may be simplified by removing this term and we will easily obtain pðtÞ ¼ imgs exp½ivðDt1 Dt2 Þexp½iDEsg ðt12 tÞFðt12 ; tÞ; þ cc
ð6:93Þ
where DEsg is given by Equation 6.82 and Fðt12 ; tÞ ¼ f ðtÞf ðt12 Þ;
ð6:94Þ
with f ðxÞ given by Equation 6.83. Furthermore, as t12 Dt1 ; Dt2 and v ¼ DEsg , the exponential function exp½ivðDt1 Dt2 Þ in Equation 6.93 can be omitted in the subsequent discussion. Performing now the averaging over the inhomogeneous distribution (Equation (6.84), we find for the macroscopic polarization
PðtÞ ¼ Nmgs exp b2 ðtt12 Þ2 =4 sin DEsg0 ðt12 tÞ Re Fðt12 ; tÞ þ cos½DEsg ðt12 tÞIm Fðt12 ; tÞ :
ð6:95Þ
The final step in our procedure is to relate this result to the expression for the radiative intensity of the photon echo signal IPE at time t ¼ Dt1 þ t12 þ Dt2 þ t. After performing the optical cycle averaging of Equation 6.95 and following the method given in the section above, the PE intensity assumes the final form
IPE ðtÞ ¼ A exp b2 ðtt12 Þ2 =2 jFðt; t12 Þj2 :
ð6:96Þ
Equation 6.96 has a clear physical significance. The temporal behavior of the photon echo from an assembly of large molecules, which are excited by two short onresonance laser pulses, is determined by the inhomogeneous dephasing contribution exp½b2 ðtt12 Þ2 =2 peaking at t ¼ t12 , while the amplitude aPE of the echo at t ¼ t12 is determined by the contribution of the intramolecular dephasing aPE ¼ jFðt; tÞj2 ¼ jCss ðtÞj4 , where Css ðtÞ being, of course, similar to that of the OFID signal. Now, following the above discussion given in connection with the function Css ðtÞ, we note that 1) For sufficiently short times t12 cj 1 (for all j), the relevant echo decay amplitude is given by Equation 6.80, so that at t ¼ t12 aPE / expð2Dsl t12 Þ;
exhibiting an exponential decay [172] with a lifetime ð2Dsl Þ1 .
ð6:97Þ
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2) For longer times t12 > c1 j , the decay amplitude is given by a sum of exponentials (compare with Equation 6.88) and the amplitude of the photon echo is X aPE / aj expð2cj t12 Þ; ð6:98Þ j
where aj 1=n2 and hcj i cs =n þ cl with n being the dilution factor of the doorway state [146–149, 186]. This physical situation can be accomplished for the intermediate-level structure [146–149, 186, 190], where the long-time depletion rate T1 will be amenable to experimental observations.
j155
7 Miscellaneous Applications In this chapter, a number of rather disconnected topics are discussed to illustrate the application of the general technique developed in earlier chapters. We shall begin our discussion with the derivation of line shape functions for optically allowed and vibronically induced transitions. This will permit us to demonstrate the influence of the Duschinsky rotation on optical spectra. As an example, we shall describe the spectrum of the p-terphenyl crystal from the same point of view and of the ½CoðCNÞ2 ðtnÞ2 Cl3 H2 O complex in its crystal structure. These examples offer little more than a glimpse into the difficult, subtle, fascinating questions encountered in almost any attempt to interpret optical transitions. The discussion is extended in Section 7.2 to the analysis of phosphorescence spectra and the description of radiationless transition of aromatic molecules. Particular emphasis is placed on the mechanism of singlet–triplet relaxation in these molecules with nonbonding electrons. In Sections 7.3 and 7.4, the temperature dependence of radiationless transitions and the effect of deuteration on the lifetimes of excited electronic states are examined. In Section 7.5, a contribution to time-resolved spectroscopy is presented. In that section, we will discuss a problem dealing with transport phenomena of electronic excitations in doped molecular crystals. The theory of singlet excitation energy transfer uses an effective Hamiltonian to account for intramolecular excited-state depopulation and energy transfer by multistep migration among guest molecules. Finally, in Section 7.6 we shall illustrate our discussion of Section 1.4 with an application to the predissociation of the triatomic molecule H2 O þ .
7.1 The Line Shape Function for Radiative Transitions 7.1.1 Derivation
In addition to the study of nonradiative decay probability (of excited electronic states), the consideration of the decay of excited electronic states has many additional
j 7 Miscellaneous Applications
156
applications. This includes such familiar examples as decay by radiative transition. This can be best described in terms of a line shape that provides a very useful basis for discussing resonance and decay phenomena. The line shape function is given for transition in emission from excited state jsi to a ground state j0i in the form [92] XX 2 f ðEÞ ¼ pðm : TÞVsm;0n dðDE þ Esm Eln EÞ; ð7:1Þ fmm g fnm g
where the sums are extended over all final states n ¼ ðn1 ; n2 ; . . . ; nN Þ and averaged over the initial states m ¼ ðm1 ; m2 ; . . . ; mN Þ, being in thermal equilibrium at temperature T. pðm; TÞ is the probability that the system will be initially in the P zeroth-order states jsmi, so that m pðm; TÞ ¼ 1. Provided that vibrational relaxations are faster than electronic transitions, thermal equilibrium prevails and pðm; TÞ ¼ Z 1 expðbEsm Þ;
ð7:2Þ 1
where Z1 is the partition function defined in Equation 3.8 and b ¼ ðkB TÞ . DE corresponds to the energy gap between the lowest vibrational components of the two electronic states DE ¼ Es;0 E0;0 ¼ hV:
ð7:3Þ
The energies Esm and Eln of the vibrational levels in each electronic manifold are measured from the zeroth level of that manifold. Thus, X X Esm ¼ hmm vsm and E0n ¼ hnm v0m : ð7:4Þ fmm g
fnm g
Rather than use (7.1), we consider its Fourier transform 1 ð
FðtÞ ¼ 1
ðEDEÞt exp i f ðEÞ dE; h
which can be expressed in the form X FðtÞ ¼ Z1 Vsm;0n expðiE0n t=hÞV0n:sm expðiEsm t= hbEsm Þ:
ð7:5Þ
ð7:6Þ
m;n
The function FðtÞ may be related to the generating function introduced in Chapter 3 for calculating the probability of radiationless transitions. If for the matrix elements in Equation 7.6 we write Vsm;ln ¼ ðxsm ðqs ÞjVs0 ðqÞjx0n ðq0 ÞÞ;
ð7:7Þ
where Vs0 ðqÞ ¼ hjs ðr; qs ÞjV jj0 ðr; q0 Þi
ð7:8aÞ
is the operator responsible for the radiation matter interaction. Using the Greens functions for the nuclear motion in the electronic states |si and j0i given by
7.1 The Line Shape Function for Radiative Transitions
Equation 3.18, the summation in (7.6) over collections of vibrational quantum numbers m ¼ ðm1 ; m2 ; . . . ; mN Þ and n ¼ ðn1 ; n2 ; . . . ; nN Þ gives FðtÞ ¼ Z1
1 ð
ðY m
1
0 0 dq0m dq0m Vs0 ð qÞrs qsm ; qsm ; wm V0s ðqÞr0 ~ q m ; qm ; zm : ð7:9Þ
The operator Vs0 ðqÞ for the radiation matter interaction may be expanded about some reference configuration q0 along some nontotally coordinates q0g of the electronic ground state ! X qVs0 X g Vs0 ðqÞ ¼ Vs0 ðq0 Þ þ q0g þ þ ¼ Vs0 ðq0 Þ þ Vs0 ðq0 Þq0g ; 0 qq g g g 0
ð7:8bÞ
where the first term is responsible for electric dipole allowed transition (see Equation g 6.10). We shall not discuss here the detailed construction of the operator Vs0 ðq0 Þq0g for the vibronically induced transitions, however, since we require only the property that it is associated with the coordinate qg . This is done, for example, in Section 7.2. Since the vibrational amplitudes of qg s remain small, we terminate the expansion on terms linear in qg . This permits us to write Equation 7.9 as FðtÞ ¼ F 1 ðtÞ þ F 2 ðtÞ;
where F 1 ðtÞ ¼ Z 1 jVs0 ðq0 Þj2
ð7:10Þ N Y m¼1
and F 2 ðtÞ ¼ Z1
ðmÞ
G1 ðtÞ;
ð7:11Þ
Y ðmÞ X g X g g0 V ðq0 Þ2 K ~ g ðtÞ G ðtÞ þ Z1 V ðq0 ÞV ðq0 Þ s0
g
~I g ðtÞ~I g0 ðtÞ
Y m6¼g;g0
m6¼g
1
g6¼g0
ðmÞ
G1 ðtÞ:
s0
s0
ð7:12Þ
ðmÞ
The terms G1 ðtÞ correspond to the single-mode generating function defined in ~ g ðtÞ corresponds to a single-mode generating function Equation 3.13. The factor K that involves the nuclear coordinate qg of the promoting mode. It induces the radiative transition ~ g ðtÞ ¼ K
ð
1 ð
dq0g dq0g rs qsg ; qsg ; wg q0g r0 q0g ; q0g ; zg q0g :
ð7:13Þ
1
ðgÞ
The latter integral is related to the integral G1 ðtÞ analogous to relation (3.72), namely, " # 2g 2bs2 k2g w 1 1 1 g ðgÞ ~ g ðtÞ ¼ K G1 ðtÞ þ s 2 0 1 0 2 bsg w g þ b0g zg bsg w 1 z þ b ðb þ b Þ w z g g g g g g g ð0Þ
ðgÞ
~ ðtÞG ðtÞ: ¼K 1 g
ð7:14Þ
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158
Considering the case with undisplaced and undistorted harmonic potential surface for the promoting mode, Equation 7.14 may be put into a simpler form analogous to the propensity rule for the promoting mode (3.73). This gives hvg h vg h 1 1 ivg t ivg t ~ ð0Þ ðtÞ ¼ þ ; coth coth K þ 1 e 1 e g 2vg 2 2 2kB T 2kB T ð7:15aÞ
which for low temperatures goes to ivg t h ~ ð0Þ e : K g ðtÞ ¼ 2vg
ð7:15bÞ
Finally, some mixed-type single-mode generating functions appear in Equation 7.12; these are governed by ~I g ðtÞ ¼
1 ð
ð
dq0g dq0g rs ðqsg ; qsg : wg Þq0g r0 ðq0g ; q0g ; zg Þ:
ð7:16Þ
1
As discussed above in the case of radiationless transitions, in the harmonic approximation, where kg ¼ 0, the latter term vanishes (see the discussion in connection with Equation 3.74). Thus, the generating function (7.12) takes the more convenient form F 2 ðtÞ ¼ Z1
Y ðmÞ X g V ðq0 Þ2 K ~ g ðtÞ G1 ðtÞ: s0 g
ð7:17Þ
m6¼g
To complete our derivation, we have yet to take the inversion formula (to (7.5)) f ðEÞ ¼ ð2phÞ1
1 ð
FðtÞ exp½iðEDEÞt= h dt:
ð7:18Þ
1
This permits us to expresses the line shape function f ðEÞ in terms of the generating function FðtÞ. This is a useful conclusion, since FðtÞ is ordinarily easier to evaluate directly than is f ðEÞ. The reader should be warned, however, that the Fourier transformations (7.5) and (7.18) hold in general only for generalized functions. In ordinary function theory, f ðEÞ and FðtÞ must fulfill some conditions for Equations 7.5 and 7.18.1) Therefore, we have chosen to modify Equation 7.1 to incorporate a finite width by using a Lorentzian distribution in Equation 7.1 to conserve energy, instead of the d-function of Dirac. This leads to a modification of Equation 7.18 by introducing a real factor Ch1 jtj in the exponent of the integrand of Equation 7.18. Using this modification, then inserting Equations 7.3, 7.4 and 7.11 in Equation 7.18, and finally carrying out 1) For example, Equation 7.18 does exist for any FðtÞ that falls off sufficiently rapidly as t ! 1 that the integral (7.18) of its square is finite.
7.1 The Line Shape Function for Radiative Transitions
the integration by applying the procedure of Section 7.3, we find for the direct electric dipole allowed process X 2cexp h mm vsm =kB T 2 X X 1 1 m f1 ðvÞ ¼ Z Vs0 ðq0 Þ 2 X X 2p fmm g fnm g mm vsm þ nm v0m þ c2 vV IN
fmm g
m1 ; m2 ; . . . ; mN : n1 ; n2 ; . . . ; nN
fnm g
ð7:19Þ
Similarly, for the vibronically induced transition with F 2 ðtÞ as generating function, we have 0 1 ( 1 1 X @ h A g 2
Vs0 coth ð hvg =2kB TÞ þ 1 f2 ðvÞ ¼ Z 2p 4v g g X s 2cexp h mm vm =kB T XX m 2 X X fmm g fnm g mm vsm þ nm v0m þ c2 vV þ vg IN
m1 ; m2 ; . . . ; mN n1 ; n2 ; . . . ; nN
XX þ coth ðhvg =2kB TÞ1 fmm g fnm g
IN
m1 ; m2 ; . . . ; mN n1 ; n2 ; . . . ; nN
)
fmm g
fnm g
X s 2cexp h mm vm =kB T
vVvg
m
X fmm g
mm vsm þ
X
2 nm v0m
þ c2
fnm g
ð7:20aÞ
where we have introduced the notation c ¼ Ch1 and E ¼ hv is the energy of the emitted light. Despite the fact that the promoting modes g enter the ID IN , they make a negligible contribution to IN , since according to Equation 7.14 and the discussion in ðgÞ Section 3.3, G1 ðtÞ ffi 1. As in the case of radiationless transitions, we see that the net effect of the promoting mode is to decrease or increase the energy gap to hV hvg with temperature dependence of ½coth ðhvg =2kB TÞ 1, respectively. Near v V; ðmm ¼ nm ¼ 0Þ;f2 ðvÞ is proportional to 0 1 ( 1 1 X @ h A g 2
2c f0 ðvÞ ¼ Vs0 cothðhvg =2kB TÞ þ 1 Z 2p 4v ðvV þ vg Þ2 þ c2 g g )
2c ; þ coth ðhvg =2kB TÞ1 ðvVvg Þ2 þ c2 ð7:21aÞ
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where the summation is restricted only to the promoting modes g. It is therefore possible to write Equation 7.20a as 0 1 XX X X s 0 f2 ðvÞ ¼ f0 @v mm vm þ nm vm Aexp ðmm hvsm =kB TÞ fmm g fnm g
IN
fmm g
m1 ; m2 ; . . . ; mN : n1 ; n2 ; . . . ; nN
fnm g
ð7:20bÞ
This is a useful conclusion since f0 ðvÞ is ordinarily easier to estimate from an optical emission spectrum than f2 ðvÞ. s If we were to follow the discussion that led to Equation 7.20b by setting wn ¼ eivn t iv0n t hv0n =kB T ivsn thvsn =kB T iv0n t and zn ¼ e (instead of wn ¼ e and zn ¼ e as in the previous derivations), we would obtain an expression for the line shape function in absorption in the same convenient form 0 1 X X ðabÞ X X ðabÞ f2 ðvÞ ¼ f0 @v mm vsm þ nm v0m Aexp ðnm hv0m =kB TÞ fmm g fnm g
IN
fmm g
fnm g
m1 ; m2 ; . . . ; mN ; n1 ; n2 ; . . . ; nN
ð7:20cÞ
where ðabÞ f0 ðvÞ ¼
8 0 1 1 1 X @ h A g 2 <
2c Vs0 cothðhvg =2kB TÞ þ 1 Z : 2p 4v ðvVvg Þ2 þ c2 g g
þ cothðhvg =2kB TÞ1
2c ðvVþ vg Þ2 þc2
) :
ð7:21bÞ
This brings to a close of the first section, in which we have reformulated the findings already presented in Chapter 3 by an alternative route. 7.1.2 Implementation of Theory and Results
The expressions derived for the line shape function play an important role in the subsequent discussion of optical spectra. Many important conclusions can be drawn from such spectra when they are fitted to expressions such as those given by Equations 7.19 or 7.20a. This is illustrated in Figure 7.1, where typical resolved line shapes that consist of sequences or progressions of individual vibronic lines are presented. The line shapes were calculated for an electric dipole allowed transition at zero temperature (according to Equation 7.19 at mm ¼ 0), involving two nonseparable accepting modes with frequencies vs1 ¼ 90; v01 ¼ 100; vs2 ¼ 300, and v02 ¼ 240 cm1 . The direct dimensionless displacements of the excited state origins ð1Þ relative to those of the lower electronic state are chosen as moderately large D12 ¼ 3:0 ð2Þ and D12 ¼ 2:0 and the widths for all vibrational levels of the lower electronic state are
7.1 The Line Shape Function for Radiative Transitions
Figure 7.1 Highly resolved spectral profile plotted versus frequency converted to wave numbers (~ n ¼ v=2pcÞ. There are clearly identifiable the existence of single-mode progressions at j ¼ 30 and j ¼ 60 as well as the scrambling of modes for other values of
j. The spectroscopic parameters for which the calculation has been carried out are ð1Þ ð2Þ D12 ¼ 3:0; D12 ¼ 2:0, vs1 ¼ 90; v01 ¼ 100; s v2 ¼ 300, and v02 ¼ 240 cm1 . For convenience, the 0–0 transition ðv ¼ VÞ has been located in the zero point of the ~n scale.
taken equal to C ¼ hc ¼ 10 cm1 . The latter reflects the effect of interaction of the molecule with the radiative continuum and the heat bath (solvent). The spectra as we see in Figure 7.1 reveal a rich structure originating from (intrastate) mode scrambling that strongly depends on the rotation angle j. It is particularly interesting to note that
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this scrambling effect becomes negligible at special values of the rotation angle j. For example, at j ¼ 30 , the mode with the frequency vl1 ¼ 100 cm1 dominates, whereas the mode with the frequency vl2 ¼ 240 cm is suppressed. At nearly j 120 , the opposite situation is observed. These extreme situations, where there is only a single mode in the spectrum, depend on the values of all spectroscopic ðmÞ parameters involved in the multidimensional ID. The displacement parameters D12 have a much larger effect than the frequency factors bm . These findings are consistent 0 0 with the conclusion previously derived that I2 behaves at some rotation n1 n2 angles j practically as an ID of the dimensionality one, distributed mainly along the n1 or n2 axis. A further relation to Figure 4.9 is more readily seen. Both Figures 4.9 and 7.1 demonstrate a striking energy spread of the line shape. In other words, a j-dependent distribution of the transition moment connecting the vibrationless excited state with the vibrational levels of the lower electronic state is shown. This is clearly illustrated by the two plots at the bottom of Figure 7.1. Variation of the angle of rotation j results in a considerable enhancement of the number of members in the single-mode progressions from about 10 for j ¼ 30 to about 20 for j ¼ 120 ð60 Þ. ð1Þ ð2Þ Clearly, this unusual spread cannot result from the displacements D12 and D12 of the individual acceptor modes alone, as in the parallel approximation. If this were the ð1Þ case, the progression in v1 with D12 ¼ 3:0 would be longer than that in v2 , where the ð2Þ displacement parameter is only D12 ¼ 2:0. We can, however, find an explanation of this rather unexpected effect by noting that owing to the mode mixing, the line shape ðmÞ is essentially determined by the dm;n parameters. The latter contain the fD12 g and fDð12Þ m g ðm ¼ 1; 2Þ in a scrambled form (see Equation 3.35) and hence become displacement parameters. Finally, note that in j-dependent via the reciprocal Dð12Þ m ðmÞ addition to the angle j of rotation and the displacement parameters fD12 g, the change of frequencies b1 and b2 and the cross frequency parameters b12 and b21 have a detectable influence of I2. Without alluding to any further numerical calculations, we can assert that variation of these parameters must be used in some manner to explain the asymmetry of the spectral profiles. To conclude, let us analyze the measured fluorescence spectrum of the p-terphenyl (PT) crystal from the same point of view. Figure 7.2 shows the PT spectrum at 4.2 K (heavy solid curve) near the electronic origin at 336 nm corresponding to the optically allowed transition from the S1 ð1 Au Þ excited state to the S0 ð1 Ag Þ ground state [154,191–193]. The intensity of the 0–0 line is reduced due to reabsorption events [192]. The vibrational structure is mainly composed of three ground-state vibrational accepting modes that can be assigned to the totally symmetric in-plane fundamentals of the PT molecule in the ground state at vS1 0 ¼ 232; vS2 0 ¼ 1256, and vS3 0 ¼ 1612 cm1 . Whereas vS2 0 and vS3 0 manifest themselves in the spectrum as two intensive progressions extending over four members and corresponding combination lines, the vS1 0 fundamental and its overtones appear as shoulders in the envelop. The assignment made above has been confirmed by calculation of the overall intensity distribution employing the line shape function (7.19) at low temperatures ðmm ¼ 0Þ and by performing a force-field calculation [194] for the Cartesian
7.1 The Line Shape Function for Radiative Transitions
Figure 7.2 (a) Experimental (heavy solid curve) and calculated (lighter curve) fluorescence spectra of p-terphenyl in the crystalline phase at 4.2 K plotted versus wave numbers. (b) As (a) with the exception that the
high-resolution spectrum (shown as lighter curve) has been calculated by means of the line shape function (7.22) with c ¼ 30 cm1 and by including the torsional mode.
displacements of the vibrational modes. Figure 7.2a presents the calculated spectrum (lighter curve) in comparison to the experimental spectrum (heavy solid curve). The parameters used in this calculation are listed in Table 7.1. The linewidth was assumed to be 120 cm1 . Among these parameters, the ground-state vibrational frequencies vSm0 have been obtained from the fluorescence spectrum. The excited-state vibrational frequencies vSm1 ðm ¼ 1; 2; 3Þ, the dimensionless displacement parameters Table 7.1 Optimized constants obtained from the calculation of the S1 ! S0 fluorescence spectrum of p-terphenyl. ðmÞ
ðmÞ
m
vSm0 (cm1)
vSm1 (cm1)
D123
k123 (A)
w (deg)
u (deg)
y (deg)
1 2 3
232 1256 1612
214 1350 1575
0.88 0.92 1.43
0.091 0.127 0.128
12
9
13
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ðmÞ
D123 ðm ¼ 1; 2; 3Þ, and the three Euler angles w; q; j parameterizing the rotation matrix W have been varied until the best fit of the experimental spectrum was achieved. The 3 3 rotation matrix 0:970 0:241 0:023 W ¼ 0:241 0:949 0:203 0:027 0:203 0:979 implies that the above three vibrational normal modes are scrambled or mixed. From the values of the off-diagonal matrix elements, it is apparent that the mixing effect between the modes v1 and v2 , as well as between v2 and v3 , is larger than between ðmÞ ðmÞ hÞ1=2 k123 , one modes v1 and v3 . From the determined parameters D123 ¼ ðvSm0 = ðmÞ obtains the magnitudes of the excited-state distortions k123 along the corresponding modes qSm0 ðm ¼ 1; 2; 3Þ. To this end, the vibrational frequencies vSm0 and the reduced masses have been determined by calculating the Cartesian displacements of the vibrational modes employing the MNDO method and the subsequent force-field (FORCE) procedure. The main displacement vectors of the vSm0 modes are depicted in Figure 7.3. The molecular structure data resulting from the MNDO geometry optimization calculation are summarized in Tables 7.2 and 7.3. From the Cartesian displacement coordinates and the parameters collected in Tables 7.1 and 7.3, the distortions along the coordinates qSm0 ðm ¼ 1; 2; 3Þ associated with the transition S1 ! S0 can be calculated. In particular, a lengthening of the interannular CC ˚ bond in the S1 state relative to the ground state S0 of PT is found to be 0:01 A. The individual vibronic lines in the fluorescence spectrum at 4.2 K are rather broad ðc ¼ 120 cm1 Þ compared to those ðc ¼ 10--20 cm1 Þ of planar rigid molecules such
Figure 7.3 Atomic displacements for the totally symmetric PT vibrations vS10 ; vS20 , and vS30 obtained from the FORCE force-field procedure. The scale of the displacements has been expanded five times.
7.1 The Line Shape Function for Radiative Transitions Table 7.2 The MNDO-optimized molecular structural parameters of p-terphenyl.
Interannular CC bond length (A)
Benzene-ring CC bond lengths (A)
CH bond lengths (A) Benzene ring CCC bond angles (deg) Interannular dihedral angle (deg)
1.485 1.401–1.404 1.085–1.091 119–121 33.23
as anthracene or naphthalene that crystallize in a well-defined lattice [195]. This intriguing paradox can be put down to the band structure of the real p-terphenyl crystal (the degenerate levels of the Np-terphenyl molecules in the periodic array broaden into bands with an energy spread of 4jbj, where b is the energy of the interaction between neighboring molecules) and to some extent to intermolecular dephasing. The latter effect is caused by the slightly different angles of the four TP molecules in the unit cell. The unit cell of crystalline p-terphenyl contains four molecules (Z ¼ 4), the site symmetry and the point group of which are Ci and C2h , respectively. The molecules take four nonplanar conformations in which the dihedral angles between the central ring and the outer ones are 15:2 ; 18:2 ; 23:4 , and 26:8
[196]. (We defer a full discussion of the crystal structure of p-terphenyl to Section 7.5.) If we now pay somewhat closer attention to the calculated spectrum in Figure 7.2a, recognizing that the torsional mode ðvS4 0 ¼ 72 cm1 Þ [197, 198] becomes populated, then we can draw some further conclusions that are important in studying the line shape in Figure 7.2a and its broadening. To do this, the torsional energies as functions of the potential barrier parameters have been determined using a perturbation procedure. The ground-state double-well potential along the torsional coordinate q has been constructed by superposing a Gaussian and a harmonic oscillator potential [199], the minima of which are assumed to be located at the average dihedral angle of q ¼ 20:9 . The barrier height of 135:1 cm1 is estimated from the phase transition temperature of about 193 K [200]. The vibrational wavefunctions for the torsional mode are obtained in terms of a series expansion of unperturbed oscillator functions, the coefficients of which are calculated by means of recursion equations as derived in Ref. [199]. If we further assume a harmonic potential of the S1 state [201, 202] and employ the partitioning technique previously introduced to separate the torsional mode from the others, the one-dimensional intramolecular distribution I1 responsible for the vibrational overlap due to the torsional mode is calculated and convoluted with the three-dimensional distribution I3 , which has been so far used in
The calculated (FORCE) ground-state vibrational frequencies c v S10 ; c v S20 ; c v S30 (in wave numbers) and their reduced masses MS10 ; MS20 ; MS30 . Table 7.3
c
v S10 (cm1)
227:82
c
v S20 (cm1) 1286.05
c
v S30 (cm1)
MS10 (amu)
MS20 (amu)
MS30 (amu)
1614.14
13.765
1.397
2.613
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Equation 7.19. Thus, the normalized (jVsl j2 = h ¼ 1) line shape involving additionally the torsional mode is written as 1X 2c 0; 0; 0 n1 n2 f1 ðvÞ ¼ I3 fD g; fbm ; bmn g P n1 ; n2 ; n3 m1 m2 p fn g vV 4 nm vSm0 2 þ c2 m¼1 m 0 D ; b I1 ; ð7:22Þ n4 4 4 where n4 denotes the torsional quantum number. In this approximation, we have effective transitions to at least three torsional levels, that is, n4 ¼ 0; 2; 4. This is clearly indicated in Figure 7.2b, where we show a comparison of the spectrum (lighter curve) of p-terphenyl calculated by choosing the values vS4 0 ¼ 55 cm1 and D4 ¼ 0:19 for the energy of the torsional mode and the displacement parameter, respectively, with the spectrum of experiment (heavy solid curve). To resolve the torsional lines, the line width is taken to be c ¼ 30 cm1 . However, in reality this resolution fails and the lines assigned to the torsional levels overlap leading to a single broad band having a width of approximately c ¼ 120 cm1. An extension of these methods to the analysis of optical spectra of other systems, especially of transition metal ions, may be found in Refs [156–162]. In that class of complexes, almost all intensity is concentrated in the so-called false origins displaced from the true electronic origin by one quantum of the odd parity promoting modes of the complexes. We shall discuss only a few of them that have proved to be particularly useful. We begin our discussion with a brief review of the vibrational fine structure that emerges in the case of the lowest spin-allowed absorption band of trans-½CoðCNÞ2 ðtnÞ2 þ ðtn ¼ 1; 3 propanediamineÞ, the latter of which stands in place of several Co complexes [94, 103–105]. In dealing with the temperature dependence of vibronically induced transition, we present in Section 7.3 the phosphorescence spectrum of the ReCl6 2 complex. In Figure 7.4, we present 1 Ag polarized absorption band of the low-energy region of the 1 Bg trans-½CoðCNÞ2 ðtnÞ2 Cl3H2 O at 4.2 K and Figure 7.5 gives information about the cationic complex and its packing in the crystal. In the crystal, the molecules are stacked collinearly to the orthorhombic crystallographic b-axis, while the NCCoCN axis occurs in two different orientations with respect to the unit cell. Both rings of the complex adopt a chair conformation. In the spectrum presented in Figure 7.4, the predominant peaks appear at 18 506, 18 706, 18 906, 19 106, 19 318, 19 523, 19 730 cm1, the intervals being 200, 200, 200, 212, 215, 207 cm1. The component at 19 106 cm1 has a shoulder on the higher frequency side. This component gains gradually in relative intensity in the higher frequency region to yield resolvable peaks. For comparison, the deuterated compound, trans-½CoðCNÞ2 ðd4 -N-tnÞ2 Cl3D2 O, shows a pattern of the spectrum similar to that of the H compound, but with a reduced interval in the progression of 195 cm1. On the basis of these observations, the vibrational fine structure can be interpreted as follows: Component A is the pure electronic origin while the components B, C, . . ., K are vibronic (false) origins of the transition. The energy intervals between A and each vibronic origin range from 0 to 620 cm1, so these vibronic components (except
7.1 The Line Shape Function for Radiative Transitions
Figure 7.4 Low-energy region of the 1 1 Bg Ag polarized absorption band of trans-½CoðCNÞ2 ðtnÞ2 Cl3H2 O at 4.2 K (next to 1 the broad-band 1 Bg ; 1 Ag ðC2h Þ Ag ðC2h Þ absorption), at extinction directions in the
rhombic crystal face parallel to the longer diagonal (heavy solid curve) and to the shorter diagonal (lighter curve). Crystal thickness 0.60 mm.
b
a sin
Figure 7.5 Crystal packing of trans- CoðCNÞ2 ðtnÞ2 Cl3H2 O: view down the c-axis.
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for the component K) can be attributed to skeletal deformational modes of the complex and to lattice modes. The component K can reasonably be well correlated to the ring deformational mode (C–C stretch), which is found by calculation to have a vibrational energy of 722 cm1 in the electronic ground state. The components nA, nB, . . ., nK ¼ vsX þ nvsd (X ¼ A, B, . . ., K) are members in the progression in the vsd total symmetric (tn cycle) mode built on the origin components. The superscript s denotes excited state. An intensity distribution analysis suggests a hidden component F at around 18 700 cm1 overlapping with the first member 1A (A þ 205) of the progression. According to these assignments, all the absorption bands corresponding to the 1 Ag ðC1 Þ are analyzed in terms of the line shape function (7.20c), transition 1 Bg ðabÞ where f0 ðvÞ is the sideband function describing the predicted vibronic structure (A, B, C, . . ., H lines) in the region around the pure electronic origin and vm are the vibrational frequencies of the progressional modes (vsm ¼ vsd in our case). As the measurement was done at low temperature, the ground-state vibrational quantum numbers n1 ¼ n2 ¼ ¼ nN ¼ 0. The index N in IN denotes the number of accepting (distorting) modes involved in the transition. Generally, it is reasonable to assume that N is larger than unity because the presence of vibrational structure implies a displacement between the potential energy surfaces of the excited state and the ground state in the configurational coordinate space, which promotes mixing of accepting modes. However, as this is strikingly illustrated in Figure 7.6 by using a ðabÞ function f0 ðvÞ (the insert in the figure) representing the vibronic structure in the 1 Ag ðC1 Þ transition, the 205 cm1 accepting electronic origin region of the 1 Bg 1 s mode vd alone is sufficient to describe the whole 1 Bg Ag ðC1 Þ absorption band shape. This means that in our particular case the structure represented in Figure 7.4 can be analyzed in terms of the one-dimensional distribution I1 ðmd ; 0; Dd ; bd Þ. The
1 1 Figure 7.6 Calculated Ag absorption spectrum of fit to the experimental Bg trans- CoðCNÞ2 ðtnÞ2 Cl3H2 O (heavy solid curve of Figure 7.4). The insert presents the peaks ðabÞ contained in the sideband f0 ðvÞ, as can be verified by careful examination of the spectrum.
7.1 The Line Shape Function for Radiative Transitions
latter depends parametrically on bd and Dd , where bd and Dd ¼ ðvd = hÞ1=2 Dqd are the frequency distortion and potential surface displacement along the coordinate qd , respectively. A close fit to the experimental absorption band, for which the peak heights of the lines as well as the vibrational frequency vd and the spectroscopic parameters Dd and bd have been varied, is given by Dd ¼ 3:2, vsd ¼ 205 cm1 , and bd ¼ 0:87. From the estimated excited-state vibrational frequency vsd and the measured ground-state frequency v0d ¼ 235 cm1, the quotient bd ¼ vsd =v0d yields 0.87, which is consistent with the value obtained above. 7.1.2.1 Excited-State Geometry 1 To analyze the question as to why the transition 1 Bg Ag exhibits one main progression in the measured absorption spectrum, we calculate the distorting forces acting on each of the atoms of the complex (especially of the skeleton CoðCNÞ2 ðN2 C3 Þ2 ) that results from the excitation of an electron from a t2 into an e orbital of the central ion. This will permit us to obtain information about the 1 Bg excited-state distortion relative to the ground state 1 Ag . The forces exerted in the electronic excited state 1 Bg with respect to the 1 Ag ground state, necessary to explain the result of absorption measurement, are given by qH 1 B i þ 1 A qH 1 A ; FA ¼ 1 Bg g g qRA qRA g
where RA ¼ ðxA ; yA ; zA Þ is the vector of three Cartesian displacements of atom A taken in directions of the x, y, and z octahedral axes. The calculation has been carried out by means of the semiempirical molecular orbital method using SCF basis sets built up from STO. The detailed description of the calculation procedure is given in 1 Ref. [105]. The Cartesian components of FA for the transition 1 Bg Ag are listed in Table 7.4. The forces acting on the corresponding atoms that are equivalent with respect to symmetry of the complex ðC2h Þ are the same but have to be taken with opposite signs. These forces give a 1 Bg state distortion (relative to the ground 1 Ag state) that is spectroscopically manifested in the occurrence of one main progression in the vsd normal mode, for which Dqd 6¼ 0. At that distorted geometry Dqd, the force P is balanced by harmonic restoring force kd Dqd , kd Dqd þ A FA ¼ 0, where kd is the force constant associated the d mode. Here, the summation is taken over all atoms of ˚ determined by the skeleton CoðCNÞ2 ðN2 C3 Þ2 . Using the value of kd ¼ 1:27 mdyn=A the normal coordinate analysis [105], we obtain reasonable estimates of the magnitude and direction of the excited-state distortion in this mode. This is summarized in Table 7.4 in terms of the displacements DxA ; DyA , and DzA of atoms A in the directions of the octahedral (molecular) axes x, y, and z (taken relative to the groundstate equilibrium geometry) and shown in Figure 7.7. From this figure, we see an elongation of the CoN bonds (i.e., the signs of DxN and DyN being positive) and a shortening of the CoC bonds in the octahedral skeleton CoC2 N4 , associated with a slight NC bond shortening and a CC bond lengthening in the propanediamine ligands. At the same time, the distance between the Co ion and the central C atom in the ring is nearly unaltered. Simultaneously with the tn ring moving out along the
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1
1
Table 7.4 Calculated totally symmetric forces FA ¼ FABg FAAg acting directly on atom A in the lowest excited ligand field state 1 Bg relative to the ground state 1 Ag and the corresponding excited-state distortion.
Atom
Co N3 N4 C4 C5 C6 C7 N5
Components of FA along octahedral axes (au)
Distortion (A)
xA
yA
zA
DxA
DyA
DzA
0.0 0.011 0.0 0.018 0.004 0.019 0.0 0.0
0.0 0.0 0.011 0.019 0.004 0.018 0.0 0.0
0.0 0.011 0.011 0.017 0.003 0.017 0.016 0.005
0.0 0.071 0.0 0.116 0.025 0.123 0.0 0.0
0.0 0.0 0.071 0.123 0.025 0.116 0.0 0.0
0.0 0.071 0.071 0.110 0.019 0.110 0.100 0.032
x þ y molecular axes, the N atoms and the C atoms in the chelate rings are shifted in the direction of the molecular z axes in an opposite phase, causing a flattening of the chelate ring chairs. The cyanide ligands move in, leading to a significant shortening ˚ of the metal–ligand CoC N bond length in the excited state 1 B of 0:1 A g (relative to the ground state 1 Ag ). ˚ and Using for comparison the experimentally determined value Dqd ¼ 0:32 A reexpressing the internal coordinates in terms of normal coordinates by means of the L matrix, one finds the relative change in the bond length CoN and the axial shift of ˚ and DzN3 ¼ DzN4 ¼ 0:06 A, ˚ respectivethe N atoms to be DxN3 ¼ DyN4 ¼ 0:061 A ly. The latter are deduced from the change of the bending coordinate dðC7 CoN3ð4Þ Þ involved in the vd mode. This agrees fairly well with DxN3 ¼ DyN4 ¼ DzN3 ¼ ˚ of Table 7.4. Simultaneously with the elongation of the CoN DzN4 ¼ 0:071 A ˚ (0.1 A by bonds, the CN bond in the chelate ring will be shortened by 0:02 A calculation), whereas the CC bond remains practically unchanged. Furthermore, ˚ the cyanide ligands shift toward the central ion, leading to a contraction of 0:03 A. At the same time, the C N bond length remains practically unchanged. This shows that while there is tolerable agreement with calculated bond lengthening, the significant difference occurs mainly in the contraction along the rings. To correct for these errors, we have to reestimate the restoring (rather than the distorting) forces in these parts of the molecular skeleton to obtain our relative atomic displacements. In conclusion, we note that the motion outward of the propanediamine ligands along the x þ y molecular axes is realistic since the lowest energy transition involves promotion to an antibonding dx2 y2 orbital of the cobalt ion, which has four lobes pointing along the x and y molecular axes containing the N atoms. Therefore, the force FA will have an appreciable amplitude along such normal coordinates q, for which the gradient qH=qq ¼ qU=qq of the dynamic ligand field exhibits the same directional property. This condition is best fulfilled by the vd mode.
7.2 On the Mechanism of Singlet–Triplet Interaction
Figure 7.7 Distortion of the skeleton CoðCNÞ2 ðN2 C3 Þ2 in the excited 1 Bg state of the trihydrate crystal summarized in Table 7.4: (a) along the z-axis; (b) in the xy plane.
7.2 On the Mechanism of Singlet–Triplet Interaction 7.2.1 Phosphorescence in Aromatic Molecules with Nonbonding Electrons
In this section, we will apply the knowledge gained in Chapter 3 to the analysis of triplet state relaxation in aromatic molecules with nonbonding electrons. We have chosen diazaphenantrenes (DAPs) as examples for our consideration because they are representative of an important class of organic compounds for which the decay
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time of the phosphorescence and the corresponding spectra have been measured. These compounds, as well as aromatic carbonyl compounds, are distinguished from their hydrocarbon counterparts by the presence of low-lying np states that arise from the promotion of an electron from a nonbonding orbital ðnÞ of the heteroatom (nitrogen or oxygen) to an antibonding p orbital of the molecule. In many of these molecules, the lowest energy np state is located very close to the lowest pp state and these states interact via (vibrational–electronic) vibronic coupling. As has been found from the triplet–triplet absorption [203], the T1 --T2 energy spacing in the cases of unprotonated 1,5-DAP, 2,5-DAP, and 3,5-DAP is about 1410–1530 cm1. This vibronic interaction has important effects on the radiative and nonradiative properties of the lowest excited state (singlet or triplet). We will describe this here. A compromise will be made to explain the important subject of spin-forbidden intersystem crossing (ISC) in aromatic molecules, using only this special class of aromatic molecules as an example. The difficulty in determining the mechanism of intersystem crossing in general will not be undertaken here. This would require almost a book in itself. However, to give some feeling for these problems, we shall briefly touch on the general theory at the end of this chapter. This section is divided into two parts. Preliminary to the principal discussion in this section, we describe the np --pp vibronic interaction and its effects on radiative T1 ! S0 phosphorescence transition in several representative DAPs. Second, on the basis of an analysis of these phosphorescence spectra, we calculate the T1 ! S0 radiationless transitions of these species and compare the obtained results with the lifetime measurements. 7.2.2 Radiative T1 (pp) ! S0 Transition
The electronic Hamiltonian of the system corresponding to the T1 ! S0 radiative transition involving np --pp interaction may be written as H ¼ H0 þ H 0 ;
ð7:23Þ
H 0 ¼ Hint þ HSO þ Hv
ð7:24Þ
where
represents a sum of terms: (i) the interaction Hint responsible for the radiative transition was introduced in Section 7.1 (see Equations 7.6 and 7.7), (ii) HSO is the spin–orbit interaction, (iii) and Hv is responsible for the vibronic interaction. H0 is the Hamiltonian of the free molecule composed of kinetic energy Te and potential energy Uðr; q0 Þ, where Uðr; qÞ ¼ Uðr; q0 Þ þ
X qU m
qqm
0
qm ¼ Uðr; q0 Þ þ Hv :
ð7:25Þ
7.2 On the Mechanism of Singlet–Triplet Interaction
j173
Triplet–singlet transitions are accompanied by emission of radiation. The probability is given by 2 X 3 wT ! S ¼ Cv hyT1 jei ri jyS0 i ; ð7:26Þ i where yT1 and yS0 are wavefunctions of the two states and the radiation matter interaction Hint is taken in the dipole approximation. From this expression, it can be concluded that as a first approximation, the probability of triplet–singlet transition is zero, since the triplet and singlet spin functions are orthogonal. It is possible however to obtain a finite transition probability by correcting the wavefunctions by means of perturbation theory for the spin–orbit interaction and eventually by the vibronic interaction. By including HSO , the triplet–singlet transition is a second-order process with respect to H0 (first order in Hint and first order in HSO ). By taking Hv , we consider an additional channel, making the process third order in H0 . This channel contains, in addition to the spin–orbit transition, virtual transitions between two triplet states. The corresponding matrix element (see below) depends strongly on the size of the gap T2 --T1 . If, for example, the T2 --T1 separation is small, then the contribution of the channel with Hv becomes important. From this consideration, we obtain the following rigorous expression for the electronic matrix element Va of the T1 ! S0 transition [134, 204, 205] Va ¼ VaI þ VaII ;
ð7:27Þ
where VaI ðq0 Þ ¼
X hjS0 ðr; q ÞjHint jjSk ðr; q ÞihjSk ðr : q ÞjHSO jjT1 a ðr; q Þi 0 0 0 0 : 0 E 0 E Sk T1 a k
ð7:28Þ
For notational convenience, we have set ES ðq0 Þ ¼ ES0 , and so on. The indices a ¼ x; y; z or 1; 0; 1 correspond to triplet sublevels by spin projection. At temperatures T 77 K, it can be treated as a threefold degenerate state since transitions between the three levels causing spin relaxation are very rapid and their spacing is small compared to kB T. At very low temperatures ðT 1 KÞ, spin relaxation is slow and the states behave independently. The summation in Equation 7.28 is taken over all singlet virtual states. This term represents the transition induced by direct spin–orbit coupling between T1 and S0 . The second term in (7.27) is given by VaII ðqÞ¼
XhjS0 ðr;q ÞjHint jjSk ðr;q ÞihjSk ðr;q ÞjHSO jjTi ðr;q ÞihjTi ðr;q ÞjHv jjT1 a ðr;q Þi 0 0 0 0 0 0 ðES0k ET01 a ÞðET0i ET01 a Þ i;k þR;
ð7:29Þ
where the vibronic interaction Hv is defined by Equation 7.25. The summation in (7.29) is over all singlet and triplet virtual states. The first term in (7.29) is illustrated in the diagram in Figure 7.8 and represents the transition induced by higher order mechanism involving both spin–orbit coupling and vibronic perturbation. The main contribution comes from the lowest excited triplet T1 and singlet S1 states. The
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S1
Ti
Hso Hν
T1
Hrad
S0 Figure 7.8 Energy levels and relevant coupling scheme for singlet–triplet coupling with virtual transition between two triplet states caused by vibronic interactions.
second term in (7.29) differs from the first term in that it contains singlet–singlet transitions instead of triplet–triplet transitions. Here, the corresponding energy denominators for the transition moment are large and hence the contribution to the overall phosphorescence intensity is negligible. Using the matrix elements (7.28) and (7.29), the phosphorescence spectrum for the intersystem crossing 3 T 1 !1 S0 transition can be written in terms of the line shape functions (7.19) with substitution of Vs0 ðq0 Þ¼VaI ðq0 Þ;
and (7.20a), with substitution of g
Vs0 ðq0 Þ¼ðqVaII =qqg Þ0 :
ð7:30Þ
To obtain the last expression, we have to introduce the expansion (7.25) for Hv in Equation 7.29. These line shape functions are used to describe the phosphorescence spectra of DAPs and some of their protonated analogues presented in Figure 7.9. The spectra were taken in glassy matrices at 84 K under the experimental conditions described in Ref. [206]. The similarity in structure between these spectra emphasizes that the same fundamentals are involved in the 3 T 1 ! 1 S0 transition. A discernible difference exists in the relative intensities of the vibronic bands. The most intense and highest energy line is attributed to the 0–0 transition. The other lines correspond to transitions terminating in overtones and combinations of vibrational levels of the electronic ground state. The spectra of 1,9-DAP and its protonated form, which are not shown in Figure 7.9, are similar in shape to those presented here. In the spectra of 1,10-DAP and its protonated species, a congestion of the two fundamentals at 1310 and 1620 cm1 forms the most intense band. To fix more accurately the band positions and intensities for these spectra, an intensity analysis is performed with the help of the line shape function derived in the
7.2 On the Mechanism of Singlet–Triplet Interaction
Figure 7.9 Calculated fit to the T1 S0 phosphorescence spectra of (a) 1,5-DAP; (b) 2,5-DAP; (c) 3,5-DAP; (d) 3,5-DAPH þ ; (e) 3; 5-DAPH22 þ ; (f) 2,4-DAP; (g) 2,4-DAPH þ using the parameters of Table 7.5. The
experimental (heavy lines) and calculated curves shown as dashed lines have been scaled to the same maximum and plotted as function of ~n ¼ v=2pc.
previous section. Since the experiment is done at low temperature, we have to set T ¼ 0 in Equations 7.19 and 7.20. Then the summation over all vibrational levels of the excited state T1 disappears. On setting mm ¼ 0 ðm ¼ 1; 2; . . . ; NÞ, we obtain f ðvÞ ¼ f1 ðvÞ þ f2 ðvÞ;
ð7:31Þ
where f1 ðvÞ ¼
1 X I 2 X V 2p a a fn g
2c
2 vV þ nm nm vSm0 þ c2 n o 0; 0; . . . ; 0 ni ;nj ; ; fb IN D ; b g m ;m m mn i j n1 ; n2 ; . . . ; nN m
P
ð7:32Þ
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and f2 ðvÞ ¼
2 1 h X qVaII X 2p 2vg a qqg 0 fn g m
IN
vV þ vg þ
n o 0; 0; . . . ; 0 ni ;nj Dmi ;mj ; fbm ; bmn g : n1 ; n2 ; . . . ; nN
2c P
S0 nm nm vm
2
þ c2
ð7:33Þ
In the last expression, we have taken only one promoting mode (see the discussion below). The calculated spectra are also shown in Figure 7.9. The latter are determined by fitting the experimental spectra with the formula (7.31) taking the spectroscopic parameters given in Table 7.5. An inspection of Table 7.5 reveals that three accepting modes (fundamentals) v1 ; v2 , and v3 of a0 ða1 Þ symmetry are involved in the transition – the two highest frequency CC and NC stretching modes at approximately 1370 and 1610 cm1 and one low frequency (in-plane ring deformation mode) at approximately 410 cm1. In addition to these, a nontotally symmetric vibration vg in the region 800----850 cm1 become active in inducing intensity. Apart from the vibrational frequencies in both the S0 and T1 states and the displacement ðmÞ parameters D123 ðm ¼ 1; 2; 3Þ determined by fitting the measured spectra with the calculated spectra, Table 7.5 also lists the values of the Euler angles that parameterize the rotation matrix W. By knowing the Euler angles, one can determine the remaining set of 15 (reciprocal and interactive) displacement parameters fDð123Þ g m 1 ;n2 Þ and fDðn m1 ;m2 g that are used to calculate the values of the ID in Equations 7.32 and 7.33. The nondiagonal nature of the matrix W implies that the three accepting modes are scrambled with each other. This mixing effect, though often small, can frequently be quite crucial to the calculation of the spectral intensity distribution. The contribution of the vibronically induced intensity via a S1 ðp pÞ ! T2 ðnp Þ ! T1 ðpp Þ coupling mechanism (to the allowed one) is given by the quotient a ¼ f2 =f1 and constitutes less than 5%. As no progression is observed in the intensity-promoting mode vg itself (in contrast to the three accepting modes with equally strong vibrational progressions), we note that Dg ¼ 0 and bg 1. The line shape function (7.33) for the vibronically induced band system is written in analogy to f1 ðvÞ with the exception that f2 ðvÞ originates at vg displaced from the true electronic origin V. Otherwise both systems are identical in appearance. Although no significant contribution of the vibronically induced transition mechanism to the phosphorescence intensity could be found in any of the spectra of the protonated DAPs, phenantrolines, and bezonaphthyridines (e.g., a < 0:01), we observe an increase in the induced band intensity in the case of monoprotonated 2,4-DAP. The factor a increases from 0.03 in the unprotonated form to a ¼ 0:05 in the monoprotonated form. One probable reason for this behavior of 2,4-DAP is a significant distortion from planar geometry in the protonated form. The reduction of symmetry compared to the planar unprotonated species leads to an increase of possible coupling pathways. By inspection of changes of vibrational frequencies in Table 7.5, it is found that while frequencies in 3,5-, 1,9-, and 1,10-DAP remain almost unchanged in both T1 and S0 states upon protonation, a considerable change is found for 2,4-DAP. Especially the frequency of the ring deformation mode
Table 7.5 Optimized spectroscopic parameters of the calculated T1 ! S0 spectra of DAPs and protonated analogues:vSm0 ; vTm1 and vg in cm1 w; q; y in deg. and c in cm1.
vS10
vT11
vS2o
vT21
vS30
vT31
v4
D123
ð1Þ
D123
ð2Þ
D123
ð3Þ
w
u
y
c
a
2,4-DAP 2,4-DAPH þ 1,5-DAP 2,5-DAP 3,5-DAP 3,5-DAPH þ 3;5-DAPH2 2 þ 1.9-DAP 1,9-DAPH þ 1; 9-DAPH2 2 þ 1,10-DAP 1,10-DAPH þ 1; 10-DAPH2 2 þ
1450 1400 1380 1370 1450 1450 1350 1400 1400 1400 1310 1330 1270
1350 1370 1300 1310 1380 1380 1250 1330 1330 1330 1280 1300 1230
430 490 455 460 425 410 410 430 410 410 410 410 410
390 450 410 350 330 350 350 350 360 360 380 390 390
1605 1600 1570 1540 1610 1630 1600 1620 1610 1610 1620 1620 1610
1550 1570 1510 1470 1570 1570 1550 1500 1540 1540 1580 1580 1500
830 840 820 850 800
0.90 1.00 1.15 0.95 1.27 1.25 1.20 0.80 1.00 1.10 1.25 0.85 1.40
1.00 0.93 1.06 1.20 1.35 0.80 1.00 1.40 1.00 0.90 1.15 1.40 0.70
0.75 0.82 0.98 0.90 0.60 0.90 0.60 0.80 0.95 0.90 1.26 0.65 1.02
5 5 5 5 3 5 5 10 5 5 5 10 10
5 5 0 4 9 5 5 10 0 0 1 1 0
0 0 1 1 0 0 0 10 0 0 0 3 5
130 180 140 140 180 250 370 120 250 250 200 320 320
0.03 0.05 0.05 0.05 0.045
7.2 On the Mechanism of Singlet–Triplet Interaction
Compound
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v2 shows a comparatively strong increase of about 12% in both electronic states, which indicates a strong alternation of the force field in the protonated form. In conclusion, some remarks are devoted to the line width c. From Figure 7.9, we infer that an increasing width c leads to broad and smooth phosphorescence bands with complete loss of detail of individual vibronic transitions (Figure 7.9d, e, and g). Information on the broadening is less unambiguous, but it seems realistic, however, to attribute this broadening to an enhancement of intermolecular interaction due to hydrogen bondings in the protic matrix. The line broadening is less pronounced in the case of 2,4-DAPH þ , where in contrast to 3,5-, 1,9-, and 1,10-DAP the solvent did not contain water. 7.2.3 Nonradiative Triplet-to-Ground State Transition
The treatment in the preceding section is now extended to the calculation of nonradiative transition for three representative DAPs [207]. The results of these theoretical calculations are compared with the experimentally determined lifetime measurements. The experimental setup for these measurements consisted of a Bruker ER 200 D spectrometer in combination with a phosphorescence spectrometer. Samples of 1,3-, 2,4-, and 3,5-DAPs were dissolved in glass forming methanol/ ethanol (1 : 4) and cooled down to 80 K inside the cavity. Sample concentration was 1 104 mol=l. Triplet state population was stimulated by using a 500 W highpressure Hg lamp in the region 300360 mm. The emission was analyzed using a Zeiss HB3 grating monochromator and detected, employing a cooled photomultiplier (RCA 4840). Triplet state lifetimes were measured by monitoring the decay of the Dm ¼ 2 signal. The decay curves were exponential over at least a decade in the intensity. The simultaneous measurements of phosphorescence and ESR spectra in combination with the results of triplet lifetime measurements allow us to separate out the nonradiative decay rate constant wnr from the observed lifetime t. For this, we need the phosphorescence quantum yield wph for each DAP. For phenanthrene dissolved in ethanol at 77 K, wph ¼ 0:12, [208], which was determined on the basis of an ISC quantum yield of 0.86 [209]. As a consequence of the similarity of experimental conditions (solvent, temperature), we may choose these values as a standard for the DAPs from among a number of available date [208, 210–213]. The phosphorescence quantum yield wph is given by the general relation [214] wph ¼
wr w ; wr þ wnr ISC
ð7:34Þ
where wISC is the ISC quantum yield and wr þ wnr denotes the total decay rate constant (averaged over the triplet sublevels). With wr þ wnr ¼ 0:2708 for phenanthrene determined from the phosphorescence lifetime, wr is calculated to be 0.038. The phosphorescence intensity is Iph ¼ kc. Here, c denotes the concentration of triplet molecules that is proportional to the observed Dm ¼ 2 signal; that is,
7.2 On the Mechanism of Singlet–Triplet Interaction Table 7.6 Radiative and nonradiative decay parameters for phenanthrene [207] and the DAPs.
Compound
Wp
tp (s)
wr (s1)
wnr (s1)
Phenanthrene 1,3-DAP 2,4-DAP 3,5-DAP
0.12 0.08 0.05 0.08
3.70 1.66 2.35 0.97
0.038 0.08 0.16 0.17
0.23 0.52 0.27 0.87
IESR ¼ a c with a taken as an apparatus constant [215]. Denoting the standard values 0 0 for phenanthrene by Iph ; wr0, and IISC , respectively, we can write Iph wr IESR ¼ 0 0 ; 0 Iph wr IESR
ð7:35Þ
from which we obtain an estimate of the radiative constant wr of the DAP. For this, the left-hand side of Equation 7.35 is determined from the ratio of the areas of the corrected phosphorescence spectra. The obtained values wr ; wt ¼ wr þ wnr , and wnr together with the triplet lifetime t and phosphorescence quantum yield wph are presented in Table 7.6. From the data in Table 7.6, we note that the radiative rates of DAPs wr < wnr and the lifetimes t are governed by the nonradiative rate constant t1 ffi wnr . 7.2.3.1 Theory and Application In this section, we want to study the mechanism of nonradiative transitions between triplet and singlet states in DAP. It is apparent from the foregoing discussion that the spin–orbit coupling between a triplet Ti ðnp Þ and the singlet ground state S0 is very much larger than the coupling between the triplet T1 ðpp Þ and the ground state. Therefore, we write the T1 ! S0 process as T1 ! Ti ! S0 process, where S0 provides the manifold of states for the nonradiative transition. In spin-forbidden transitions, the perturbation is H 0 ¼ HSO and the rate expression in first order for radiationless process T1 ! S0 in the zero-temperature limit is given by wnr ¼
2 2p X X T1 a y0 jHSO jySn0 r hVEnS0 : h a n
ð7:36Þ
r is the density of final vibronic states fnm g near hV given by a Lorentzian 1 r hVEnS0 ¼ p
hV
P
C
hvSm0 fnm g nm
2
þ C2
;
ð7:37Þ
which is characterized by a finite (average) width C. The latter indicates the effect of radiation and radiationless damping, configuration mixing, interaction with the bath modes, and other kinds of broadening mechanism in the molecular eigenstates. The summation in (7.36) includes the contribution of the individual transitions from the
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components of the quasi-degenerate sublevels a of the triplet state T1 . The y are total wavefunctions of the system; y0T1 a is the zeroth-order vibronic state of the first triplet state and ySn0 is the manifold of vibronically highly excited levels of the singlet ground state S0 . In the pure spin adiabatic BO representation, the matrix element of intersystem crossing between the T1 state and the singlet state S0 is given by ðxSn0 hjS0 jHSO jjTa1 ixT0 1 Þ, where jTa1 ðr; qÞ is a purely electronic wavefunction of the triplet sublevel T1a ði:e:; T þ ; T and Tz Þ evaluated at the nuclear geometry described by q and jS0 ðr; qÞ is the electronic wavefunction of the ground singlet state. xT0 1 and xSn0 are the corresponding multidimensional nuclear wavefunctions, with 0 ¼ ð01 ; 02 ; . . . ; 0N Þ and n ¼ ðn1 ; n2 ; . . . ; nN Þ being the associated sets of vibrational levels. At 77 K and higher temperatures, the three triplet sublevels T1;a ði:e:; T þ ; T ; and Tz Þ can be treated as a threefold degenerate state. Using a Herzberg–Teller expansion in a crude adiabatic electronic wavefunction at the equilibrium geometry q0, the BO wavefunction jTa1 ðr; qÞ can be written as jTa1 ðr; qÞ
¼
jTa1 ðr
: q0 Þ þ
X X jTai0 ihjTai0 ðqU=qqg Þ0 jTa1 i i6¼1
a0
E T1 ðq0 ÞE Ti ðq0 Þ
qg ;
ð7:38Þ
where E Ti ðq0 Þ is the electronic energy of the triplet state Ti and the electronic wavefunctions on the left are np triplet states, all understood to be evaluated at q0 . In that case, qg is an out-of-plane coordinate [216]. Using this form of the wavefunction of the triplet states, the transition probability for intersystem crossing T1 ! S0 is the sum of the probabilities via all coupling routes wnr ¼
2p X X g 2 T1 S0 2 h T1 S0 2 Va x0g qg xng x0 xn0 r hVEnS0 ; h a n
ð7:39Þ
where Vag
X X jS0 jHSO jjTai0 jTai0 ðqU=qqg Þ0 jTa1 ¼ : E T1 ðq0 ÞE Ti ðq0 Þ i6¼1 a0
ð7:40Þ
The primed 00 and n0 in Equation 7.39 exclude the promoting mode g that g contributes to Va via hjTai0 ðqU=qqg Þ0 jTa1 i. In writing Equation 7.38, we have S0 assumed that hj jHSO jjTa1 i is negligible relative to hjS0 jHSO jjTai0 i; that is, we rule out the direct spin–orbit mechanism. Substituting the density-of-states function (7.37) into Equation 7.39 and proceeding as in Chapter 3, we obtain 2 wnr ¼ 2 h
X 2 V g a
! 1 ð
a
~ g ðtÞGN1 ðtÞ; dt exp½iVtC h1 jtjK
ð7:41Þ
1
~ g ðtÞ is defined by Equation 7.14. Since the experiment was carried out at low where K temperature (mm ¼ 0 for all m and cothð hvg =2kB TÞ 1), Equation 7.41 can be simplified and written finally in the form
7.2 On the Mechanism of Singlet–Triplet Interaction
! X g 2 X 2 h wnr ¼ Va h 2vg a fn g m
IN
0; 0; . . . ; 0 : n1 ; n2 ; . . . ; nN
C 2 P hV hvg m nm hvSm0 þ C2 ð7:42Þ
Both the ground and excited surfaces can be quite complicated since they are of high dimensionalities. Therefore, to obtain a complete description of the T1 ! S0 radiationless transition, the calculation will now be extended (in comparison to the calculation in the preceding section) by including further vibrational degrees of freedom. If the vibrational frequency is large, fewer vibrational quanta are required to bridge the energy gap between the T1 and S0 states and the most interesting dynamics occur in the subspace of high-frequency CH or NH stretching modes. Moreover, since the subspace of the highest frequency modes may safely be assumed as separable from the other subspace (of the skeletal modes), the overall vibrational factor may therefore be written in terms of 0; 0; . . . ; 0 0; 0; 0; 0 0; 0; . . . ; 0 IN ¼ I4 IN4 ; ð7:43Þ n1 ; n2 ; . . . ; nN n1 ; n2 ; n3 ; n4 n5 ; n6 ; . . . ; nN comprising the four skeletal modes observed in the phosphorescence spectra on the one hand and the high-energy CH stretching modes on the other. The molecular parameters for the three accepting modes are the same as those obtained from the analysis of the phosphorescence spectra. Following the same line of reasoning, the fourth mode in Equation 7.41 is the promoting mode, which is an asymmetric skeletal vibration, with frequency vg ¼ 800850 cm1 and zero displacement Dg ¼ 0. For the ground-state high-frequency CH accepting modes, we take average values obtained from the normal coordinate analysis of phenanthrolines [217]. The corresponding frequencies in the triplet state are expected to be lower by about 1–10%. Comparatively little is known about appropriate values of reduced origin shifts DCH ¼ ðvCH =hÞ1=2 DqCH , where DqCH denotes the dimensioned shift. The most reliable estimates of these deltas lie in the range 0:01----0:1 [218, 219]. In Equation 7.42, the overall vibrational factor is additionally convoluted with the Lorentzian distribution, leading to a density-of-state weighted vibrational overlap factor. At the same time, the summation over the vibrational quantum numbers nm is subject to P the requirement of energy conservation V vg þ fnm g nm vTm1 with an uncertainty given by the width c ðhc ¼ CÞ of the vibrational levels in the manifold S0 . The values of the latter are obtained from the fit to the experimental phosphorescence intensities. Table 7.7 lists in the last row the numerical values of the density-of-states weighted vibrational overlap in unit of centimeter, the inverse of wave numbers; only seven modes are included, as the other poor accepting modes are not sufficiently known. In a spin-forbidden transition in DAPs, the change of the positions of the N atoms can alter the following: (i) the number and effectiveness of the accepting and promoting vibrations, (ii) the T1 –S1 energy gap, (iii) the spin–orbit coupling g contribution to Va , and hence the magnitude of the whole transition rate S1 ! T1 . The first two points are fully included in the calculation of the density-
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Table 7.7 Spectroscopic parameters and the corresponding density-of-state vibrational overlaps
for selected DAPs (the Duschinsky rotation matrices for 2,4-DAP and 3,5-DAP can be derived directly from the Euler angles given in Table 7.5; the rotation matrix of 1,3-DAP is identical to that of 2,4-DAP). 1.3-DAP
2.4-DAP
3.5-DAP
Vibrational frequencies (cm1) vT2 1
380
390
320
vS2 0
400
430
425
vT1 1
1350
1350
1380
vS1 0
1400
1450
1450
vT3 1
1550
1550
1570
vS3 0
1600
1605
1610
v4
840
830
800
vT5 1
2700
2700
2700
vS5 0
3000
3000
3000
vT6 1
2750
2750
2750
vS6 0
3050
3050
3050
vT7 1
2800
2800
2800
vS7 0
3100
3100
3100
Dimensionless displacements ð1Þ
D123 ð2Þ D123 ð3Þ D123 ð4Þ D4 ð5Þ ð6Þ ð7Þ D567 ; D567 ; D567 1
Linewidth c (cm ) X 0 0 I7 n 1 n2
a)
0 rðcm1 Þ1 a) n7
0.90
0.90
1.27
1.25
1.00
1.35
0.95
0.75
0.60
0.00
0.00
0.00
0.10
0.10
0.10
130
130
0.7390 6
10
130
0.6166 6
10
0.8987 6
10
The quantities in the last row (inverse of energy) are given in units of wave numbers 1=l, where l is the wavelength. For conversion between energy and wave numbers, use the relation 1=l ¼ E=2pch. For instance, 1 eV energy corresponds to a wave number of 8:0654 103 cm1 .
of-states weighted vibrational overlaps, which are nearly constant within the DAPs listed in Table 7.7. The alternation for the electronic factor presents interesting difficulties because the convergence of the H–Texpansion (7.38) is very slow. CNDO/ S-CI calculations of the spin–orbit matrix elements hjS1 jHSO jjTai0 i (by using molecular wavefunctions in the crude BO approximation) have shown that many of the triplet spin sublevels are coupled to S1 yielding hjS1 jHSO jjTai0 i 1----10 cm1 (only the z components of jTai0 do not contribute to the mixing). When complete interactions
7.2 On the Mechanism of Singlet–Triplet Interaction
between these states are invoked, the interplay between the excited-state energies g g E Ti ðq0 Þ and spin–orbit coupling in Va destroys any simple relation for Va (Equation 7.38). The uncertainties in the energies of these states will result in large uncertainties in the estimation of the individual rate constants of the sublevels of the triplet state T1 . Furthermore, the need to include vibronic mixing into the calculation further complicates the matter. The difficulties noted above can be avoided by comparing the data presented in Tables 7.6 and 7.7. The nearly invariant wnr listed in Table 7.6 and the calculated vibronic overlaps reported in Table 7.7 indicate that neither the electronic nor the vibrational factors vary essentially within the group of investigated DAPs. The former can be estimated by means of Equation 7.42, using the data in Tables 7.6 and 7.7. P 1=2 g 2 contributes These imply that the electronic matrix element ðh=2vg Þ1=2 a Va terms of the order of 103 cm1 . This is obviously an expected result for the investigated nitrogen heterocyclic compounds, and it is an indication that although np --pp vibronic interaction in DAPs makes a substantial contribution to the electronic term, the mixed np triplet states are well separated in energy from the T1 state. If this were not the case, the contribution of the np ----pp vibronic coupling g to the electronic factor Va would be stronger and the shape of the potential energy surfaces of these mixed triplet states and their energy levels would be affected by the pseudo-Jahn–Teller interaction (see Appendix K). From the form of the rate constant for radiationless transition (Equations 7.40–7.42) and the discussion accompanying Equation 7.42, we can conclude that there are at least three major factors that determine the probability of the transition T1 ! S0 : a. The change in the electronic (orbital) configuration between states jT1 and jTi by the motion of nuclei, that is, hjTi jHv jjT1 i, b. The abrupt change of the spin configuration in state jT1 relative to state jS1 , that is, hjS1 jHSO jjT1 i, and finally c. The structure and motion of the nuclei in state jT1 relative to those in jS1 . These factors usually contrive to place a prohibition on the maximum (zero point motion limited) transition rate that is usually of the order of 1013 ----1014 s1 . We can, therefore, conclude that the observed radiationless transition always proceeds at a slower rate. We shall see in Section 7.6 that potential surface crossing remove the above restrictions somewhat for radiationless processes. 7.2.4 Remarks on the Intersystem Crossing in Aromatic Hydrocarbons
The theory of intersystem crossing in aromatic molecules has been developed in a series of investigations [90, 205, 220–227]. The mechanism of intersystem crossing is here more complicated than in the case considered previously for aromatic molecules that contain heteroatoms with n electrons [221]. One of the reasons for this is that spin–orbit coupling in aromatic hydrocarbons is generally small compared to that in
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aromatic molecules containing heteroatoms with nonbonding electrons. It is even expected that the magnitude of the spin–orbit coupling in aromatic hydrocarbons is smaller than that of vibronic coupling or at most of comparative magnitude. Another complication is presented by the difficulty in determining the mechanism or pathway of intersystem crossing. It is generally recognized that several possible pathways may contribute to the intersystem crossing in aromatic hydrocarbons and that the promoting modes for intersystem crossing are directly related to these mechanisms. Generally, the promoting modes can be classified into groups according to the perturbation causing intersystem crossing. The direct S1 --T1 process governed by vibronic spin–orbit coupling matrix elements hSjHSO jTi falls into one group. The coupling other group employs an indirect mechanism S1 ----T2 ----T1 including vibronic q=qq matrix elements that involve the nuclear momentum operator hS 1 g Si i or hT1 q=qqg Ti i. In the particular case of intersystem crossing in benzene S1 ð1 B 1u Þ ! T; CH out-of-plane vibration acts as a dominant promoting mode for both S1 --T1 direct and S1 ----T2 ----T1 indirect mechanisms. The promoting mode that induces the singlet–triplet transition in pentacene guest in p-terphenyl is assigned to the lowest frequency out-of-plane (butterfly) vibration of pentacene [227]. To find a really compelling set of arguments, however, it is necessary to delve rather deeply into the literature on the subject.
7.3 Comment on the Temperature Dependence of Radiationless Transition
As a further illustration of the general formalism developed in Chapter 3, we discuss the dependence of radiationless transition on temperature. One can distinguish clearly in Equations 3.75 and 3.77 between two contributions (of difference sources) to the temperature dependence. The dominant effect is given by the coth factor associated with the promoting modes. The second contribution is associated with the large number of accepting modes. At T ¼ 0, all mm values in Equation 3.77 have to be zero. This means that the excited vibronic levels of the initial state jsi are not populated. As T increases, some of the mm s take values other than zero; that is, some of the normal modes of the initial electronic state will be thermally excited, particularly those of lower frequencies and for which displacement parameters Dm are appreciable. Acceptor modes of high frequency do not contribute to the temperature dependence. To analyze these two contributions separately, we recall that the expression for the nonradiative decay rate bears a strong resemblance to the expression for the optical transition, gaining intensity via a vibronic coupling mechanism (as emphasized in Section 7.1). The latter is characterized by false origins displaced from the true electronic origin hV by one quantum of the promotion modes. It can therefore be regarded as a symmetry-forbidden emission process, where the nontotally symmetric modes g, which induce the optical transitions, act as promoting modes (see Equation 7.20a). Figure 7.10 illustrates such a situation. This example shows the C7 ð2 T 2g Þ ! C8 ð4 A 2g Þ phosphorescence spectrum of Rb2 TeCl6 crystal doped with ReCl6 2 at selected temperature between 20 and 240 K, [228] employing the 633 nm
7.3 Comment on the Temperature Dependence of Radiationless Transition
Figure 7.10 Emission spectra of Rb2 TeCl6 : ReðIVÞ (powder sample) in the temperature range from 20 to 240 K; lexc ¼ 633 nm. The spectra of Rb2 TeCl6 : ReðIVÞ, revealing peaks determined by the v6 ; v4 ; v3 bands (fundamentals) of odd parity
of the complex ReCL6 2 . The peaks v6 ; v4 are the corresponding hot bands. 0–0 is the pure electronic origin of the C7 ð2 T 2g Þ ! C8 ð4 A 2g Þ transition; l and l are the lattice vibration regions.
line produced by a He–Ne laser. The typical feature characteristic for such octahedral complexes are that the sidebands off the true electronic origin are build upon several peaks labeled by v3 ; v4, and v6 (often also designated as Stokes sidebands), where 1 2 ; T1u , and T2u vi ði ¼ 3; 4; 6Þ refer to the three (odd parity) promoting modes of T1u 2 symmetry of the complex ion ReCl6 . In such a manner, the spin-forbidden C7 ð2 T 2g Þ ! C8 ð4 A2g Þ transition steals intensity from the nearly spin-allowed C7 ð4 T 2g Þ ! C8 ð4 A 2g Þ band due to vibrational borrowing. The bands v4 and v6 are assigned to the corresponding hot bands (the so-called anti-Stokes sidebands) and the peak at about 13660 cm1 to the even parity vibronic sideband v2 ðEg Þ. To detect v3 , the temperature applied should be high enough for populating the corresponding vibronic level in the electronic excited state C7 ð2 T 2g Þ of the complex. The position of the bands v6 ; v4 , and v3 relative to the 0–0 line are 129ð1Þ; 169ð2Þ, and 323ð3Þ cm1 , respectively. As the temperature rises, the peak heights in the spectra of Figure 7.10 are nearly constant while the corresponding half-widths c grow,2) so that the integrated intensities increase with increasing temperature according to the coth law ½cothðhvg =2kB TÞ þ 1. Let us now suppose for the sake of simplicity that the transition induced by the three odd parity modes is accompanied by a total symmetric accepting mode of frequency va1 ða ¼ s; 0Þ. This is the situation that most often occurs in a series of spectra of transitionmetalionsthathavebeeninvestigatedbythepresentauthor(see,forexample, Ref. [100]). In this case, the overall line shape (see Equation 7.20b) is described by ! X X m1 T s 0 ; ð7:44Þ wrad ¼ f0 v hvs1 =kB T I1 D ;b m1 v1 n1 v1 exp m1 1 1 n1 m1 ;n1
m1 ;n1
2) We are restating here conclusions obtained Chapter 4.6 about the temperature dependence of wvr ¼ cj h.
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where f0T ðvÞ represents the experimentally observed spectrum plotted in Figure 7.10 at several temperature T, and m1 and n1 are the vibrational quantum numbers of the (totally symmetric) progressional mode in the excited and ground states, respectively. The overall spectrum thus consists of a single progression in v1 , and the individual P members in this progression are given by f0T v m1 ;n1 m1 vs1 n1 v01 . Unfortunately, the second, third, and so on members in the progression could not be depicted in Figure 7.10 in order to maintain graphical legibility. A corresponding band analysis carried out on this part of the spectrum yields vs1 ¼ 346cm1 ; D1 ¼ 0:3--0:4, and b1 ¼ 0:99 [100]. With these values available, the relative (integrated) intensities wrad of the overall spectrum may be calculated. In most practical calculations for temperatures up to 250 K, one rarely needs to carry the expansion in (7.44) beyond the first three lowest vibrational levels m1 ¼ 1;2;3 of the excited state. That this is a general conclusion is clear after the results obtained on the behavior of the distribution I1 for small values of D1 . For m1 3, the distribution I1 increases as a function of n1 up to a level of approximately 1 at n1 ¼ m1 , at which point it begins to decrease more rapidly than expðm1 hv1 =kB TÞ (Figure 4.3). Furthermore, from peak positions of Stokes and anti-Stokes sidebands, which yield the frequency factors of b6 ¼ 128=129 ¼ 0:99 and b4 ¼ 168=169 ¼ 0:99, it is evident that the curvature of the potential surfaces in the subspace spanned by the vibrational coordinates of the v6 and v4 modes is identical in the excited and ground electronic states. This gives an additional test of the validity of the coth law that was derived under the assumption of identical frequencies of the promoting modes in both considered electronic states. The temperature dependence of the intensities in the three Stokes sidebands is shown in Figure 7.11 (solid curves). The latter are calculated for two values of D1 , namely, D1 ¼ 0:4 and D1 ¼ 0:8. For comparison, the coth factor is also depicted (dashed curves). This result suggests that the temperature dependence comes mainly from the coth dependence of the active (promoting) modes. A deviation from the coth dependence comes from the third factor in Equation 7.44 whose values are < 1. In the case of strongly coupled states, when the potential surface of the excited state will show a large shift (Dq1 ) relative to the ground state, the situation is quite different. Here, an energy conserving summation over all m1 and n1 levels of the accepting mode (and only these) will continue to contribute appreciably to the nonradiative transition rate (Figures 4.7 and 4.8).
7.4 Effect of Deuteration on the Lifetimes of Electronic Excited States 7.4.1 Partial Deuteration Experiment
In a series of experiments [229, 230], a dramatic increase in the lifetime of the triplet state in aromatic hydrocarbons was measured when they were completely deuterated. At 77 K, naphthalene in a durene solid solution has a 2.5 s lifetime (inverse of the
7.4 Effect of Deuteration on the Lifetimes of Electronic Excited States
Figure 7.11 Transition rates wi ; ði ¼ 3; 4; 6Þ versus temperature T calculated from Equation 7.44 with b1 ¼ 0:99 ðb1 ¼ 0:005Þ and D1 ¼ 0:4 and for D1 ¼ 0:8 using spectroscopic data as derived for the present system; the coth law is indicated by the dotted lines.
phosphorescence decay rate) versus 16.2 s for naphthalene-d8 . Determinations of the decay rates of seven partially deuterated naphthalene species [231, 232] show a linear dependence on the number of deuterons in the molecules and a little or no dependence on the position of substitutions (Table 7.8). Studies on three other systems suggest that this phenomenon is general. The rate of intersystem crossing in the fluorescing state 1 B 2u of benzene was found to be twofold greater in C6 H6 than in C6 D6 [234]. A similar effect was recorded for azulene [235]. The lifetime of the triplet pp state of acetophenone in H3 PO4 at 77 K and two of its deuterated derivatives exhibit a nearly linear dependence on the number of deuterons in the molecules [233]. The phosphorescence quenching of a number rare earth ions ðSm2 þ ; Eu3 þ ; Tb3 þ ; Dy 3 þ Þ in D2 O solution is strictly linear with the concentration of H2 O [236]. It was found experimentally that deuteration reduces the phosphorescence decay rate of Cr ðIIIÞ–amine complexes by a factor of 50–100 at low temperatures [237, 238]. The major routes of this nonradiative process are assumed to be S1 ! T1 or S1 ! T2, with S1 ! S0 assumed to be unimportant, i.e., WS1 T1 WS1S0. According to our results obtained in Chapter 6, there is a simple relation between the rate of intersystem crossing WS1 T1 and the width Ds1 of the relaxing doorway state
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Table 7.8 Triplet lifetimes of partially deuterated molecules. Adopted from Ref. [232].
Compounds
Position of deuteration
Lifetime (s)
References
Naphthalene in durene at 77 K
None 1 2 (in durene-d14 ) 1,4 1,4,5,8 2,4,6,7 (in durene-d14 ) 1,2,3,4,5,6,7,8 None a; a; a 2,3,4,5,6
2.5 0.1 2.8 0.1 2.6 0.1 3.4 0.1 5.4 0.2 4.8 0.2 16.2 0.3 1.51 1.85 2.25
[229] [232] [229] [232] [229] [229] [229] [233] [233] [233]
Acetophenone in H3 PO4 at 77 K
S1 ; namely, WS1T 1 ¼ Ds1 =h (Equation 6.23). This line width is caused by the interaction between the zeroth vibronic state of the upper state ys m ¼ js xs m and 1 1 1 the manifold of highly excited vibronic levels of the lower electronic state yT n ¼ jT xT n that are degenerate with it. To complete the theory of deuteration 1 1 1 it remains to consider (under the assumption made above) the manner in which the phosphorence lifetime of the lowest triplet state changes under the influence of deuteration. To do this, we consider the decay rate from the lowest triplet T1. In deriving the expression for the nonradiative decay rate, we must distinguish clearly between the promoting modes g, which are responsible for the electronic transition, and the large number of accepting modes m, which act as a sink to accept the electronic energy. Whether part of electronic energy can be directly converted into the lattice modes (intermolecular vibrations) or not depends on the magnitude of the g ID and of the matrix element Va . The promoting mode g changes its quantum number according to the propensity rule; that is, it must gain or lose one quantum of vibration energy, whereas the accepting modes are limited in their change of quantum numbers only by the density-of-states weighted ID. The summation over all possible distributions of the vibrational quantum numbers n1 ; n2 ; . . . ; nN and m1 ; m2 ; . . . ; mN must be included here to bridge the electronic energy gap plus thermal energy if the temperature is not zero. For large electronic energy gaps, the vibrational overlap integral decreases rapidly with increasing vibrational quanta. Thus, for radiationless transitions of aromatic hydrocarbons involving large energy gaps, the vibrational factors are expected to be dominated by the CH stretching modes, which are the highest frequency oscillators in aromatic molecules. The dramatic reduction in the T1 ! S0 intersystem crossing rate accompanying deuteration of aromatic hydrocarbons supports such a conjecture. On the other hand, the bond length and frequency changes of the CH stretching modes upon electronic excitation are small compared to those for the CC modes, so that CC stretching becomes important for transitions involving relatively small energy gaps. Out-ofplane bending modes are considered to be unimportant in aromatic hydrocarbons (for any energy gap) since the magnitude of the frequency as well as frequency change and equilibrium displacement of these modes is small [239–243]. This observation is transferable to Cr ðIIIÞ–amine and Cr ðIIIÞ–alkylamine complexes
7.4 Effect of Deuteration on the Lifetimes of Electronic Excited States
with CrN6 skeletons, where the high-frequency NH accepting modes are dominant in the radiationless deactivation of the lowest doublet 2 E g [244, 245]. On substituting the hydrogen of ½CrðNH3 Þ6 3 þ by alkyl groups of different numbers of NH bonds, the skeleton CrN6 is conserved and the ligand field changes only slightly. As the number of active hydrogen atoms increases, an approximately proportional increase in the nonradiative decay rate is observed. The conclusion regarding the minor role of out-of-plane vibrations in aromatic hydrocarbons is not, however, expected to hold for nitrogen heterocyclic and aromatic carbonyl compounds in which the lowest energy np and pp states are vibronically coupled via some of these modes [216]. If the energy gap between these states is smaller than the vibronic interaction energies, the lower state, which will be a mixture of np and pp states, should be strongly distorted ðb 6¼ 1Þ and it may even be displaced ðD 6¼ 0Þ along an out-of-plane coordinate. This frequency and the potential surface distortion in the configuration space can lead to a large increase in the vibrational factor (ID) for radiationless transition, which is known to depend strongly on the frequency changes and displacements of the accepting modes. In Section 7.2, we have discussed this characteristic in some detail. Returning to the simpler case of aromatic molecules and Cr ðIIIÞ complexes, where the high-frequency vibrations act as accepting modes, we will give a qualitative explanation for the partial deuteration effect. The large number of vibrational degrees of freedom allows us to arrange the vibrations of the molecule into two groups: those that correspond to the high-frequency CH or NH stretching modes ðiÞ and those that consists of the vibrational set of all other modes ð jÞ. Assuming the validity of statistical limit, the nonradiative decay rate of the lowest triplet state in the zerotemperature limit can be written as ! ! k X vg X g 2 X 0; . . . ; 0 wnr ¼ Va rðVvg nvi ÞIk n; ai ; b INk ; nk þ 1 ; . . . ; n N 2h a i n;fnj g
ð7:45Þ
where it is assumed for simplicity that only one mode g promotes the nonradiative transition. The high-frequency modes are represented in (7.45) by a k-fold ID with k being the number of highest frequency oscillators in the molecule. The remaining low-frequency skeletal modes j ¼ k þ 1; . . . ; N are represented by INk. The quantum numbers n and nk þ 1 ; . . . ; nN are subject to the requirement of energy conservation P Vvg N j¼k þ 1 nj vj þ nvi , where V is the energy gap between the lowest triplet and final ground states. rðVvg nvi Þ is the density of vibronic states fnj g in the range near the energies hðVvg nvi Þ. The ID Ik can be expressed as a k-fold convolution of one-dimensional IDs, Ik ¼ I1 I2 I1 , or explicitly ! k X X Ik n; ai ; b ¼ I1 ðn1 ; a1 ; bÞI1 ðn2 ; a2 ; bÞ I1 ðnk ; ak ; bÞ; ð7:46aÞ i¼1
n1 þ n2 þ þ nk ¼n
where the frequency factor bi ¼ ð1bi Þ=ð1 þ bi Þ ¼ vli vsi = vli þ vsi for all highfrequency modes has been assumed to be equal b. For this same example, the effective displacement parameter in Ik is given by
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a¼
k X i¼1
ai
k k 1X 1 X D2i ¼ bsi 0 k2i ; 2 i¼1 2 i¼1
ð7:47Þ
so that the high-frequency modes contribute to the nonradiative decay rate by the sum of the normal mode displacement parameters ai or, in other words, by the sum of the squares of ki . Because of the sensitive dependence of the ID Ik on the magnitude of the displacements, this result predicts significant increase in the rate of electronic relaxation toward lower values of n and vice versa. Furthermore, since the multidimensional distribution Ik depends on n, which arises by summation over all combinations of quantum numbers ðn1 ; n2 ; . . . ; nk Þ, it can be regarded as weighted by the exact density of states associated with the high-frequency modes. This can be seen in the increase of the values of Ik with increasing degeneracy k (Figures 4.5–4.8). For a rough estimation, we may put expression (7.46a) into a simpler form if we assume now b ¼ 0 (no frequency changes). Then Ik ð0; n : a; 0Þ ¼ exp ðaÞ
an ; n!
ð7:46bÞ
where a is given by Equation 7.47. For a small number of a or even moderately large number a, Ik falls off rapidly with increasing ni . We see that large numbers ni are not favorable for acceptance of electronic energy. Thus, normal modes with high frequencies, which need a smaller number of vibrational quanta to bridge the electronic energy gap, will be favored in the electronic relaxation. This implies that in aromatic molecules the CH stretching modes of vCH 3000 cm1 as well as the NH stretching modes in Cr ðIIIÞ complexes are important in radiationless deactivation. Deuteration of these solute molecules is accompanied by a drastic decrease in the rate of electronic relaxation (and hence increase in the lifetime of the excited states) due to the lower CD or ND frequencies ðvND 2400 cm1 Þ, respectively. From this, it appears that the description of the multimode problem using separable harmonic oscillators for the high-frequency modes is a good approximation for the analysis of a deuterium experiment. From the available data discussed above, the isotope effect in the T1 ! S0 radiationless transition is nearly independent of position; it depends mainly on the number of deuterons. This supports the assumption that the CH stretching modes are not, in general, promoting modes because any dependence on position can be ascribed to the normal modes inducing the transition. The weak promoting contribution can be gauged from the small difference in phosphorescence decay rate of pairs of partially deuterated naphthalene isomers listed in Table 7.8. A similar situation occurs in the series of Cr ðIIIÞ alkylamine complexes, discussed above, where the high-frequency ligand vibrations are not mixing modes. The decay of the lowest doublet 2 E g state occurs predominantly by radiationless transition. With the same number of substituents having high-frequency NH vibrations, the vibrational factors governing the radiationless transition are essentially the same. A position dependence of the substituents on the radiationless rate constant is exclusively due to an effect on the electronic matrix element h4 T2g jHint j2 E g i, where
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals
Hint ¼ HSO þ Hvib . The latter differs from zero only for pathways related predominantly to the skeletal CrN6 vibrations. In the case of nitrogen heterocyclic compounds, the situation is more complicated but it is nonetheless possible to uniquely identify the promoting mode; the El-Sayed rule determines the path of the intersystem crossing.
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals 7.5.1 Transport Phenomena in Doped Molecular Crystals
For the study of time-resolved processes such as discussed in Chapter 6, but with many strongly coupled states in the manifold fyl g, a closed-form solution cannot be carried through analytically and approximate treatments are necessary. This is not the case when solving Equation 6.58 for many states, which can always be integrated by numerical methods. All require modern, high-speed computers for their execution and the development of numerical recipes to handle large determinants. Furthermore, numerical solutions may often be obtained much more easily than closed-form solutions and may be sufficiently accurate, as the physical situation warrants. On the other hand, the closed-form solution given by Equation 6.58 serves as a convenient introduction to pursue much more difficult problems when possible. The spirit of the analysis that follows deals with transport phenomena of electronic excitations in doped molecular crystals. The theory uses an effective Hamiltonian stated implicitly in Appendix A to account for intramolecular excited-state depopulation and electronic excited-state transfer by multistep migration among an assembly of guest molecules. When the number of guests becomes large, the defining representation of the Hamiltonian is therefore a matrix of high dimension. The mathematical solution of such a problem is carried out by numerical integration and the result of the calculation is presented as a time-dependent position of excited states of dipole–dipole coupled molecules in the bulk of a crystal. Preliminary to the principal discussion of this section, we shall give a brief review of the experimental system used and the technique of lifetime measurements in high-concentration crystals. 7.5.2 The System Pentacene in p-Terphenyl
As the case of a mixed crystal, we consider p-terphenyl doped with pentacene. In the low-temperature p-terphenyl lattice, pentacene exhibits four distinct sites denoted by O1 ; O2 ; O3 ; O4 . These sites result from the p-terphenyl phase transition at 190 K, in which p-terphenyl ring rocking freezes out [246]. The final ring distribution produces a low-temperature unit cell that contains conformationally different p-terphenyl
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a-axis M2
b-axis
M1
M1
M3 M2
M4 M1
M4 M1
M2 M3
M2
Figure 7.12 Schematic representation of the pseudo-monoclinic elementary cell of crystalline p-terphenyl (low-temperature modification), viewed in projection onto the (0 0 1) plane. After Ref. [9]. The discussion in the text refers to the b domain structure shown here; the a domain structure is related to it by
M1
simple mirror symmetry. The elementary cell contains four nonequivalent p-terphenyl molecules denoted as M1 -- M4 . The open bars show the orientation of the two outer phenyl rings of each molecule, while the shorter solid lines indicate the direction of the central ring.
molecules ðM1 ----M4 Þ in Figure 7.12. At 113 K, the molecules are nonplanar with the central ring rotated with respect to the two outer rings about the long axis of the molecule. Neighboring molecules along the a and b crystal axes have this twist in an opposite sense, so that there is a doubling of the respective distance along a and b, as shown in Figure 7.12. The environment of a pentacene replacing a p-terphenyl molecule will be different in each of the four positions. Calculations of the guest alignments in the lattice and its molecular structure accomplished by carrying out a potential energy minimization procedure for the four distinct site configurations [155] are presented in Figure 7.13. The total potential energy for the respective site of pentacene in the low-temperature phase was calculated using the Buckingham atom–atom potential function with Williams parameter set IV to optimize the intermolecular atomic distance [247]. In addition, the in-plane and out-of-plane force fields of pentacene [248, 249] were included in the minimization procedure of the site potential energy. For simplicity, the p-terphenyl molecules of the host cage were treated as rigid bodies. The intermolecular potential energy accounts for all ˚ which consequently atom–atom interactions within a cutoff distance up to 6 A, includes the 71 p-terphenyl considered as being nearly planar, whereas those in the O3 =O4 sites assume static out-of-plane distortions having lower symmetries. At liquid helium temperature, the absorption spectrum of pentacene at each site reveals an intense zero-phonon line associated with the electronic transition 1 Ag ! 1 B2u (Figure 7.14) and an accompanying phonon sideband (not shown in Figure 7.14). The latter appears as a mirror image in fluorescence and excitation and stems from pseudo-local phonons due to guest–host interactions [155]. The 1 Ag ! 1 B 2u pentacene transition in p-terphenyl is strongly b-axis polarized [250, 251].
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals
Figure 7.13 Calculated equilibrium configurations of pentacene at O1 =O2 ½ðaÞ; ðbÞ and O3 =O4 ½ðcÞ; ðdÞ in triclinic p-terphenyl and in O0 ½2ðeÞ in monoclinic p-terphenyl. The scale of the displacement vectors has been expanded considerably (15 times).
Figure 7.14 also shows vibronic transitions Oi þ vi assigned to the excited-state vibronic frequency of the stretching mode vi ¼ 267 cm1 of pentacene in the corresponding sites Oi . The p-terphenyl pentacene crystals used in the experiment described below were grown from the melt by the Bridgman technique using extensively zone-refined pterphenyl. The pentacene obtained from Aldrich was vacuum sublimed once before
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Figure 7.14 Low-temperature (4.2 K) absorption spectrum of pentacene associated with the pure electronic transition 1 Ag ! 1 B 1u at the various sites Oi ði ¼ 1; 2; 3; 4Þ. Note the narrow bands of the individual lines in comparison to the broad bands in the spectrum
of crystalline p-terphenyl host (Figure 7.2). This is due to the vanishing overlap of the wavefunctions of neighboring pentacene in different lattice sites. The transitions marked by parallelograms are taken in the transient grating experiment.
use. For fluorescence measurement, the crystal was cleaved along the ab plane with a thickness of 1–3 mm and mounted in a helium bath cryostat. 7.5.3 Techniques
The experimental study of transport phenomena within the assembly of guest molecules requires high guest concentrations, so that the average distance between the guests becomes sufficiently small and the dipole–dipole coupling sufficiently large to give rise to excitation energy transfer. While conventional fluorescence spectroscopy is confined to small optical densities because of reabsorption, special techniques such as transient grating methods are required to monitor the excitation dynamics in high-concentration doped crystals [246, 252, 253]. New developments have taken place in the 1990s. These were mainly due to the use of laser excitation yielding time-resolved spectra. These were especially of importance for the understanding of energy transfer phenomena. In a transient grating experiment, two time coincident and spatially overlapping excitation pulses are used to create an optical interference pattern inside the sample (Figure 7.15). Optical absorption creates a spatially varying optical interference pattern. This in turn produces a periodic variation in the sample index of refraction n that acts as a Bragg diffraction grating for a probe pulse. The time evolution of the transient grating is measured by monitoring the intensity of the Bragg-diffracted probe pulse (which scatters off the grating) as a function of delay time. In the absence of guest–guest dipolar
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals
(a)
(b) λp IB
x
x x
kA
kA
Θ
y
Θ
q z
Λ kB IA
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kB I
Figure 7.15 (a) Creation of a laser-induced dynamic interference pattern by two coherent plane waves A and B with intensities IA ¼ IB and wavelength l. (b) Shows the connection between the grating vector q and the wave vectors kA and kB .
coupling (i.e., at low guest concentrations), the lifetime of the excited singlet state determines the decay rate of the transient population grating. In sufficiently highly doped crystals, guest-to-guest energy transfer may destroy the grating pattern by dissipating the excitation due to the effective intramolecular and intermolecular interactions between resonant guest states and by trapping of the excitation by lower energy guest sites. In this case, the decay of the transient grating, as measured by its diffraction efficiency, is determined by both level depletion lifetime and transfer of excitation energy among the coupled guest molecules. The first transient grating experiments on mixed molecular crystals were performed on high-concentration p-terphenyl–pentacene crystals at room temperature [254]. The observed fast grating decay curves were interpreted to arise from diffusive excitation energy transfer by pentacene guests. In subsequent photon echo measurements of naphthalene:pentacene and p-terphenyl:pentacene crystals at helium temperature, the observation of concentration-dependent dephasing in the range 107 ----105 mol=mol was attributed to resonant or virtual energy transfer between the pentacene guest [254–256]. In a further study, transient grating experiments on pentacene guest in p-terphenyl crystals performed between 2 and 40 K show evidence of resonant as well as nonresonant excitation energy transfer occurring between pentacene guests in inequivalent lattice sites [251, 257]. The transient population gratings were created by exciting the electronic origin and first vibronic band off the electronic origin of pentacene in the O4 site of p-terphenyl using 4 ps laser pulses. The pulse energies of the excitation and probe pulses were hold at 0.5 mJ and 40 nJ, respectively. There are two reasons to select the O4 site for the study of excitation energy transfer: (i) the spectral overlap between its electronic origin and the phonon sidebands of the lower lying O1 ; O2 ; O3 sites is very small [177, 251, 257] and (ii) the fluorescence lifetime of pentacene tF ¼ 9:4 ns [177] is independent of temperature in the range 2–100 K, thus allowing for investigation of the temperature behavior of the energy transfer. The transient grating decay was measured as a function of the guest concentration cG ranging from 3 104 mol=mol to the highest accessible
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concentration of approximately 3 103 mol=mol. The transient grating was observed to decay faster than that produced by monitoring the pentacene guest, exhibiting a decay time of approximately half of the 1 S1 state lifetime, that is, tTG ¼ tF =2 ¼ 4:7 ns. Note that the decay of the transient grating is not a pure exponential. The effect of the guest concentration on the transient grating decay is illustrated in Figure 7.16. The decay curves recorded at 2 K are shown for crystals with various guest concentrations cG : (i) 4:9 104 mol=mol, (ii) 5:7 104 mol=mol, (iii) 1:2 103 mol=mol, and (iv) 2:1 103 mol=mol [251]. All the curves display a very fast initial drop in the diffraction efficiency followed by a much slower decay. Since the amplitudes of the slope of the fast component were observed to become larger with the increase in energy of the excitation pulses from 0.35 to 1 mJ [251, 257], the following theoretical analysis is limited to the dominant slow component of the transient grating decay curves that are independent of the excitation pulse energy up to 1 mJ. The slow component decays significantly faster with rising guest
Figure 7.16 Transient grating decay signals recorded (lighter curves) for excitation into the pure electronic origin at O4 ðT ¼ 2 K; L ¼ 20 mmÞ for various guest concentrations: (a) cG ¼ 4:9 104 mol=mol, (b) cG ¼ 5:7 104 mol=mol, (c) cG ¼ 1:2 103 mol=mol, and (d) cG ¼ 2:1 103 mol=mol. The heavy solid lines were calculated on the basis of the time
evolution of the excitation energy transfer using the following set of parameters: (a) Mi;i þ 1 ¼ i;N þ 1 þ i ¼ 4 108 s1 ; 1:35 102 cm1 and w i;N þ 1 þ i ¼ (b) Mi;i þ 1 ¼ 1:59 102 cm1 and w 6 108 s1 ; (c) Mi;i þ 1 ¼ 3:3 102 cm1 and N þ 1 þ i ¼ 9:5 108 s1 ; (d) Mi;i þ 1 ¼ w 5:7 102 cm1 and i;N þ 1 þ i ¼ 1:86 109 s1 . w
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals
concentration. This behavior indicates efficient excitation energy transfer between pentacene guests since the responsible dipole–dipole interactions are enhanced with decreasing distances among the pentacene molecules. Measurements of the transient grating dynamics at different grating constants L in the range 8.5–20 mm (by changing the angle q) show that the lifetime tTG is independent of L. This provides useful information about the nature of intermolecular processes and confines the range of energy transfer to a scale of distance much smaller than 10 mm. As a second example, we illustrate the temperature dependence of the grating decay at particularly high concentration cG ¼ 2:1 103 mol=mol (Figure 7.17). When the temperature increases from 2 to 36 K, the grating decay was found to become considerably slower. This temperature effect clearly excludes the hopping mechanism, as predicted for incoherent exciton transport. For concreteness, we assume that the excitation energy delocalized over resonant O4 sites is associated with temperature-inhibited dipole–dipole interaction among pentacene guest in these sites. The grating decay curves are rationalized to arise from fast energy transfer between resonantly coupled pentacene guests in O4 being in competition with slower trapping process by lower lying guest sites O3 ; O2 , and O1 .
Figure 7.17 Transient grating decay signals ðL ¼ 20 mmÞ recorded for excitation into the pure electronic origin of O4 for cG ¼ 2:1 103 mol=mol and various temperatures: (a) 36 K; (b) 24 K; (c) 10 K; and (d) 2 K.
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7.5.4 Nature of the Energy Transfer: Theory
In order to most simply explain these phenomena, we consider the response of an assembly of molecules presented in Figure 7.18 to a short optical pulse. The assembly consists of two different subsets of guest molecules occupying (energetically) nonequivalent sites in the host crystal (e.g., pentacene guest in the O4 and O3 sites of p-terphenyl). The guests occupying the highest lying lattice site O4 are initially excited by interaction with two resonantly tuned laser pulses, thus creating the transient grating. The destruction of phase coherence in the excited electronic state will originate from (i) intramolecular (radiative and nonradiative) transitions to the ground state ðS0 Þ (ii) by optical diffusion originating from resonant excitation energy transfer to the nearest-neighbor guest in the higher lying O4 sites and (iii) by nonresonant energy transfer to lower lying trapping sites O3 . The nonradiative coupling responsible for the resonant energy transfer is of the dipole–dipole type. The energy transfer mechanism between the guest molecules occupying O4 sites is of the cascade type, namely, by emission of photons by one guest and reabsorption of the photons by the nearest neighbor. The trapping process by the lower lying guest sites (traps) arises from phonon-assisted dipole–dipole coupling. In the scheme presented in Figure 7.18, only the trapping sites O3 are considered (the other lower lying trapping sites are neglected). In both the first and the second subset, the pentacene guests are separated from one another by the distance Ri;i þ 1 , which is dependent on the concentration cG (Table 7.9). Note that along the crystallographic axes the distances Ri;i þ 1 are calculated under the assumption that all pentacene guests are equally distributed among the four nonequivalent sites O1 ; O2 ; O3 ; O4 of the pterphenyl crystal. Note also that the distance Ri;i þ 1 is many times larger than the ˚ The ground states in both subsets are assumed length of the b-axis (i.e., b ¼ 5:613 A). to be degenerate and the energy difference in the excited singlet state between the O4 W23
W12 1 Ψ1s
2 Ψ1s
Ψgs
O4 site
W1,N+2
N+3 Ψ1s
W2,N+3
N+1 Ψ1s 2N+1 Ψ1s
∼ ν=17005.5±0.2cm-1
∼ ν=17064±2cm-1
N+2 Ψ1s Trap
... ...
3 Ψ1s
O3 site
O4
O3
O4
O3 site
O4 site
Figure 7.18 Model used to describe the population of guest molecules at O4 sites. The traps O3 are operative as killer sites. The deeper traps at O2 and O1 sites are omitted.
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals The critical distance R0 and the mean nearest-neighbor distance Ri;i þ 1 (both calculated for pentacene guest occupying O4 sites) along the three axes of the pseudo-monoclinic unit cell of p-terphenyl [252]. Table 7.9
˚ R0 ðT ¼ 4:2 KÞ=A ˚ R0 ðT ¼ 25 KÞ=A ˚ Ri;i þ 1 ðcG ¼ 4:9 104 mol=molÞ=A ˚ Ri;i þ 1 ðcG ¼ 5:7 104 mol=molÞ=A ˚ Ri;i þ 1 ðcG ¼ 1:2 103 mol=molÞ=A ˚ Ri;i þ 1 ðcG ¼ 2:1 103 mol=molÞ=A ˚ Ri;i þ 1 ðcG ¼ 2:7 103 mol=molÞ=A
a0
b0
c
71 66 161 153 120 99 91
126 117 112 106 83 69 63
118 110 136 130 101 84 77
and O3 sites is hV. For simplicity, we assume that each guest in the O4 is coupled to a single trap in the O3 site. The Hamiltonian describing the system of N oriented guests in a host crystal is given by H ¼ H0 þ V ¼ Hðr; qÞ þ Hrad þ Hint ;
ð7:48Þ
where Hðr; qÞ ¼
X i
Hi ðri ; qi Þ þ
1X Vij 2 i;j
ð7:49Þ
is the Hamiltonian of the guest molecules in sites i and Vij is the dipole–dipole interaction HDD between molecules in sites i and j. Hrad in Equation 7.48 is the Hamiltonian of the radiation field (which is switched on at t ¼ 0 to create the transient population gratings) and Hint represents the radiation–matter interaction, defined by Equation 6.10. If we ignore for a moment the interaction Vij , the eigenfunction of Hi ðri ; qi Þ, which describes the ground state of system of N guest molecules, is Yg;r ¼
N Y i
Wign ðri ; qi Þ:
ð7:50Þ
Here, Wign ðri ; qi Þ ¼ jig ðri ; qi Þxign ðqi Þ is the ground-state BO wavefunction of a guest molecule at site i.ri ; qi are, respectively, the electronic and vibrational normal coordinates of the guest molecule at site i, and n stands collectively for the set of vibrational occupation numbers. The energy associated with Equation 7.50 is Eg ¼ Neg , where eg represents the ground-state (electronic plus vibrational) energy of an isolated guest molecule. The wavefunction of the excited state corresponding to the excitation of the molecule in position i in the kth electronic state and rest of the molecules in the ground electronic state is Y Yikmi ¼ Wikm ðri ; qi Þ Wjgn ðrj ; qj Þ; k ¼ 1; 2; . . . ð7:51Þ j6¼i
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with the energy Ek ¼ ðN1Þeg þ ek, where ek is the energy of the isolated guest in the kth electronic state and Wikm ¼ jik ðri ; qi Þxikm ðqi Þ. We have written explicitly Yik;m with the superscript i to emphasize that it is assigned to the molecule (pentacene) at site i. The N different jik electronic eigenfunctions of H0 are N-fold degenerate. The state Wikm is coupled to the manifold of vibronic levels of the ground state Wign . As a consequence, Wikm can either decay radiatively or nonradiatively through interactions with the radiation field or alternatively by internal conversion to the ground state. Both of these possibilities involve population relaxation and are called lifetime or T1 processes. At high guest concentrations, when electric dipole–dipole interaction Vij between the guests becomes efficient, resonant as well as nonresonant guest-to-guest transfer occurs that predominantly influences the decay of the initially excited guest state Wikm . In the case of resonant energy transfer between neighboring guest j molecules being in the first excited state k ¼ 1, Wi1m and W1m0 , the relevant matrix element for energy transfer is given (see Appendix H) by Mij ¼
1 i i j j i j j i 3 j1 mi jg tij jg mj j1 x1m xgn x1m0 xgn0 : eRij
ð7:52Þ
ij Þ and mi ¼ mj ¼ m is the electric dipole of the guest Here, tij ¼ 13cos2 ðm; R molecules and Rij is the unit vector along the Rij distance. The energy transfer rate may easily be evaluated in the form (see Appendix H) ð 2p wij ¼ 2 J 2 dvFS ðvVS ÞFA ðvVA Þ; ð7:53Þ h DD where J is the matrix element of the dipole–dipole interaction Hint in Equation 7.52 and FS ðvVS Þ and FA ðvVA Þ are the spectral functions for emission and absorption. In more conventional terminology, the F€ orster energy transfer rate (7.53) is generally written in terms of a critical transfer distance R0 1 R0 6 wij ¼ ; ð7:54Þ tF Rij
where R0 and Rij are the critical interaction distance and the distance between the interacting molecules i and j, respectively. For the special case of pentacene guests in the O4 site of p-terphenyl, the values of R0 were determined from the overlap between the absorption and the fluorescence spectrum at the O4 site at 4.2 and 25 K (Table 7.9). The table also lists the mean distance between two neighboring pentacene guests in the O4 site for several pentacene concentrations cG along the crystal axes of the pseudo-monoclinic unit cell of p-terphenyl. Since they are smaller than R0 along the baxis, the nearest-neighbor electric dipole–dipole interaction is strongest along this axis (note that along the b-axis the crystal is most densely packed). This means that the transfer rate along this b-axis will dominate the fluorescence quenching, whereas the energy transfer along the a-axis and c-axis will be neglected. Another effect indicated in Table 7.9 is that R0 decreases as the temperature increases from 4.2 to 25 K. This effect stems from the fact that the critical distance R0 depends considerably on the spectral overlap between fluorescence and absorption origins VS and VA . Since in
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals
the investigated temperature range between 2 and 36 K a shift between the pure electronic transitions in fluorescence and absorption exists [257, 258], the spectral overlap integral is reduced that decreases R0 . As a slightly more complicated process, we next consider the trapping of energy between the O4 sites and the lower lying guest site O3 (trapping by the other, even lower lying sites, labeled O1 and O2 , is neglected for simplicity). The rate of this nonresonant energy transfer is given by (see Appendix F) ð p Jðf gÞ 2 ij ¼ dvFS ðvV1 ÞFðvV2 vk Þ; w ð7:55Þ hvk hvk where the energy of the emitted phonon hvk is assumed to be equal to the trap depth of O3 , Ei EN þ 1 þ i ¼ hðV1 V2 Þ 60 cm1 . 7.5.5 Time Evolution of the Guest Excitations
The time evolution of an initially prepared state by the crossed excitation beams is Yikmi ðr; q; tÞ ¼ exp ðiHt=hÞYikmi ðr; q; t ¼ 0Þ;
ð7:56Þ
where exp ðiHt=hÞ ¼
1 2pi
1 ð
exp ðiEt=hÞGðEÞdE;
ð7:57Þ
1
with GðEÞ ¼ 1=ðEHÞ. For further consideration, it is convenient to separate the space comprising the states of guests using the projection operator P, defined by X Yi ihYi : ð7:58Þ P¼ 1mi 1mi i
1 The operator P will project on states associated with the first singlet excited state S i of the guest in the highest site O4 . Note that this model space is completely 1 degenerate. The complementary space Q consists of the remaining states ðk 6¼ 1; gÞ of pentacene including those of the guest in the trapping site O3 . The transform of the time evolution is clearly (analogous to that of Equation 2.10) PGðEÞP ¼ ½EPH0 PPRðEÞP1 P;
ð7:59Þ
RðEÞ ¼ V þ VQðEQHQÞ1 QV
ð7:60Þ
where
is the level shift operator introduced in Chapter 2. The operator contained in Equation 7.59 defines the effective Hamiltonian Heff ¼ PH0 P þ PRðEÞP;
ð7:61Þ
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which will be now used to calculate the time evolution operator exp ðiHeff t= hÞ for the decay of the transient grating signal due to intramolecular excited-state depopulation and excitation transfer along the assembly of guest molecules. For this reason, it is convenient to rewrite Equation 7.60 by expanding the right-hand side to give RðEÞ ¼ V þ VQðEQH0 QÞ1 QV þ ðhigher order termsÞ:
ð7:62Þ
The first term on the right-hand side of Equation 7.62 describes (within the subset of space) the transition due to the intermolecular interaction Vij alone. The physical interpretation of the second term may be regarded in the following manner. Recalling that V is the full (intra- and intermolecular) interaction, the diagonal transition matrix element of RðEÞ may evidently be written in the form 2 X X j hYi1mi jRðEÞjYi1mi i ¼ hYi1mi jV jY kmj i k¼1;g
PP
1 j
EEkmj
j
2 X X j j ip Yi1mi jV jYkmj d EEkmj k¼1;g
j
¼ DðEÞiCðEÞ=2:
ð7:63Þ
There are now two important contributions to the width C. According to the physical situation discussed in the previous section, one may insert on the right-hand side of Equation 7.63 two different intermediate states and the associated interactions. If one takes, for example, the ground-state wavefunction ðk ¼ g; j ¼ iÞ and considers the coupling of the molecule to the radiation field Hint and to the ground state Yig;n due to nonadiabatic interaction, the width C is fully determined by the lifetime of the 1 S1 i state tF ; C ¼ ht1 F (compare to Equation 6.29). Regarding V to be determined by the phonon-assisted energy transfer and taking k ¼ 1 and j ¼ N þ 1 þ i, the contribution to the width C is given by the energy transfer rate ij , where w ij is given by Equation 7.55. The level shift to the traps, for example, C ¼ hw DðEÞ, which is defined as a principal value integral (see Equations 213–215), is small and can be neglected subsequently. Let us now return to the scheme of Figure 7.18. Denoting as above the first excited states of the guest molecules in the O4 site by Yi1mi , the time evolution of the superposition of these states after pulse excitation is presented by the compound state YðtÞ ¼
N X i¼1
xi ðtÞYi1mi :
The probability amplitudes here are xi ðtÞ ¼ hYi1mi jexp ðiHeff t=hÞjY11m1 i ;
ð7:64Þ
i ¼ 1; 2; . . . ; N
ð7:65Þ
and the quantities jxi ðtÞj2 present the probability density of finding the excitation in the ith highest lying site O4 . This problem can thus be treated in a brute-force manner by constructing a matrix equation of high order as shown below. Indeed by applying the Wigner–Weisskopf approximation, Equations 7.64 and 7.65 are equivalent to the following set of coupled differential equation for the amplitude xi ðtÞ
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals
1 E1 iC1 M 0 0 1 2 2 1 x1 ðtÞ x1 ðtÞ M1 2 E2 iC2 M2 3 0 2 x2 ðtÞ x2 ðtÞ d 1 x3 ðtÞ ih x3 ðtÞ ¼ E3 iC3 M3 4 0 M2 3 ; . dt .. 2 .. . ... 0 xN ðtÞ xN ðtÞ . . . M N1;N 1 0 0 M E iCN N1;N N 2 ð7:66Þ
or in abbreviated form ih
d xðtÞ ¼ Heff xðtÞ: dt
ð7:67Þ
According to the discussion above E1 ¼ E2 ¼ ¼ EN ð1 S1 Þ:
ð7:68Þ
The decay rate Ci =h is given by Ci ¼ h
1 i;N þ 1 þ i ; þw tF
i ¼ 1; 2; . . . ; N:
ð7:69Þ
The off-diagonal matrix elements Mij in Equation 7.66 are responsible for the resonant energy transfer rate. The latter are nonzero for nearest-neighbors sites j ¼ i 1 and otherwise zero, that is, Mij ¼ Mðdi;j1 þ di;j þ 1 Þ. This follows from the fact that the single-step energy transfer rate decreases inversely with the sixth power of the distance between the interacting guests i and j (Equation 7.54). In a further calculation where substitutional disorder is taken into account, this assumption will i;N þ 1 þ i (see Equation 7.53) that characterize be dropped. The energy transfer rates w the single-step trapping process are treated as adjustable parameters. Their values are obtained from the best fit of Equation 7.66 to the transient grating data. The initial condition at t ¼ 0 for the just formed grating is 1 0 xð0Þ ¼ .. : . 0 Equation 7.66 is solved by diagonalization of Heff via complex orthogonal transformation using Mathematica version 2.2.1. Before continuing with our description of energy transfer, it is perhaps worth presenting a closed explicit formal solution of Equation 7.66. This solution can be provided by diagonalization of Heff via an orthogonal transformation D (see Appendix G). The time evolution operator in
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P Equation 7.65 is then Uðt; 0Þ ¼ expðiHeff t= hÞ ¼ jiexp½iEj t= hCj t=2 hhj and j P hCj t=2 hhjY11m1 i.3) the solution of Equation 7.65, xi ðtÞ ¼ j hYi1mi jiexp½iEj t= The integration of the differential Equation 7.66 leads to a solution (Figure 7.19) [259] that makes the energy transport a direct experimental observable. For the presentation of the probability density jxi ðtÞj2 along the time axis, we would need space of several meters. Therefore, in Figure 7.19a only every fifth step in the sequence of the squared transient grating amplitude jxi ðtÞj2 is presented and in Figure 7.19b we show a part of the first 15 members of jxi ðtÞj2 in greater detail. The calculations of xi ðtÞ were performed for N ¼ 79. The off-diagonal matrix element occurring in the matrix (Equation 7.66) and the single-step nonresonant energy transfer rate used in this calculation are Mi;i þ 1 ¼ 1:35 102 cm1 and i;N þ 1 þ i ¼ 4 108 s1 , respectively. These values give the best fit to the transient w grating decay (curve (a) in Figure 7.16) for the lowest concentration cG ¼ 4:9 104 mol=mol. Figure 7.19 demonstrates directly how the resonant excitation travels from O4 to the O4 site, being simultaneously depleted due to trapping by O3 sites. The latter that is related to the width Ci , Equation 7.69, is mainly responsible for the decay of excited state (see Equation 7.64). The effect of guest concentration on the excitation energy transfer in this system under study may be easily seen in Figure 7.20, where the same calculation has been performed for a concentration cG ¼ 2:1 103 mol=mol (compare curve (d) in Figure 7.16) and an off-diagonal matrix element of Mi;i þ 1 ¼ 5:7 102 cm1 . This leads to stronger interactions between resonantly coupled pentacene molecules in the O4 sites and results in a faster energy transfer along the chain of these molecules. Both calculations reveal an oscillatory behavior (interferences) in the transient grating contributions jxi ðtÞj2 . The rather small oscillation frequency ð 109 s1 Þ becomes larger when the resonant energy transfer rate wi;i þ 1 and thereby the off-diagonal matrix elements Mi;i þ 1 increase. Both Figures 7.19 and 7.20 give energy transport parameters directly, for example, the velocities of the energy transport. For the low guest ˚ concentration, the average value of the transfer velocity is about 540 A=ns, while that ˚ for the high guest concentration amounts to 1400 A=ns. The less the off-diagonal matrix elements Mi;i þ 1 , the lower the mean energy transfer velocity, and hence the longer it takes to go a given distance. In the course of time, the energy transfer evolves according to the following rules: a. The excitation energy migrates over several O4 sites before it will decay by transfer to the traps. The parameters that characterize the excitation energy transfer are related to (i) the off-diagonal matrix elements Mi;i þ 1 , (ii) the nonresonant transfer rate, as well as (iii) to intramolecular transitions described by the lifetime tF . b. The energy transfer between nearest-neighbor pentacene guests occurs within the fluorescence lifetime tF .
3) A useful reference of this subject is the work of H. F. Baker On a Simple Transitive Continuous Group, Proc. London Math. Soc., 1902, pp. 91–129.
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals
Figure 7.19 (a) The time-dependent evolution of the excited states of a system of dipole–dipole coupled pentacene guests occupying resonant O4 sites in p-terphenyl crystal. The energy transfer is shown for the 1st, 5th, 10th (first row), 15th, 20th, 25th (second row), 30th, 35th, 40th (third row), 45th, 50th, 55th (fourth row),
and 60th, 65th, 70th (fifth row) steps. The calculations have been carried out by taking i;N þ 1 þ i to give the best fit values for Mi;i þ 1 and w to the transient grating decay curve (a) in Figure 7.16. (b) Portion of (a) of the first 15 such coupled pentacene guests in greater detail.
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Figure 7.19 (Continued)
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals
Figure 7.20 Same as Figure 7.19a but for a stronger interaction between resonantly coupled i;N þ 1 þ i ¼ 1:86 109 s1 have pentacene guests. The values of Mi;i þ 1 ¼ 5:7 102 cm1 and w been chosen to obtain the best fit to the transient grating decay curve (d) in Figure 7.16.
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c. The excitation energy may be transferred many times through the O4 sites before it becomes trapped by the O3 sites. This takes place when the electric dipole–dipole interaction between neighboring O4 sites will be sufficiently strong (i.e., if Mi;i þ 1 is of the order 102 cm1 or larger). For guest concentrations between 3 103 and 5 104 mol=mol, the mean nearest-neighbor distance between pentacene guest in O4 sites along the crystallo˚ (Table 7.9). From this and the velocities graphic b-axis ranges between 60 and 100 A estimated above, it follows that d. Resonant and nonresonant excitation energy transfers lead to efficient depletion of the excitation population along the b-axis within 1 mm, which is 5% of the grating constant L. This becomes apparent from the contributions jxi ðtÞj2 , which represent a descent sequence of the excited-state energy migration (Figures 7.19 and 7.20). An interesting situation arises if the chain of dipole–dipole interacting guest molecules along which the resonant energy transfer takes place is interrupted by removing a guest. Figure 7.21 illustrates such a case, where the sixth site is unoccupied by a guest and where the excitation energy migrates from the fifth site to the seventh site along the array. Correspondingly, the calculation has been performed by taking Mi;i þ 1 and Ci as used in the calculation presented in Figure 7.20, with the exception that now M5;6 ¼ M6;5 ¼ 0 and C6 ¼ 0. Instead of this, the next nearest-neighbor off-diagonal matrix elements M5;7 ¼ M7;5 are nonzero and 23 ¼ 8 times smaller than the remaining nearest-neighbor element Mi;i þ 1 . Figure 7.21 clearly shows that a deviation from a perfect substitutional order of pentacene guests in the crystal will lead to additional oscillations or interferences in the excitation transfer. This effect may be caused by back transfer from the array discontinuity. Apart from the fact that the excitation transfer falls off rapidly after the discontinuity in the array, the excited-state probability distribution jxi ðtÞj2 differs only slightly from that of the unperturbed array presented in Figure 7.20. 7.5.6 The Decay of the Transient Grating Signal
The excitation probability densities jxi ðtÞj2 (which correspond to the excitation density) generated by tuning the laser pulses to the absorption peak at the electronic origin m ¼ ð01 ; 02 ; . . . ; 0N Þ (Figure 7.14) or the first vibronic transition of pentacene at the O4 site originating from the level m ¼ ð01 ; 02 ; . . . 1; . . . ; 0N Þ are utilized to calculate the grating decay presented in Figures 7.19 and 7.20. The decay of the transient grating signal [246, 253] or the temporal evolution diffraction efficiency SðtÞ is proportional to the square of the numberdensity of the excited states YðtÞ at the P 2 2 . Here, A is a constant that contains all grating peaks, that is, SðtÞ ¼ A N i¼1 jxi ðtÞj of the time-independent parameters such as beam geometry, the extinction of the absorption peak, and the number of density of absorbing molecules. Figure 7.16 shows a fit (heavy solid curves) of the calculated signal SðtÞ to the experimental data (lighter curves) obtained for various guest concentrations cG . As cG and consequently
7.5 Theory and Experiment of Singlet Excitation Energy Transfer in Mixed Molecular Crystals
Figure 7.21 The time-dependent evolution of the excited states of a system of N ¼ 79 dipole–dipole coupled pentacene guests occupying O4 sites in a p-terphenyl host crystal, where the sixth site remain unoccupied. The
i;N þ 1 þ i are the same as values of Mi;i þ 1 and w for Figure 7.19 with the exception that now M5;6 ¼ M6;5 ¼ C6 ¼ 0 and M5;7 ¼ M7;5 are taken (see text.)
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the excitation energy transfer to the O4 sites and the traps O3 increases, the signal SðtÞ will decay faster. The off-diagonal elements Mi;i þ 1 used in these calculations were estimated from the overlap integral of Equation 7.52 and from the resonant transfer rate, which in turn was calculated using the values of R0 and Ri;i þ 1 listed in Table 7.9. i;N1 þ i are obtained from the fit to the experimental The nonresonant transfer rates w curves. Generally, the decay is not a pure exponential and depends on the complex eigenvalues of the matrix (see Equation 7.66). Combining these results with the feature discussed above, we conclude that transient population gratings with a grating constant L varied between 8.5 and 20 mm cannot decay by filling in the nulls and depleting the peaks of the grating. Instead, the excited 1 S1 state population density of pentacene guest at O4 sites is responsible for the observed fast grating decays in the concentration range between 3 104 and 3 103 mol=mol. This result explains the observed insensitivity of the grating decay dynamics to the grating constant L on the mm length scale. Since in the experiment discussed above, the transient gratings could not be utilized as direct probes for energy transfer on the distance scale of the grating constant, the same information could, in principle, be obtained from pump and probe experiments. However, it must be pointed out that a transient grating experiment is inherently more sensitive than the pump and probe experiment, since the diffracted probe beam is detected against a dark background and the excitation power densities are lower by several orders of magnitude compared to that of a pump and probe experiment. In the situation displayed in Figure 7.17, the guest concentration cG is kept constant, while the temperature is increased from 2 to 36 K. As already discussed above, the diffraction efficiency decays slower with rising temperature. This observed phenomenon appears to follow from simple and general arguments (see Section 6.5 for detail information). Pentacene in p-terphenyl exhibits a temperature-dependent increase of the line width (full width at half maximum), which is governed by the equation Dnhom ¼
1 1 1 ¼ þ ; pT2 2pT1 pT2
where T2 is the dephasing time, T1 is the level depletion lifetime, and T2 the pure dephasing time associated with phase destructive events (e.g., by pseudo-local phonons [155]). Measurements by photon echo have shown [258] that at temperatures below 2 K the pure dephasing processes are negligibly small ðT2 ¼ 2T1 Þ. For T > 2 K, the dephasing of the electronic origin by a T1 -type scattering to local phonons and intermolecular interactions varies with temperature as DE T2 ðTÞ ¼ T2 ð1Þexp ; kT
where DE is an activation energy and it is probably safe to consider the values for T2 ð1Þ between 2 and 5 ps (depending on the concentration cG ) [258]. This asserts that at T ¼ 10 K and values of DE lying somewhere in the range of phonons with energies of 30 cm1 , T2 reduces to about 200 ps. For the line shift dT , a similar expression holds, but with a different meaning of the preexponential factor. The description of the
7.6 Electronic Predissociation of the 2B2 State of H2O þ
excitation motion outlined above assumes that the spectral overlap of sensitizer and activator is constant. This is true if the temperature is kept constant. However, as described above, a temperature increase affects the spectral overlap mainly due to the redshift in fluorescence and absorption lines [257]. This leads to a decrease of the spectral overlap and thus to an energy transfer rate that varies with temperature.
7.6 Electronic Predissociation of the 2B2 State of H2O þ 7.6.1 Evaluation of the Nonadiabatic Coupling Factor
In this section, we limit our attention to a special case of the results obtained in ~ 2A0 states of H2 O þ ~ 2A0 and A Section 1.4 for the conical intersection connecting the B 2 to consider the vibronically induced predissociation of the B2 state. According to the interpretation in [260–262] and the calculations of the nonadiabatic couplings in Section 1.4, after preparing the molecule H2 O þ in the metastable state 2B2 by excitation with photon energy hn in the ranges between 18.0 and 20.2 eV, the latter plays an important role in producing OH þ ions. This nonradiative conical intersection seems to be at least competitive with the electronic predissociation of the 2B2 state of H2 O þ by two repulsive states 4A00 and 2A00 [262] for production of, respectively, H þ and OH þ . ~ 2A =2A 0 Þ ~ 1 A1 Þ þ hn ! H2 O þ ðB~ 2B2 = 2A 0 Þ ! H2 O þ ðA H2 OðX 1 ! OH þ ð3 S Þ þ H ! H þ þ OHð2 PÞ;
The nonradiative transition for the above process will be examined here. The required probability is then w /¼
2p X X 2 Cif ; h i f
ð7:70aÞ
where Cif is the probability amplitude ~ jq=qRjBiqx ~ i =qRJ 1=2 Þ: Cif ¼ ðxf hA
ð7:70bÞ
~ jq=qRjBi ~ is the nonadiabatic electronic coupling matrix element and R is the gR ¼ hA reaction or dissociation coordinate, which will be defined below. The braket ( ) appearing in Equation 7.70b denotes integration over nuclear coordinates. Hence, determination of the matrix element (7.70) requires the evaluation of a multidimensional FC-type factor as well as the electronic matrix element hj ji. The Jacobian J in (7.70) insures that initial- and final-state wavefunctions are normalized with respect to the same volume element (in a sense to be made more precise below). The integrand in Equation 7.70 is a sharply peaked function over the nuclear coordinates, so that the integration may be confined to a restricted region of the
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nuclear coordinates around the apex of the conical intersection. This becomes particularly clear later when we estimate the electronic matrix element gR . Evaluation of gR is not trivial, however, it can be obtained from the nonradiative coupling factors derived in Section 1.4 (see formulas (1.68)). Since the dissociation process is represented as Y1 XY2 ! Y1 þ XY2 , a suitable coordinate system is given by the body-fixed (BF) reference frame [263–266] as shown in Figure 7.22, the Z-axis of which lies along the vector R from atom Y1 to the center of mass (c.m.) of the diatomic molecule XY2 . The angle c is the polar angle of the diatomic bond axis XY2 (the length of which is rd ) in the body-fixed system. The coordinates ðR; c; rd Þ, which we use below, are denoted as the Jacobi coordinates. In the same Figure 7.22, the angle w between the body-fixed Z-axis and the space-fixed (SF) x-axis describes the rotation of the entire system about the center of mass (C.M.). Since we are only interested in the motion in the xy plane, the azimuthal angles of rd in the body-fixed system are assumed to be zero. The coordinates ðR; c; rd Þ, which are suitable for describing the receding motion of the molecule on the potential surface, are now used to evaluate the matrix element (7.70). For this reason, we need a transformation between the normal coordinates of the triatomic molecule H2 O þ in its bound state and the Jacobi 3
mx
(a)
r2
α my
y
αeq
req
2
r1 my
1 x
(b) 3 γ
(c.m.) rd (C.M.)
y 2
R φ 1
x Figure 7.22 (a) Internal coordinates of a bent triatomic molecule. (b) Space-fixed and body-fixed coordinate systems for a 123 triatomic molecule.
7.6 Electronic Predissociation of the 2B2 State of H2O þ
mx
S1 αeq
re my
S1
S1
my
2my m x S2
S2 αeq S2
S2
my
my
2my sin αeq m x S3
S3 αeq my
S1
S1
my
Figure 7.23 Symmetry coordinates of a bent symmetric triatomic molecule. After Ref. [75].
coordinates ðR; c; rd Þ. Since the normal coordinates are related to the symmetry coordinates linearly (Figure 7.23), we start with the presentation of the latter in terms of ðR; c; rd Þ. The result is [267] 1 S1 ¼ ½R sin w þ ðmXY =mY Þrd sin ðw þ cÞ þ re sin aeq ; 2 S2 ¼
1 ½R cos wð1 þ mXY =mX Þrd cos ðw þ cÞ þ re cos aeq =p; 2p
1 S3 ¼ cos aeq ½R cos w þ ðmXY =mY Þ rd cosðw þ cÞ; 2
ð7:71Þ
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where p ¼ 1 þ 2mY =mX , with mX and mY being the mass of atom XðX ¼ OÞ and atom YðY ¼ HÞ, respectively. re and aeq are the bond length and the half valence angle in the equilibrium geometry of the triatomic YXY in the initial bound state. mXY ¼ mX mY =ðmX þ mY Þ is the reduced mass of the diatomic fragment XY. The angle w describes the orientation of the molecular framework YXY during the ~ It is given by [267] ~ , A. transition B w ¼ wðR; rd ; cÞ ¼ arctan
Rp tan aeq þ ðmXY =mY Þrd p tan aeq cos c þ ð1 þ mXY =mX Þrd sin c : Rð1 þ mXY =mX Þrd cos c þ ðmXY =mY Þrd p tan aeq sinc
ð7:72Þ
Over a restricted range of R, the transformation (7.71) is quasilinear in respect to R and rd but nonlinear in respect to c and w. With the aid of the nonadiabatic coupling terms along the internal coordinates a and r ¼ 12 ðR1 R2 Þ, the relevant nonadiabatic coupling between the potential surfaces of states 2B2 and 2A1 calculated along the reaction coordinate R can now be expressed as ~ jq=qRjBi ~ ¼ gR ðR; rd ; cÞ ¼ ga hA
qa qr þ gr : qR qR
ð7:73Þ
In order to calculate gR , we need the dependence of a on R and r on R. These relations can be obtained by recalling (see Ref. [268], p. 149, eq. (II. 122)) that the symmetry lowering coordinate r can be expressed in terms of the symmetry coordinate S3 , r ¼ 2tS3 ;
ð7:74Þ
where t ¼ 1 þ 2ðmY =mX Þsin2 aeq . Similarly, for the change of the valence angle a around its value ac at the conical intersection between states 2B2 and 2A1 (when r ¼ 0; ac ¼ 2aeq ¼ 71:6 ), we have (Figure 7.23) aac ¼ 2ðpS2 sin aeq S1 cos aeq Þ=re :
ð7:75Þ
Substituting Equation 1.68 in Equation 7.73 and using the relations (7.74) and (7.75), we write Equation 7.73 in the form gR ðR; rd ; cÞ ¼
1 tFa Fr =re 2 ðFr tS3 Þ2 þ ðFa =re Þ2 ðpS2 sin aeq S2 cos aeq Þ2 0 1 3 2 qS3 @ qS2 qS1 A 5 4 ðpS2 sin aeq S1 cos aeq Þ p sin aeq cos aeq S3 ; qR qR qR ð7:76Þ
where according to (7.71) and (7.72) qS1 1 qw ¼ sin w þ ½R cos w þ ðmXY =mY Þrd cosðw þ cÞ ; qR 2 qR
ð7:77Þ
7.6 Electronic Predissociation of the 2B2 State of H2O þ
qS2 1 qw ¼ cos w þ ½R sin w þ ð1 þ mXY =mX Þrd sin ðw þ cÞ ; qR 2p qR
ð7:78Þ
qS3 1 qw : ¼ cos aeq cos w½R sin w þ ðmXY =mY Þrd sinðw þ cÞ qR qR 2
ð7:79Þ
and qw qR ¼
sin wp tan aeq cos w : R cos wð1 þ mXY =mX Þrd cosðw þ cÞ þ p tan aeq ½R sin w þ ðmXY =mY Þrd sinðw þ cÞ ð7:80Þ
Figure 7.24 shows the nonadiabtic electronic matrix element gR plotted as a ˚ and fixed values of mY ¼ function of R and c for constant rd ¼ 1:15 A 1836:151 amu and mX ¼ 16mY . Figure 7.24 clearly demonstrates that the coupling factor gR has considerable variation with R and c, which may greatly affect the critical relaxation rate by orders of magnitude. One of the interesting results of this analysis is the extent to which the coupling factor gR resembles a generalized function. Viewing the c-axis, gR resembles a function d0 ðccc Þ, where d0 is the derivative of the delta Dirac distribution centered at cc ¼ 105:5 . Along the R-axis, we have a function ˚ The coupling gR is found to be positive for resembling dðRRc Þ, where Rc ¼ 1:14 A.
c smaller than cc ¼ 115:5 and negative for c larger than cc . A dynamic study by means of classical trajectory calculations [70] shows that the rate constant describing
Figure 7.24 Nonadiabatic electronic coupling matrix element gR as a function of R and c; (a) view against the c-axis. (b) A second view down the c-axis. The diatomic internuclear OH distance rd is
kept fixed at a value of 1.15 A.
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the internal conversion from the upper cone to the lower adiabatic surface is of the order of 1014 s1 . Note the difference of this reasoning to that employed at the end of Section 7.2. There, however, we concluded that the matrix element responsible for the nonradiative transition is determined in higher order by motion of the nuclei and by abrupt change in the spin configuration. Here, we conclude that the energies of the adiabatic states 2 B2 and 2 A1 are very close and the coupling matrix element gR ðR; rd ; cÞ between these states evolves the derivatives of the electronic wavefunction with respect to the nuclear coordinates (Equations 1.15 and 1.16). This term is expected to be large in the vicinity of the conical intersection (in the cusp intersection), where the wavefunction changes rapidly. If, for example, the bending frequency v2 of H2 O þ is taken as 1600 cm1 , it is seen that the m2 ¼ 1 level will lie 2400 cm1 above the 2 B2 minimum, which is very close to the energy of the cups of intersection ( 1300 cm1 ). Perturbations due to the E2 E1 coupling between the upper cone and the lower adiabatic surface may be very significant for levels in that energy region (see Figure 1.1) and lead to a ultrafast intramolecular relaxation with a lifetime of 1014 s. As far as the photodecomposition of H2 O þ is concerned, the nonadiabatic passing through the conical intersection between the ~ states of H2 O þ plays an important role in producing the surprisingly large ~ and A B amount of H þ . Finally we note that the rotation angle w is a slowly varying function of R and depends parametrically on c [267]. The change of the diatomic distance rd has little or no effect on the strength of gR and can be safely assumed rigid allowing rd to be replaced by a suitable equilibrium value r0 . When this is substituted into Equation 7.76, gR is then set to be gR ðR; r0 ; cÞ. The stretching coordinate rd becomes important in calculating the vibrational frequencies of the diatom and must be fully incorporated into the nuclear functions of both electronic states. 7.6.2 The Basis State Functions
We now turn to the vibrational wavefunctions appearing in the matrix element (7.70a). 7.6.2.1 The Initial-State Wavefunction xi To evaluate the integral (7.70a), it is necessary to obtain expressions for the nuclear wavefunctions xi and xf . The upper adiabatic state can often be described in the harmonic approximation as a product of three oscillator functions xi ¼ xi;m1 m2 m3 ðqm ðR; rd ; cÞÞ ¼ xi;m1 ðq1 Þxi;m2 ðq2 Þxi;m3 ðq3 Þ:
ð7:80aÞ
The normal coordinates q1 and q2 for the symmetric stretching and bending vibrations are then linear combinations of the symmetry coordinates S1 and S2 used above for calculating the electronic coupling factor gR and q3 ¼ c33 S3 is the asymmetric stretching coordinate [70]
7.6 Electronic Predissociation of the 2B2 State of H2O þ
q1 ¼ c11 S1 þ c12 S2 ; q2 ¼ c21 S1 þ c22 S2 ; q3 ¼ c33 S3 :
ð7:81Þ
After utilizing (7.71), we eliminate ðq1 ; q2 ; q3 Þ in favor of ðR; rd ; cÞ to give xi ¼ xi;m1 ;m2 ;m3 ðfqm ðR; rd ; cÞgÞ:
ð7:80bÞ
The transformation coefficients of Equation 7.81 are determined by solving the usual secular equation in terms of the masses, force constants, and frequencies [267]. The numerical values of the coefficients cij for the ground state of the neutral molecule are [70] c11 ¼ 49:343 aum1=2 ; c21 ¼ 35:772 aum1=2 ;
c12 ¼ 37:310 aum1=2 ; c22 ¼ 52:337 aum1=2 ;
c33 ¼ 62:922 aum1=2 :
Figure 7.23 provides a graphical representation of the results expressed by Equation 7.81. The Jacobian for that transformation is given by [267] J¼
Dðq1 q2 q3 Þ Rrd ¼C ; 2pD cos aeq DðR; rd ; cÞ
where C ¼ ðc11 c22 c12 c21 Þc33 and D ¼ R cos wð1 þ mXY =mX Þrd cosðw þ cÞ þ p tan aeq ½R sin w þ ðmXY =mY Þrd sin ðw þ cÞ: 7.6.2.2 The Final Vibrational Wavefunction xf : The Closed Coupled Equations One of the most difficult aspects in treating polyatomic predissociation is the proper description of the xf wavefunction. The complication arises because the wavefunctions for the translational motion are obtained as a solution of coupled differential equations. In deriving this, we may proceed as follows: When the bent triatomic molecule is initially nonrotating (J ¼ 0) and the diatom is assumed to be bound for all energies considered, the nuclear Hamiltonian for motion of the nonlinear triatomic molecule Y1 XY2 on the final state of H2 O þ can be written as [263–266] 2 h2 q L2 HN ¼ Hd þ VðR; r0 ; cÞ; ð7:82Þ R þ 2m1 R qR2 2m1 R2
where L is the angular momentum operator for the relative motion of atom Y1 about the diatomic center of mass (with zero projection on the space-fixed x-axis) and 1 1 is the interfragment reduced mass. That is, m1 1 ¼ mY1 þ ðmX þ mY2 Þ h2 q q L2 ¼ sin c : ð7:83Þ sin c qc qc
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Hd in Equation 7.82 is the Hamiltonian for the bound component of the motion over the final surface 2 h2 q l2 Hd ¼ þ V þ ; ð7:84Þ r d d 2m2 rd qrd2 2m2 rd2 2 1 1 2 with m1 2 ¼ mX þ mY2 being the reduced mass and l ðcÞ ¼ L ðcÞ, where I is the rotational angular momentum operator associated with the diatomic fragment XY2 . VðR; r0 ; cÞ is the lower state adiabatic energy potential surface E1 , where the instantaneous interatomic distance of the diatomic fragment is replaced by its suitable equilibrium value r0 (the diatomic bond in the interaction region, at the apex of the cone). The potential VðR; r0 ; cÞ is not known analytically, but numerically ˚ in the region of strong for various values of R and c (at constant r0 ¼ 1:15 A) nonadiabatic interaction around the apex of the double cone (Figure 7.25). As a ˚ the potential VðR; r0 ; cÞ is attractive over the function of R, for R extending to 1:8 A, interval 0 c < 150 . For c outside this interval, VðR; r0 ; cÞ is repulsive. (The origin of the energy scale for VðR; r0 ; cÞ in Equation 7.82 is taken at the energy of the completely separated products OH þ þ H.) The diatomic potential Vd in Equation 7.84 is taken to be a simple harmonic oscillator of the form
1 Vd ¼ m2 v2d ðrd r0 Þ2 De 2
ð7:85Þ
with vd being the vibrational frequency.
Figure 7.25 Potential energy surface of the lower adiabatic surface E1 of H2 O þ in the region of strong nonadiabatic interaction around the apex of the double cone plotted as
function of Jacobi coordinates R and c. The insert shows the adiabatic potential surfaces E1 and E2 calculated in Jacobi coordinates. (Note: 103 hartree is equivalent to 219 cm1.)
7.6 Electronic Predissociation of the 2B2 State of H2O þ
As is usually done in atom–diatom scattering theory [263–266], we expand the final-state wavefunction in terms of diatomic basis functions. We choose these functions to be harmonic oscillator rigid rotor functions wn;l;0 ðrd ; c; 0Þ ¼ xn ðrd ÞYl;0 ðc; 0Þ;
ð7:86Þ
where xn ðrÞ ¼ gn ðjÞ=r is the diatomic vibrational wavefunction with gn ðjÞ ¼ ðb1=2 =p1=2 2n n!Þ1=2 exp ðbj2 =2ÞHn ðb1=2 jÞ;
j ¼ rd r0
ð7:87Þ
and Hn is the nth Hermite polynomial. These functions are, to good approximation solutions of the equation, 2 2 h q 1 1 2 2 v ðr r Þ ðr Þ ¼ h v n þ ð7:88Þ r x m x ðrd Þ: 0 d d d n 2 2m2 rd qrd 2 2 2 n It should be noted, however, that the diatomic basis functions of Equation 7.86 are not true eigenfunctions of the diatomic Hamiltonian Hd . This becomes evident if we calculate the matrix elements of the diatomic Hamiltonian between the basis functions (7.86) ðwnl0 jHd jwn0 l0 0 Þ ¼ enl dnn0 dll0 þ
2 lðl þ 1Þ 2 h ðxn 1=rd 1=r02 xn0 Þdll0 ; 2m2
ð7:89Þ
where 1 þ Blðl þ 1ÞDe ; en;l ¼ hvd n þ 2
ð7:90Þ
with vd and B ¼ h2 =2m2 r02 ¼ h2 =2I being, respectively, the vibrational frequency and the rotational constant of the diatomic fragment. The centrifugal coupling term in Equation 7.89 couple the rotational and the vibrational motion of the diatomic. The frequency factor in the oscillator function, Equation 7.87, is defined as b ¼ m2 vd = h. The spherical harmonics in Equation 7.87 reduce to ordinary Legendre polynomials rffiffiffiffiffiffiffiffiffiffiffiffi 2l þ 1 Yl;0 ðc; 0Þ ¼ ð7:91Þ Pl ðcos cÞ: 4p The total wavefunction of the system must be an eigenfunction of the total angular momentum J and its z-component (M) in the space-fixed frame xy [264]. Since J ¼ 0, the total wavefunction, specified by the Hamiltonian (7.82), may therefore be written as a sum of products X xf ðR; rd ; cÞ ¼ xn ðrd ÞYl;0 ðc; 0ÞWnl;E ðRÞ=R; ð7:92Þ n;l
where Wnl;E are expansion coefficients to be determined numerically. All that remains is to determine these functions subjected to the boundary condition corresponding to those of the bound vibrational–rotational states of the system. To do this, let the Hamiltonian (7.82) operate on the function of this type and
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take matrix elements of (7.82) with respect to the vibrational and angular function. This gives 2 3 2 2 2 h d h 4 þ lðl þ 1ÞðEenl Þ5Wnl;E ðRÞ þ 2m1 dR2 2m1 R2 X xn Yl;0 V R; rd ; c xn0 Yl0 ;0 Wn0 l0 ;E ðRÞ n0 ;l0
þ
X 2 h lðl þ 1Þ ðxn 1=rd2 1=r02 xn0 ÞWn0 l;E ðRÞ ¼ 0: 2m2 n0
The Equation 7.93 may be written in a more concise form X ½Hnl ðEenl ÞWnl:E þ Vnl;n0 l0 Wn0 l0 ;E ¼ 0
ð7:93Þ
ð7:94Þ
n0 l0 6¼nl
by introducing the notation Vnl;n0 l0 ¼ Ll;l0 dll0 þ xn Yl;0 V R; rd ; c xn0 Yl0 ;0 dnn0 þ 2 h lðl þ 1Þ xn 1=rd2 1=r02 xn0 dll0 ; 2m2
ð7:95Þ
with Ll;l ¼
2 h lðl þ 1Þ 2m1 R2
ð7:96Þ
and Hnl ¼
2 d2 h þ Vnl;nl : 2m1 dR2
ð7:97Þ
In arriving at Equation 7.94, we have used the fact that the spherical harmonic Yl0 ðc; 0Þ is an eigenfunction of L2 and l2 L2 Yl0 ¼ l2 Yl0 ¼ h2 lðl þ 1ÞYl0 ;
ð7:98Þ
since L2 and l2 are diagonal in l, respectively. Equation 7.94 are identical to that that arises in the atom-diatomic scattering problem. They are a set of coupled differential equations. Each equation, or channel, is labeled by the set of quantum numbers ðnlÞ. The solution of these equations with the appropriate boundary conditions Wnl;E ðRÞ !0 R!0 !0 Wnl;E ðRÞ R!1
ð7:99Þ
corresponds to bound states at energies Enl;i , in particular, if ðEnl enl ÞVnl;nl < 0 for large R. This boundary conditions differ from those of scattering theory in that the wavefunction for the scattering coordinate R must go to zero at both R ¼ 0 and
7.6 Electronic Predissociation of the 2B2 State of H2O þ
R ¼ 1 rather than just at R ¼ 0 as in the scattering case. These boundary conditions are in fact identical to those of closed channels in scattering theory. We now utilize this fact and set up an artificial scattering problem in which the bound-state problem of interest forms the closed channels of a scattering problem [264]. This in turn enables us to use with a modification the standard techniques of molecular scattering theory [276–279]. In the following, it will often be convenient to condense our notation. For example, a single label a ¼ ðnlÞ may be employed to indicate state and channel. The label a0 will mean in general ðn0 l0 Þ a different specific channel and state of that channel. Then we may write quite generally X ½Ha ðEea ÞWa þ Vaa0 Wa0 ¼ 0: ð7:100Þ a0 6¼a
We have commented on the fact that the set of Equation 7.100 are identical to that arising in the atom-diatomic scattering problem. To utilize the well-developed theory of molecular scattering processes, the boundary conditions, as have been stated above, must correspond to continuum scattering states and not to the bound states as given by Equation 7.99. This can be accomplished by adding two additional equations, or channels denoted by b and c, to the set of coupled equations (7.100). Both these extra channels are open at large R and correspond asymptotically to scattering states that are oscillatory, that is, ðEeb ÞVbb > 0 for large R. The augmented set of differential equations has the form [264] ½Ha ðEea ÞYa þ
X
Vaa0 Ya0 ¼ Vac Yc ;
a ¼ 1; 2; . . . ; n;
ð7:101aÞ
a0 6¼a
½Hb ðEeb ÞYb ¼
X
Vba0 Ya0 ;
ð7:100bÞ
a0
½Hc ðEec ÞYc ¼ 0;
ð7:101cÞ
where Vab and Vac are the potential matrix elements coupling the artificial channels b and c to the bound-state channels a, respectively. Note that the two scattering channels are not coupled to each other directly. The boundary condition for the additional channel c that the wavefunction vanish at infinity is replaced by Yc ðRÞ ! sinðkc R þ jc Þ: R!1
ð7:102Þ
This condition restricts the form of Yc ðRÞ for large R. Here, k2c ¼ ð2m1 = h2 ÞðEec Þ specifies the c channel wave number of the outgoing wave, with Eec being the asymptotic fragment energy. The real number jc is known as the phase shift, since it specifies the change of the phase of the outgoing wave due to the influence of the potential Vac . The Equation 7.101 appearing here have been used in Ref. [264] to calculate the vibrational–rotational energy levels of H2 O and the transition ampli-
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tudes or Tb ! c matrix element for an inelastic collision from channel b to channel c.4) The calculation of the vibrational–rotational levels has been carried out using a basis set of 47 (or 46) coupled channels (45 or 44 for the bound-state manifold and two for the extra channels). Considering the right-hand side of Equation 7.101 as an inhomogeneous term, the radial wavefunctions Ya of Equation 7.101 may be expressed as [264] 1 Xð Ya ðRÞ ¼ Gaa0 ðR; R0 ; EÞVa0 c ðR0 ÞYc ðR0 ÞdR0 ; ð7:103Þ a0
0
where Gaa0 is the Greens function corresponding to the left-hand hand side of Equation 7.101a and Yc are solutions of the uncoupled Equation 7.101c with the boundary condition of Equation 7.102. These solutions, regular at R ¼ 0, are given by the following integral equation [269, 270]: 1 ð 2 Yc ðRÞ=R ¼ jl ðkc RÞ þ ð2m1 kc =h2 Þ jl ðkc R< Þnl ðkc R> ÞVcc ðR0 ÞYc ðR0 ÞR0 dR0 ; 0
ð7:104Þ 0
where gl ðR; R Þ ¼ kc jl ðkc R< Þnl ðkc R> Þ is the Green function corresponding to the operator Hc with R< being the lesser and R> the greater of R and R0 . Here, jl ðkc RÞ and nl ðkc RÞ are, respectively, the spherical Bessel and the spherical Neumann functions of the first kind [271]. Both are particular solutions of the homogeneous counterpart of Equation 7.101c (when Vcc ¼ 0). Using the spectral resolution of a Greens function, the Greens function that appears inside the integrand (7.103) can be expressed (in the R-representation) in terms of eigenstates of the closed-state channels (7.94) 0
Gaa0 ðR; R ; EÞ ¼
X Wai ðRÞWa0 i ðR0 Þ i
EEi
1 ð
þ 0
Wa ðE 0 ; RÞWa0 ðE 0 ; R0 Þ dE 0 : E þ E 0
ð7:105Þ
The first term in Equation 7.104 is a summation over all the bound states Wai ðRÞ corresponding to the energies Ei of the original problem (Equation 7.94) and the second term is an integral over the continuum solution (E 0 ) of the same problem. We have so far not dealt with the potential energy matrix elements involving the extra two channels b and c. The theory leaves us here a more or less free choice. The only constraint on these matrix elements is that they must vanish at large R. (A diagonal potential matrix element of realistic strength is Vcc ¼ AexpðaRÞ and correspondingly for the off-diagonal ones Vac ¼ A0 expða0 RÞ). The kinetic energy E in the extra channels should also be chosen to be small so that the radial wavefunction should not be too oscillatory.5)
4) The T matrix element or precisely its energy dependence is applicable, for example, for the problem of determining the exact bound state energies Ei. 5) Wc oscillates very rapidly as kl becomes large.
7.6 Electronic Predissociation of the 2B2 State of H2O þ
The above calculations are quite extensive and highly specialized. To explore this problem further would take us well beyond the scope of this book, for we should have to review the entire area of quantum calculations of the three-dimensional reactive scattering problem. The reader who wishes to acquire even an elementary working knowledge to this methodology will find an extensive literature (of dedicated journals and books) on all aspects of this subject [272–280]. Thus, the present treatment of determining the radial function Wnl;E must be viewed as a brief introduction to this subject; this introduction may help the reader to be acquainted with the formalism.
j223
j225
8 Multidimensional Franck–Condon Factor The consideration, which we will now in Chapter 8 devote to the rather old-fashioned Franck–Condon (FC) factor or the FC integral, may be greeted by the reader with some initial skepticism. These reservations and skepticism will be dispelled, at the latest, once we have explored a few applications in which we employ the FC integral. To obtain a complete description for even the simplest molecules, we wish to generalize our treatment to include several nonseparable normal modes. This means that the generating function, by which the factors will be derived, is a multidimensional function that depends on several dummy variables. The generating function incorporates the transformation (rotation) of both the normal mode coordinates between the initial and final electronic states and their frequency distortions. Both of them scramble the occupations of the normal modes, leading to unusual distributions. At certain values of the angle of rotation, the distribution may reduce to only a few modes or even to a single mode. Mathematically, this selectivity can be described in terms of normal mode displacement parameters generated by the rotation matrix. These normal mode displacements, as well as the set of crossed frequency parameters due to mode mixing, have no counterparts in the parallel mode approximation and are the reason that polyatomic FC integrals are of formidable analytical complexity. This complexity is analyzed with particular attention to the resemblance between the FC factors and the intramolecular distributions (IDs) used in our previous chapters. As an illustration of this complexity, calculations of the scattered intensities in the resonance Raman process as well as the study of sequential two-photon processes are presented. These show a strong dependence on the rotation angles.
8.1 Multidimensional Franck–Condon Factors and Duschinsky Mixing Effects 8.1.1 General Aspects
In Chapters 3 and 4, a multidimensional ID was derived that most often describes the complex problems of molecular spectroscopy such as nonradiative and any radiative
j 8 Multidimensional Franck–Condon Factor
226
(allowed and vibronically induced) transitions. The ID enters into the emission or absorption spectral line shape (SLS) directly as the square of the vibrational overlap integral convoluted with a Lorentzian profile. This convolution that creates a band shape function is weighted by electronic coupling factor. The Lorentzian, being a function of the variable frequency v, is centered around the individual vibronic components involved in the transition. The relative intensity distribution of these components is then governed by the values of the ID. In the case of radiationless transitions, the multidimensional ID appears in the decay rate expression. Here, it is coupled with a Lorentzian (to ensure energy conservation in the transition), but now v is fixed and equal to the energy gap V. The latter must be bridged by final-state vibrational quanta. This leads to a weighted sum (the weighting factors being the square of the electronic matrix elements) of density of state weighted vibrational overlaps (DSWVO), each of which includes all ground- and excited-state vibrational levels subject to the energy conservation constraint. Although the ID, as a vibrational overlap factor, is related to the Franck–Condon factor, a closer examination reveals several reasons for performing the former, which we enumerate below. First, the ID for N (separable or nonseparable) vibrational modes is derived from the knowledge of generating function GN . The Fourier transformation of GN is a DSWVO (or a line shape function), the latter of which appears in the decay rate expression (or in the SLS for any radiative transition). Thus, by expanding the generating function in a multiple power series (the coefficients of which are given by the values of an ID for several occupation number sets), the Fourier transformation of GN and therefore the aforementioned spectroscopic quantities can be calculated. This is what makes the ID so manageable. Second, since the ID for an arbitrary set of vibrational occupation numbers, m1 ; m2 ; . . . ; mN ; n1 ; n2 ; . . . ; nN , can be obtained by equating coefficients of the 2N expansion variables in the infinite multiple power series of GN , the IDs can be easily convoluted with themselves through the use of simple rules for multiplication of power series. In this way, some addition theorems concerning the normal mode shifts and the order (dimension) of the IDs can be derived (see Sections 4.1.1 and 4.2.2). So the convolution of two or more IDs of given orders leads to a joined ID, the order of which is equal to the sum of the orders of the factors. This important aspect of the ID is of practical use in treating dense manifolds of vibronic states that occur in the statistical limit. Third, as a consequence of the foregoing, the use of IDs is suitable in investigating the dependence of the electronic matrix element for radiationless transition on the nuclear coordinates. This problem can be solved, as has been shown in Chapter 5, by considering the matrix element as one that of an operator that depends upon both electronic and nuclear displacements and by introducing a q-centroid approximation for the electronic factor. The latter is obtained as an average with DSWVO factor. The familiar Condon approximation can be so improved as to write the whole matrix element as a product of a vibrational overlap integral and an electronic factor, the latter being evaluated at some q-centroid for the nuclear positions. It is not clear what the most useful applications of such procedure will turn out to be. We have already mentioned the determination of the q-centroid for evaluating
8.1 Multidimensional Franck–Condon Factors and Duschinsky Mixing Effects
matrix elements. There are applications to the theory of radiative and nonradiative transitions. In addition, a number of applications have been given in Chapter 7. A similar study of the effect of anharmonicity in the vibrational motion is not too far behind. For historical reasons, there is a great deal of satisfaction in solving the multimode problem (with high vibrational degrees of freedom) analytically or at least in reducing it to lower dimensionality in a manner that the problem becomes qualitatively understood. Despite the advantages of using the IDs in a wide range of spectroscopic phenomena, the determination of polyatomic FC factors currently has great appeal [281]. The FC integrals prominently appear in the so-called vibronic theories of Raman and resonance Raman intensities and in studies of time-delayed two-photon processes, the cross sections of which are obtained by adding amplitudes and then squaring (see below). In addition, the FC factors find the widest application in calculations of matrix elements between several molecular eigenstates. Calculations of such factors present some difficulties or problems (as also appears in calculating multidimensional IDs). In polyatomic molecules, this difficulty stems from the high vibrational degrees of freedom. This is because the nuclear motion is inextricably coupled to the motion of the valence electrons. Thus, upon excitation the molecular skeleton is deformed, displacing the nuclei from the ground-state equilibrium positions. Hence, the vibrational wavefunction will be deformed as well in a manner that can be quite difficult to deduce with any precision. One copes with this problem by making the so-called adiabatic approximation. In this approximation, the normal modes of vibrations in an electronic excited state (after separation from the electronic motion) are displaced and rotated relative to those of the electronic ground state. Since this normal mode rotation (and consequently mixing) cannot always be ignored, we must deal from the start with a multidimensional FC integral that is of formidable analytical complexity and that cannot be represented in many cases as a product of integrals of lower dimensionality that are easier to calculate. One of the earliest attempts at a quantitative analysis of the problem was put forward by Coon, DeWames, and Loyd [282] in an approximate method for calculating two-dimensional integrals specifically for nonlinear triatomic systems. Later, Sharp and Rosenstock [283] developed a more general approach in which a generating function was derived and the FC factors are obtained as coefficients in the expansion of this function in a multiple power series of dummy variables. In this way, they were able to determine relative probabilities of transitions starting from the vibrationless level (i.e., having zero vibrational quanta in all of the normal modes) of the ground (initial) electronic state of linear, symmetric, triatomic molecules to overtones as well as to some low combination levels of the final electronic state. The generating function technique was also used by Karplus and Warshel [284, 285] in their study of vibronically assisted electronic spectra of conjugated hydrocarbons and by Doktorov et al. [286]. The latter authors have employed the coherent-state method of Glauber to derive a generating function and recurrence equations to compute the vibrational overlap integral. However, the coefficients in these recurrence equations are given for only N ¼ 2. The authors
j227
j 8 Multidimensional Franck–Condon Factor
228
applied their method to analyzing the intensity distribution of a single mode progression in the 1 A1g ! 1 B2u electronic transition in benzene. Another approach for calculating polyatomic FC factors has been reported by Faulkner and Richardson [287]. As an alternative to the previous methods, they used contact transformation perturbation operator of the form U ¼ expðiSðp; qÞÞ to construct the vibrational wavefunctions of an excited electronic state in terms of the vibrational wavefunctions of the ground state. Thus, the calculation of polyatomic FC factors is reduced to the evaluation of vibrational matrix elements exclusively within the ground-state vibrational manifold. In the opinion of the authors, this method has only limited applicability due to the slow convergence of the perturbation expansion of Sðp; qÞ in power series. Another method developed by the same authors used a linear transformation of the normal coordinates to remove the Duschinsky rotation. The multidimensional FC integrals are then written as sums of factorizable integrals in the new intermediate nuclear coordinates. This method having markedly better computational efficiency than the perturbation method is restricted to the zero-temperature limit (i.e., when one of the vibrational wavefunctions in the FC integral is vibrationless). Recently, Kikuchi et al. based on Sharp–Rosenstocks method have developed a computational algorithm to calculate MFC factors including mode mixing. As an application, the authors calculate the fluorescence spectrum of SO2 , originating from the lowest vibrational level of the excited electronic state, taking as input parameters the familiar G and F matrices of Wilson [288]. Another approach given in Ref. [289] is quite different. Here, one seeks closed-form solutions. In the sections that follow, we present a more elaborate analysis of mode mixing and give explicitly general expressions for calculating multidimensional FC integrals, from which precise qualitative and quantitative results can be extracted. The analysis is similar to that in Section 4.4. We shall take from the beginning an affine (not necessarily orthogonal) relation between the normal modes of the excited- and ground-electronic states and derive a multidimensional generating function FN . The latter quantity includes all mode mixing effects and frequency distortions. At this stage, we pause in our derivation to explain the physical phenomena governed by mode mixing. Subsequently, with the help of this generating function, a set of 2N recurrence equations (i.e., one recurrence equation for each of the excited- and ground-state occupation numbers m1 ; m2 ; . . . ; mN ; n1 ; n2 ; . . . ; nN ) is derived that offers a very convenient and efficient way of calculating polyatomic FC integrals. 8.1.2 Derivation
We consider two electronic states, l (lower or ground) and s (excited), and a set of N vibrational modes associated with these states. The harmonic vibrational wavefunctions in these states are denoted as before by xln ðql Þ and xsm ðqs Þ, respectively, where n ¼ fnm g represents the collection of vibrational occupation numbers in the normal coordinates, ql , of the lower electronic state, and m ¼ fmm g represents the collection of the vibrational occupation numbers in the normal coordinates, qs , of the excited
8.1 Multidimensional Franck–Condon Factors and Duschinsky Mixing Effects
electronic state. The relation between both sets of normal coordinates qs and ql is given by qs ¼ Wql þ k1 2 N ;
ð8:1Þ
or explicitly by Equation 4.57. The vector k1 2 N describes the shift of the coordinates qs measured in a coordinate system with base vectors qlm ðm ¼ 1; 2; . . . ; NÞ. In the notation established above, the FC integral associated with an electronic transition, jsmi , jlni, is given by JN
m1 ; m2 ; . . . ; mN n1 ; n2 ; . . . ; nN
1 ð
¼
xsm ðqs Þxln ðql Þdql ;
ð8:2Þ
1
where the vibrational wavefunctions xsm ðqs Þ and xln ðql Þ are expressed explicitly as an N-fold product of one-dimensional harmonic oscillator functions (Equation 3.1). If we assume that the transformation (8.1) is affine, then the right-hand side of Equation 8.2 should be multiplied by the normalization constant of xsm ðqs Þ, ðdet WÞ1=2 .1) To derive the generating function for JN, we start from the well-known generating function for the Hermite polynomials X1 k
k!
Hk ðxÞuk ¼ exp u2 þ 2ux ;
ð8:3Þ
where u is a dummy variable. With the help of Equations 1.49 and 8.3, we can write for every mode m in the excited electronic state 1 1=2 mm 1=4 X 1=2 1=2 1 2 wm xsmm bsm qsm ¼ exp wm2 þ 2wm bsm qsm bsm qsm p=bsm 2mm =mm ! 2 mm ð8:4aÞ
and analogous expressions for the electronic state jli 1 1=4 X 1=2 1=2 nm 1=2 1 2 p=blm 2nm =nm ! zm xsnm blm qlm ¼ exp z2m þ 2zm blm qlm blm qlm : 2 nm ð8:4bÞ
Now, multiplication of all 2N equations (8.4) with themselves and subsequent integration with respect to ql yields 1 X
1 X
w1m1 w2m2 wNmN zn11 zn22 znNN
m1 ;m2 ;...;mN ¼0n1 ;n2 ;...;nN ¼0
ð2ðm1 þ m2 þ þ mN þ n1 þ n2 þ þ nN Þ =m1 !m2 ! mN !n1 !n2 ! nN !Þ1=2 1) TheÐ normalization constant C is determined from the relation (8.1) by the requirement that C 2 jxsm ðqs Þj2 dN ql ¼ 1.
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j 8 Multidimensional Franck–Condon Factor
230
JN
m1 ; m2 ; . . . ; mN n1 ; n2 ; . . . ; nN
0 1N=2 ð ð N Y 1=4 1 1 bsm blm dN ql ¼@ A p 1 m¼1
2
3 1 s t s s 1 l t l l t s1=2 s 1=2 l t l exp4ðw w þ z zÞ þ 2 w b q þ z b q ðq Þ b q ðq Þ b q 5: 2 2 t
t
ð8:5Þ s
l
Here, w and z are N-dimensional column vectors (as are q and q ) of the dummy variables and bs and bl are diagonal matrices with elements ðbs Þmm ¼ bsm and ðbl Þmm ¼ blm , respectively. In writing Equation 8.5, we suppressed the parametric dependence of JN on the spectroscopic parameters. The integrand, as it is written in Equation 8.5, contains different sets of coordinates qs and ql . Therefore, to evaluate the integral, we utilize Equation 8.1 and rewrite the right-hand side of Equation 8.5 in the form " ð1 ð 1 Y 1 N=2 s l 1=4 N l bm bm FN ¼ ð1=pÞ d q exp wt w þ zt z ðql Þt xql 2 1 m¼1 þ
yt1
þ yt2
þ yt3
where
x ¼ WT bs W þ bl ¼
k
# N N X 2 1X s ðmÞ s1=2 ðmÞ q b k þ 2 bm k12 N wm ; 2 m¼1 m 12 N m¼1 l
N X 2 s wm1 bm þ bl1 m¼1 N X m¼1
wm2 wm1 bsm .. .
N X m¼1
wmN wm1 bsm
P
s m wm1 wm2 bm
l 2 s m wm2 bm þ b2
P
P
s m wm1 wmN bm
P
s m wm2 wmN bm
.. .
P
s m wmN wm2 bm
ð8:6Þ
P
.. .
s l 2 m wmN bm þ bN
k
ð8:7Þ
and yt1
yt2
¼
N X m¼1
¼2
ðmÞ wm1 bsm k12 N ;
N X m¼
1=2 wm1 bsm wm ;
X m
X m
ðmÞ wm2 bsm k12 N ; . . . ;
1=2 wm2 bsm wm ; . . . ;
1=2
1=2 1=2 yt3 ¼ 2 bl1 z1 ; bl2 z2 ; . . . ; blN zN :
X m
X m
! ðmÞ wmN bsm k12 N
;
ð8:8aÞ
! 1=2 wmN bsm wm
;
ð8:8bÞ
ð8:8cÞ
8.1 Multidimensional Franck–Condon Factors and Duschinsky Mixing Effects
Note that the matrix x, Equation 8.7, resembles those in Section 4.4 with the exception that now the dummy variables disappear in the matrix (8.7). The integral (8.6) is a multiple Gaussian integral over ql that can be carried out using the general formula (4.63). Thus, we find FN ðw1 ; w2 ; . . . ; wN ; z1 ; z2 ; . . . ; zN Þ ¼ FN ð0; . . . ; 0; 0; . . . ; 0Þ
ð8:9Þ
exp½D11 þ D22 þ D12 þ D1 þ D2 þ wt wzt z;
where D11 ¼
1 t 1 y x y2 2wt w; 2 2
ð8:10aÞ
D22 ¼
1 t 1 y x y3 ; 2 3
ð8:10bÞ
D12 ¼
1 t 1 1 t 1 y x y3 þ y3 x y2 ; 2 2 2
ð8:10cÞ
D1 ¼
N X 1=2 ðmÞ 1 t 1 1 t 1 bsm k12 N wm ; y1 x y2 þ y2 x y1 þ 2 2 2 m¼1
ð8:10dÞ
D2 ¼
1 t 1 1 t 1 y x y3 þ y3 x y1 ; 2 1 2
ð8:10eÞ
and N=2
FN ð0; . . . ; 0; 0; . . . ; 0Þ ¼ 2
N Y m¼1
¼ 2N=2
N Y m¼1
2
1=4 1 1 bsm blm exp4 y1t x 1 y1 h
bsm =blm
2
1=4 exp 12 A=B
2 m¼1
i
ðBÞ1=2
3 N X 2 s ðmÞ bm k12 N 5
; ð8:11Þ
with A¼
X 1 j1 N
þ
ð1 2 NÞ2
Dj1
X
þ
X
X
ði i iN1 Þ2
1i1
X
1i1
ði i i Þ2 Dj1 1j2 j23 N2
Dj1 1j2 2
þ þ
X 1i1 N
ði Þ2 D1 12 N ;
ð8:12Þ
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j 8 Multidimensional Franck–Condon Factor
232
where i1 < i2 < ip forms a complete system of r lexicographically ordered indices as do j1 < j2 < jq , both taken from among the indices 1; 2; . . . ; N and subject to the condition p þ q ¼ N þ 1, and B¼W
12 N 12 N
2
N 2 ða11 22 N Þ
X
þ
X
W
1i1 <
X
X
þ
1i1 <
i1 i2 iN1 j1 jp1 jp þ 1 jN
W
j1 jp1
2
2 ðaij11 i2 jp1iN1 jp þ 1 jN Þ
i1 i2 iN2 jp þ 1 jq1 jq þ 1 jN
2
2 iN2 ðaij11 i2 jp1 jp þ 1 jq1 jq þ 1 jN Þ þ þ 1:
ð8:13Þ
In arriving at these results, we have made use of the Binet–Cauchy formula that enables us to express the minors of the product Wt W in terms of minors of the i i ip factors. The latter are denoted in Equation 8.13 by W 1 2 , where the upper j1 j 2 j q indices refer to the rows and the subindices to the columns of the matrix W. Note that expressions (8.12) and (8.13) have the same algebraic form as the expression for d0;0 and a0;0 in Section 4.4 (see Equations 4.68 and 4.71). They have the feature of being diagonal in terms of quantities that contain all the dependence on rotation angles and ði i i Þ
geometrical distortion. The quantities Dj1 1j2 2 jp p in Equation 8.12 are dimensionless geometrical displacement parameters associated with the s , l transition and i i i
aj11 j22 jpp in Equation 8.13 are generalized parameters describing the frequency changes of normal modes in the ðsÞ and ðlÞ states. The former are scaled (relative to the dimensioned ones) as follows: ð1 2 NÞ D ip
¼
ði i2 jN1 Þ
Djp 1jq
ð1 2 NÞ kjp
bs1 bs2 bsN
bl1 bl2 bljp1 bljp þ 1 blN
ði i iN1 Þ
¼ kjp 1jq 2
!1=2
bsi1 bsi2 bsiN1
ð1 jp NÞ;
ð8:14aÞ
!1=2
bl1 bljp1 bljp þ 1 bljq1 bljq þ 1 blN
ð8:14bÞ
... ði Þ
ði Þ
D1 12 N ¼ k1 12 N bsi1
1=2
ð1 i1 NÞ;
ð8:14cÞ
8.1 Multidimensional Franck–Condon Factors and Duschinsky Mixing Effects ði i i Þ
where the interactive displacement parameters kj1 1j2 2 jp q ð1 < p N; q < NÞ are defined by Equation 4.69. The generalized frequency change parameters are defined as i i i aj11 j22 jpp
bsi1 bsi2 bsip
¼
!1=2 ð1 i1 NÞ:
blj1 blj2 bljp
ð8:15Þ
Note the full resemblance of the expressions for A and B to the previously derived expressions A1 and B1 in Chapter 4. The former are obtained from the expressions A1 and B1 , respectively, by dividing both of them by bl1 bl2 blN. Consequently, the scaling to dimensionless quantities according to Equations 8.14 and 8.15 differs from those defined earlier in Section 3.2 for N ¼ 2 (see Equations 3.28 and 3.29). Indeed, for the special case of N ¼ 2, we now find from Equations 8.14a and 8.14c ðmÞ
ðmÞ
D12 ¼ bsm k12
ð12Þ D1
1=2
¼
bs1 bs2 bl2
ðm ¼ 1; 2Þ;
!1=2 ð12Þ k1
and
ð12Þ D2
¼
bs1 bs2 bl1
!1=2 ð12Þ
k2 ;
which differ slightly from those defined in Section 3.2 by just the prefactors. From Equations 8.11 to 8.15, which (as will be seen more explicitly below) describe 0; 0; . . . ; 0 the FC integral FN , we observe that mode mixing due to coordinate 0; 0; . . . ; 0 rotation gives rise to whole sets of displacement parameters and frequency change parameters that have no counterparts in the parallel mode approximation. Note that ðmÞ
ðmÞ
in the latter case the integral JN depends solely upon k1 2 N (or D1 2 N ) and m
am ¼ ðbsm =blm Þ1=2 per mode. This means that the variety of spectroscopic phenomena that can be described if mode mixing is accounted for is considerably richer than in the case of no mode mixing. Some of these effects have been illustrated in Chapters 4 and 7, where the consequences of normal mode rotation on the spectral band shape and radiationless transitions have been investigated. Here, we only note that the displacement parameters (8.14) depend on the matrix W via the dimensioned ðmÞ
parameters k1 2 N (Equation 4.69), and therefore some of them can be zero in m1 ; m2 ; . . . ; mN special cases. As a consequence of this, the integral JN becomes n1 ; n2 ; . . . ; nN strongly selective. This explains the absence of any observable contribution of some vibrational degrees of freedom in the integral. Returning to the derivation, we can show from Equation 8.9 using the procedure applied previously in this section that
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j 8 Multidimensional Franck–Condon Factor
234
N X
2 D11 ¼ bmg wm wg ¼ B m;g¼1
(
1j1 N
X
X
þ
X ð1 2 NÞ 2 ðw1 ; w2 ; . . . ; wN Þ Xj1
1i1
þ þ
ði1 i2 iN1 Þ 2 Xj1 j2 ðwi1 ; wi2 ; . . . ; wiN1 Þ
X
X
1i1
ði1 i2 Þ 2 Xj1 j2 jN1 ðwi1 ; wi2 Þ
) þ w12 þ w22 þ
þ wN2
;
ð8:16Þ
where ð1 2 NÞ
X1
ðw1 ; w2 ; . . . ; wN Þ
23 N 13 N N N a22 33 a12 33 w W N 1 N w2 23 N 23 N 1 2 N1 1 2 N1 þ þ ð1ÞN þ 1 W a2 3 N wN ; 23 N 23 N ð1 2 NÞ N a21 33 ðw1 ; w2 ; . . . wN Þ ¼ W X2 N w1 13 N 13 N 1 2 N1 1 2 N1 N þW w2 þ þ ð1ÞN þ 2 W a11 33 a1 3 N wN ; N 13 N 13 N ¼W
ð1 2 NÞ
XN
ðw1 ; w2 ; . . . ; wN Þ ¼ ð1ÞN þ 1 W
þ þ ð1Þ2N W ði i2 iN1 Þ
X121
23 N a2 3 N w 1 2 N1 1 2 N1 1
1 2 N1 1 2 N1 a w ; 1 2 N1 1 2 N1 N
ðwi1 ; wi2 ; . . . ; wiN1 Þ ¼ W
i2 i3 iN1 ai32 4i3NiN1 wi1 34 N
i1 i3 iN1 ai31 4i3NiN1 wi2 34 N i i iN2 þ þ ð1ÞN W 1 2 ai31 4i2NiN2 wiN1 ; 34 N i2 i3 iN1 ði1 i2 iN1 Þ ai22 4i3NiN1 wi1 X13 ðwi1 ; wi2 ; . . . ; wiN1 Þ ¼ W 24 N i i iN1 ai21 4i3NiN1 wi2 þW 1 3 24 N W
ð8:17aÞ
8.1 Multidimensional Franck–Condon Factors and Duschinsky Mixing Effects
i i iN2 þ þ ð1ÞN þ 1 W 1 2 ai21 4i2NiN2 wiN1 ; 24 N ði i i
Þ
1 2 N1 ðwi1 ; wi2 ; . . . ; wiN1 Þ ¼ ð1Þ1=2NðN1Þ W XN1;N
þ ð1Þ1=2NðN þ 1Þ W
i2 i3 iN1 ai2 i3 iN1 w 1 2 N2 1 2 N2 i1
i1 i2 iN2 ai1 i2 iN2 w 1 2 N2 1 2 N2 iN1
ð8:17bÞ
for all combinations of the N1 indices 1 i1 < i2 < < iN1 N selected from among the indices 1 2 N and arranged in a lexicographic order,
and finally i2 i aiN2 wi1 W 1 aiN1 wi2 ; N N i2 i1 ði1 i2 Þ 2 ðwi1 ;wi2 Þ ¼ W wi1 þW aiN1 ai 1 w ; X1 2N2;N N1 N1 N1 i2 ði i Þ
1 2 X1 2 N1 ðwi1 ;wi2 Þ ¼ W
ði i Þ
1 2 ðwi1 ;wi2 Þ ¼ ð1ÞN þ1 W X2 3N
i 2 i2 i a1 wi1 þð1ÞN W 1 ai11 wi2 ð1 i1 < i2 NÞ: 1 1 ð8:17cÞ
Similarly, D22
N X
2 ¼ amn zm zn ¼ B m;g¼1 þ
(
X
1i1 N
X
X
1i1
þ
X
ði Þ
½Y1 12 N ðz1 ; z2 ; . . . ; zN Þ2
X
1i1
ði i Þ
Yi1 1j2 2 iN1 ðzj1 ; zj2 ; . . . ; zjN1 Þ
2
þ
) 2 ði1 i2 iN1 Þ 2 2 2 ðzj1 ; zj2 Þ þ z1 þ z2 þ þ zN ; Yj1 j2 ð8:18Þ
where
ð1Þ
Y1 2 N ðz1 ; z2 ; . . . ; zN Þ ¼ W þ þ ð1ÞN þ 1 W
23 N 23 N N N a22 33 a21 33 z W N 1 N z2 23 N 13 N
23 N N a21 32 N1 zN ; 1 2 N1
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j 8 Multidimensional Franck–Condon Factor
236
13 N N a12 33 N z1 23 N 1 3 N 1 3 N 13 N N þ2 a a1 3 N z ; þW z þ þ ð1Þ W 1 3 N 1 3 N 2 1 2 N1 1 2 N1 N
ð2Þ
Y1 2 N ðz1 ; z2 ; . . . ; zN Þ ¼ W
ðNÞ
Y1 2 N ðz1 ; z2 ; . . . ; zN Þ ¼ ð1ÞN þ 1 W þ þ ð1Þ2N W
1 2 N1 N1 a12 23 N z1 23 N
1 2 N1 N1 a11 22 N1 zN ; 1 2 N1
ð12Þ
Yj1 j2 jN1 ðzj1 ; zj2 ; . . . ; zjN1 Þ ¼ W
ð8:19aÞ
34 N a3j2 4j3NjN1 zj1 j2 j3 jN1
34 N a3j1 4j3NjN1 zj2 j1 j3 jN1 34 N þ þ ð1ÞN W a3j1 4j2NjN2 zjN1 j1 j2 jN2 24 N ð13Þ Yj1 j2 jN1 ðzj1 ; zj2 ; . . . ; zjN1 Þ ¼ W a2j2 4j3NjN1 zj1 j2 j3 jN1 24 N a2j1 4j3NjN1 zj2 þW j1 j3 jN1 24 N N þ1 þ þ ð1Þ W a2j1 4j2NjN2 zjN1 ; j1 j2 jN2 W
1 2 N2 ðN1;NÞ Yj1 j2 jN1 ðzj1 ; zj2 ; . . . ; zjN1 Þ ¼ ð1Þ1=2NðN1Þ W a1j2 2j3N2 jN1 zj1 j2 j3 jN1 1 2 N2 a2j1 4j2NjN2 zjN1 ; þ þ ð1Þ1=2NðN þ 1Þ W j1 j2 jN2 ð8:19bÞ
and finally ð1 2 N1Þ Yj1 j2 ðzj1 ; zj2 Þ
ð1 2 N2;NÞ
Yj1 j2
¼W
N j2
ðzj1 ; zj2 Þ ¼ W
! aN j2 zj1 W N1 j2
ð2 3 NÞ Yj1 j2 ðzj1 ; zj2 Þ
þ ð1ÞN W
¼ ð1ÞN þ 1 W
1 a1j1 zj2 ; j1
!
N
!
j1
aN j1 zj2 ;
aN1 zj1 þ W j2
N1 j1
! aN1 zj2 ; j1
1 a1j2 zj1 j2
ð1 j1 < j2 NÞ:
ð8:19cÞ
8.1 Multidimensional Franck–Condon Factors and Duschinsky Mixing Effects
The bilinear term D12 , Equation 8.10c, is somewhat tedious to derive (because of the complicated algebra involved) and is given explicitly by D12 ¼
N X
cpq wp zq ;
ð8:20Þ
p;q¼1
where cpq ¼
4 1 2 N 1 2 p1; p þ1 N 1 2 p1; p þ1 N N W ð1Þpþ q W a11 22 a1 2 q1; q þ1 N N 1 2 N 1 2 q1; q þ 1 N B X
þ
ð1Þr þs W
1i1 <
i1 ir1 ; p; ir þ 1 iN1 i ir1 ; p; ir þ1 iN1 aj11 js1 ; q; jsþ 1 jN1 j1 js1 ; q; js þ1 jN1
1j1 < <js1
W þ
i1 i2 ir1 ir þ 1 iN1 i1 i2 ir1 ir þ1 iN1 aj1 j2 js1 js þ1 jN1 j1 j2 js1 js þ1 jN1 X i ir1 ; p; ir þ 1 iN2 i ir1 ; p; ir þ1 iN2 ð1Þr þs W 1 aj11 js1 ; q; jsþ 1 jN2 j1 js1 ; q; js þ1 jN2
1i1 <
W
) i1 i2 ir1 ir þ 1 iN2 ii2 ir1 ir þ1 iN2 p p aj1 j2 js1 js þ1 jN2 þ þW a q q j1 j2 js1 js þ1 jN2
ð8:21Þ
Finally, the linear forms in wm and zm are given in terms of the quantities derived previously in Equations 8.14, 8.17 and 8.21 as follows: N X 2 D1 ¼ bm wm ¼ B m¼1
"
X 1j1 N
X
X
þ
ð1 2 NÞ
Dj1
ði i iN1 Þ
1i1
X
þ
X
1i1
ð1 2 NÞ
Xj1
ðw1 ; w2 ; . . . ; wN Þ ði i2 iN1 Þ
Dj1 1j2 2
Xj1 j1
ði i Þ
ði i Þ
ðwi1 ; wi2 ; . . . ; wiN1 Þ þ
2 Dj1 1j2 2 jN1 Xj1 j12 jN1 ðwi1 ; wi2 Þ þ
X 1i1 N
ði Þ
D1 12 N wi1 ð8:22Þ
and D2 ¼
N X
aq zq ;
ð8:23Þ
q¼1
where aq ¼
N 1X ðpÞ cpq D1 2 N : 2 p¼1
ð8:24Þ
j237
j 8 Multidimensional Franck–Condon Factor
238
To conclude this section, we briefly comment on the results expressed in Equations 8.17 and 8.19 that are of some interest. First, we observe a striking ði i i Þ
similarity between the Xj1 j12 2 jq p function set defined in Equation 8.17 and the ði i i Þ
interactive displacement parameters kj1 1j2 2 jq p derived in Section 4.4 and that occur (again) in Equation 8.14. In fact, both these sets of quantities are defined by systems of equations having the same algebraic structure, determined by the compound matrices of W or their elements. So, the coefficients in the system of Equation 8.17a are, apart from the sign, elements of the ðN1Þth compound matrix of W. Those of the system (8.17b) are elements of the ðN2Þth compound matrix of W, and so on, until the first compound matrix is achieved in the system of Equation 8.17c. In other words, the matrix W scrambles the normal modes (represented by the set of dummy variables wm ) in a way that is governed by the compound matrices of W. Next, ði i i Þ
we emphasize the simple relation between the upper and lower indices of Xi1 j12 2 jq p on i i ip the left-hand side and the indices of the minors W 1 2 and the dummy j1 j 2 j q variables wm on the right-hand side of Equation 8.17. This justified the notation adopted for the X and Y function sets. Let us now focus our attention on Equation 8.19. A comparison of Equation 8.17 with Equation 8.19 shows that the latter may be obtained by interchanging the top and bottom sets of indices on the quantities in the former and replacing the variableswm by zm and vice versa. Similar symmetry properties exhibit both the expressions A and B defined by Equations 8.12 and 8.13 and the remaining quantities appearing in FN . Hence, the generating function FN possesses a certain symmetry with respect to the exchange wm , zm . The analytical results obtained in this section for the generating function FN are valid for the case of arbitrary harmonic potentials in the ground and excited states (coordinate shifts, frequency distortion, and Duschinsky rotation). Anharmonic effects can be included by taking perturbation expansions for the vibrational wavefunctions arising from anharmonicities. To derive FN , we have assumed that all N modes mix. However, if the molecule has elements of symmetry, the configuration space is separable into subspaces comprising normal modes belonging to the same irreducible representation of the largest subgroup common to both the groundand excited-state conformations. Thus, the rotation matrix W is block diagonal and Equation 8.1 decomposes into several sets of equations belonging to single symmetry species. Consequently, the generating function FN as well as the overlap integral JN factorizes into independent contributions of the subspace dimensions and the calculational effort is diminished.
8.2 Recursion Relations
We shall now use the Equations 8.9–8.24 to evaluate the values of m1 ; m2 ; . . . ; mN JN for any occupation number set. This problem is best solved n1 ; n2 ; . . . ; nN
8.2 Recursion Relations
j239
by constructing 2N recurrence equations. There is one equation for each of the occupation numbers m1 ; m2 ; . . . ; mN ; n1 ; n2 ; . . . ; nN contained in JN . In doing this, let us come back to Equation 8.5. Using Equation 8.6, we rewrite Equation 8.5 as 1 X
1 X
m1 ;m2 ;...;mN ¼0n1 ;n2 ;...;nN ¼0
w1m1 w2m2 wNmN zn11 zn22 znNN
ð2ðm1 þ m2 þ þ mN þ n1 þ n2 þ þ nN Þ =m1 !m2 ! mN !n1 !n2 ! nN !Þ1=2 m1 ; m2 ; . . . ; mN JN n1 ; n2 ; . . . ; nN n o n o
ði i i Þ ði i i Þ ¼ FN w1 ; w2 ; . . . ; wN ; z1 ; z2 ; . . . ; zN kj1 1j2 2 jq p ; aj1 1j2 2 jr r : ð8:25Þ
Putting now w1 ¼ w2 ¼ ¼ wN ¼ 0 and therefore m1 ¼ m2 ¼ ¼ mN ¼ 0 in Equation 8.25 and differentiating with respect to zm , we obtain 1 X n 1 zn11 zn22 zmm znNN nm ð2n1 þ n2 þ þ nN =n1 !n2 ! nN !Þ1=2 JN 0; 0; . . . ; 0 n1 ; n 2 ; . . . ; n N n1 ;n2 ;...;nN ¼0 ¼ FN
! ! n ði1 i2 ip Þ o n ði1 i2 ir Þ o qD22 qD2 0; 0; ; 0; z1 ; z2 ; . . . ; zN kj1 j2 jq ; aj1 j2 jr þ 2zm ; qzm qzm ð8:26Þ
where use has been made of Equation 8.9 and the fact that both D11 and D1 are homogeneous polynomials in w1 ; w2 ; . . . ; wN and D12 is a bilinear form containing the variables w1 ; w2 ; . . . ; wN (Equations 8.16, 8.20, and 8.22). From Equations 8.18 and 8.23, N X qD22 qD2 þ 2zm ¼ 2ðamm 1Þzm þ ðamn þ anm Þzn þ am : qzm qzm n¼1 n 6¼ m
ð8:27Þ
Substituting Equation 8.27 into Equation 8.26, utilizing the series expansion (8.25) for FN, and equating terms of the same power in z1 z2 zN , we obtain ðnm þ 1ÞJN
0; . . . ; 0; . . . ; 0 n1 ; . . . ; nm þ 1; . . . ; nN
¼
nm þ 1 2
!1=2
am JN
0; . . . ; 0; . . . ; 0 n1 ; . . . ; nm ; . . . ; nN
0; . . . ; 0; . . . ; 0 n1 ; . . . ; nm 1; . . . ; nN 1=2 1 X 0; . . . ; 0; . . . ; 0 : nn ðnm þ 1Þ ðamn þ anm ÞJN þ n1 ; . . . ; nn 1; . . . ; nN 2 1=2 ðamm 1ÞJN þ nm ðnm þ 1Þ
n¼1
n6¼m
m ¼ 1; 2; . . . ; N
ð8:28Þ
j 8 Multidimensional Franck–Condon Factor
240
For notational convenience, we have suppressed the parametric dependence of JN on the spectroscopic parameters. In a similar manner, by differentiating Equation 8.25 with respect to wm , we obtain the corresponding equation for m1 ; m2 ; . . . ; mN calculating JN , namely, n1 ; n2 ; . . . ; nN ðmm þ1ÞJN
m1 ;...;mm þ1;...;mN n1 ;...;nm ;...;nN
¼
mm þ1 2
1=2 bm JN
m1 ;...;mm ;...;mN n1 ;...;nm ;...;nN
m1 ;...;mm 1;...;mN n1 ;...;nm ;...;nN N 1 X m1 ;...;mn 1;...;mN ½mn ðmm þ1Þ1=2 ðbmn þbnm ÞJN þ n1 ;...;nn ;...;nN 2 n¼1 n 6¼ m N 1X m1 ;...;mn ;...;mN 1=2 þ ½nn ðmm þ1Þ cmn JN ; m ¼ 1;2;...;N: n1 ;...;nn 1;...;nN 2 n¼1
þ½mm ðmm þ1Þ1=2 ðbmm þ1ÞJN
ð8:29Þ
Thus, for each mode m there are two equations, leading to a total of 2N recurrence equations as is appropriate to the 2N occupation numbers (two for each mode). The coefficients amn ; bmn ; and bm appearing in these equations are given explicitly in the Appendix I. Others are given by Equations 8.21 and 8.24 directly. The procedure of applying these equations and the method of computation are exactly the same as 0; 0; . . . ; 0 described earlier in Section 4.4.6. First, the numerical value of JN is 0; 0; . . . ; 0 calculated. According to Equation 8.25, this value is equal to FN ð0; . . . ; 0; 0; . . . ; 0Þ, 0; 0; . . . ; 0 which is defined by Equations 8.11–8.15. Subsequently, the values of JN n1 ; . . . ; nN for a given occupation number set ðn1 ; n2 ; . . . ; nN Þ are calculated by successive use of the N recurrence equation (8.28); that is, the mth equation is employed to raise the occupation number nm. Finally, taking these values as our initial values in Equation 8.29, we proceed in a similar manner as before raising the occupation numbers m1 ; m2 ; . . . ; mN again by successive use of Equation 8.29. This procedure offers a very convenient and efficient method of calculating overlap integrals. The computational advantage lies in the fact that Equations 8.28 and 8.29 are applied separately, allowing the calculation of JN for several or many modes and for high combination states ðm1 ; m2 ; . . . ; mN Þ and ðn1 ; n2 ; . . . ; nN Þ with the Duschinsky effect. The most time-consuming factor in the computation is the calculation of the coefficients of the recursion relations (see, for example, Equations 8.21, I1, and I2). The number of summands in these expressions is on the order of N 1 X i¼1
N1 i
2 :
8.3 Some Numerical Results and Discussion
8.3 Some Numerical Results and Discussion
As an application of the general theory developed in Sections 8.1 and 8.2, we present some FC integral calculations for N ¼ 3 vibrational degrees of freedom and on this m1 ; m2 ; m3 basis, we discuss some properties of J3 from a more fundamental n1 ; n2 ; n3 point of view. To relate them to earlier calculations of the three-dimensional ID, we take the same choice of input parameters for the lower and excited-state potential surfaces and the same parameterization of the orthogonal matrix W by means of the three Euler angles j; q, and y (Section 4.4.7). As already mentioned above, the effect of W is mainly carried in the additional displacement parameters. For N ¼ 3, they are ð123Þ
given by km
ði i Þ
ðm ¼ 1; 2; 3Þ and nine kj1 1ij2 2 ð1 i1 < i2 3; 1 j1 < j2 3Þ interac-
tive displacement parameters. The former (the so-called reciprocal displacement ðmÞ
parameters) are connected with the direct displacement parameters k123 ðm ¼ 1; 2; 3Þ through the inverse transformation kð123Þ ¼ W1 k123 ;
ð8:30Þ
which means that the vector kð123Þ describes the normal mode shifts (or the difference between the geometrical equilibrium positions of the s and l electronic states) in a coordinate system with base vector qsm. (Remember that according to Equation 8.1 the vector k123 describes the same normal mode shifts in a coordinate system with base vectors qlm .) Having all dimensioned displacement parameters and the vibrational frequencies bsm ¼ vms =h and blm ¼ vlm =hðm ¼ 1; 2; 3Þ, we determine from Equations 8.14 and 8.15 the corresponding dimensionless parameters. Next, using all these parameters, we calculate the coefficients in the recurrence equations and the quantities A and B. The latter are given for N ¼ 3 by the more explicit forms ð123Þ2
2
A ¼ D1 ð123Þ þ D2 ð23Þ2
þ D12
ð23Þ2
þ D13
ð123Þ2
þ D3
ð23Þ2
þ D23
ð12Þ2
þ D12 ð1Þ2
ð12Þ2
þ D13 ð2Þ2
ð12Þ2
þ D23
ð13Þ2
þ D12
ð13Þ2
þ D13
ð13Þ2
þ D23
ð3Þ2
þ D123 þ D123 þ D123
ð8:31Þ
and
123 B¼W 123 þW
2
13 12
23 þW 13
2 ða123 123 Þ þ W
2 2
2 ða13 12 Þ þ W
2 ða23 13 Þ þ W
12 12
13 13 23 23
2
2 2
2 ða12 12 Þ þ W
2 ða13 13 Þ þ W
2 ða23 23 Þ þ W
12 13
13 23
2
2
2 ða12 13 Þ þ W
2 ða13 23 Þ þ W
12 23
23 12
2
2
2 ða12 23 Þ
2 ða23 12 Þ
2 2 1 2 1 2 ða3 Þ þ W ða23 Þ2 3 3
j241
j 8 Multidimensional Franck–Condon Factor
242
2 2 2 2 3 1 2 3 3 2 1 2 2 2 þW ða3 Þ þW ða2 Þ þ W ða2 Þ þ W ða32 Þ2 3 2 2 2 2 2 2 1 2 3 þW ða11 Þ2 þ W ða21 Þ2 þ W ða31 Þ2 þ 1: ð8:32Þ 1 1 1
The starting value J3 ð0Þ is then calculated from Equation 8.11. To solve the recurrence equations, one requires the coefficients bmn ; amn; bm ; am , and cmg . These are given explicitly in Appendix I. Figure 8.1 selects some plots arising from such calculations and surveys some of the fundamental consequences arising directly from Duschinsky mode mixing. For comparison with previous calculations of the ID, we take the same choice of input parameters as given in the caption of Figure 4.10. As 0 0 0 there, we plot only J3 for n3 ¼ 10, showing the variation of J3 with the n1 n2 n3 first Euler angle j, whereas the remaining angles q and y are kept constant. Note the extraordinary resemblance in the behavior of both forms of vibrational overlaps as the angle j, which describes the rotation of qs ¼ ðqs1 ; qs2 ; qs3 Þ about the ql3 axis, varies in the interval ð0; 180 Þ. This leads, among other consequences, at approximately j ¼ 30 to a selectivity of J3 distributed in the ðn1 ; n2 Þ plane with strongly attenuated contribution for n1 ¼ 0. If the angle increases further toward j ¼ 120 , the distribution of J3 at n3 ¼ 10 is confined mainly to the n1 axis, with no significant spread into the n2 direction. This happens because in the first case the rotation-dependent ð123Þ ð123Þ component k1 vanishes, as does k2 in the second case. In the second half period 0 0 0 p j 2p, the absolute values of J3 are the same as in the first n1 n2 n3 period but of different phase. The characteristic motion of J3 in the plane ðn1 ; n2 Þ, as we see in Figure 8.1 for the case m1 ¼ m2 ¼ m3 ¼ 0 (zero-temperature limit), is quite general regardless of the manner of occupation of the excited state s. In this lies the predominant effect of mode mixing. The only significant difference is that the relief plots of J3 for the remaining occupation number sets ðm1 ; m2 ; . . . ; mN Þ are more complicated, especially when j ¼ 30 and j ¼ 120 . Of course, the aforementioned motion and therefore selection can be carried to the extreme case of the absence of any observable contribution of two vibrational degrees of freedom. In this case, only quanta of one mode are observed. This occurs when two of the components of the vector kð123Þ vanish simultaneously due to coordinate rotation. This phenomenon is shown in Figure 8.2, where the angles of rotation have ð123Þ ð123Þ ð123Þ ¼ k3 ¼ 0 and k1 6¼ 0. This selects v1 , and no sign of been chosen so that k2 v2 and v3 contribution is seen. The spectroscopic consequences of such mode mixing have been discussed earlier. At certain values of the angles of rotation, such mode mixing leads to the observation of unusually long single progressions instead of a dense manifold of combination lines in absorption or emission spectra. A considerable change in the radiationless decay rate is observed as well. Although there are recognizable similarities to the three-dimensional ID, there are also quite noticeable differences. J3 exhibits rapid oscillations at almost all angles of rotation. Values above and below the ðn1 ; n2 Þ plane then give a strongly broken surface. Precisely, this may give rise to a large increase or decrease of calculated cross
8.3 Some Numerical Results and Discussion
Figure 8.1 A representation of the three 0 0 0 dimensional FC integral J3 at n1 n2 n3 n3 ¼ 10 for a system of electronic surfaces characterized by vs1 ¼ 200; vs2 ¼ 400; vS3 ¼ 900; vl1 ¼ 240; vl2 ¼ 600, and vl3 ¼ 800 cm1 ,
ð1Þ
ð2Þ
displaced from each other by D123 ¼ D123 ¼ 4 ð3Þ and D123 ¼ 1 and whose normal coordinates are rotated by q ¼ 30 ; y ¼ 30, and angle j as indicated. (The vibrational frequencies and the components of the displacement vector are the same as in Figure 4.10).
j243
j 8 Multidimensional Franck–Condon Factor
244
Figure 8.2 Selective properties of 0 0 0 J3 at j ¼ 60 ; q ¼ 30 , and n1 n 2 n3 y ¼ 270 showing the reduction of the threedimensional J3 into a one-dimensional one,
distributed mainly along the n1 axis. ðmÞ The molecular geometry change k123 associated with the transition s ! l is the same as in Figure 4.11a. The set of vibrational frequencies is the same as in Figure 8.1.
sections since they are sensitively dependent upon the phases of the FC integrals. This will now be illustrated for the resonance Raman process in the next section.
8.4 Implementation of Theory and Results 8.4.1 The Resonance Raman Process and Duschinsky Mixing Effect
In this section, we shall discuss two examples to help clarify and illustrate the somewhat formal development in the last two sections. The first is the familiar
8.4 Implementation of Theory and Results
example of the resonance Raman process. As a second example, we shall present a discussion of time-delayed two-photon processes. Both these examples can be used to infer properties of the excited-state and ground-state potential surfaces. On the other hand, the problems are instructive in that the qualitative features are general. The spectroscopy of time-delayed two-photon processes is also of interest in studies of the transition states in chemical reactions. A very thorough survey is given in Refs [290–292]. The scattering intensity of the resonance Raman process that carries the molecule from an initial vibrationless n1 ¼ n2 ¼ 0 to final vibrational state n ¼ ðn1 ; n2 Þ (in the ground electronic state 0) by absorption at frequency n and emission at hn0 ¼ hnnhv0 is given by Refs [219, 293–296]
"
s00 ! n1 n2 ¼ Cs0
m1 X J 2 0 m1 m2
þ
X X J2 m1 m2 m 0 m 0 1 2
m1 0
2 m2 m1 m2 J2 0 0 0 2 2 Em þ Cm1 m2 1 m2
0 0 m2 m1 m2 m1 m20 m1 J2 J2 J2 0 n1 n2 0 0 n1 2 2 2 2 ðEm1 m2 þ Cm1 m2 ÞðEm0 m0 þ Cm0 m0 Þ 1
2
1
m20 n2
2
m6¼m10 m2 6¼m20
ðEm1 m2 Em10 m0 þ Cm1 m2 Cm10 m20 Þ
# ;
ð8:33Þ
where Em1 m2 ¼ DE þ m1 hvs1 þ m2 hvs2
ð8:34Þ
with DE ¼ hVhn being a detuning energy and Cm1 m2 is the damping factor or natural half-width of the resonance states jsm1 m2 i. In writing Equation 8.33, we have taken the resonant part of the tensor s00 ! n1 n2 and restricted ourselves solely to two accepting modes only, with frequencies v1 and v2 . The cross or mixed terms appearing in the double summations of Equation 8.33 represent the interferences between contributions from different homogeneous broadened states jsm1 m2 i
and sm10 m20 . If the particular values of the Raman FC factors m1 m2 m1 m2 J2 become negative for some values m1 and m2 , this may J2 0 0 n1 n2 lead to destructive interferences and therefore to considerable changes in the scattering intensity compared to that resulting from the sum of individual resonances (first term in Equation 8.33). Since the latter and the interferences in the scattering intensity of the resonance Raman process are strongly affected by mode mixing, the cross section as given by Equation 8.33 is very sensitive to the rotation
j245
j 8 Multidimensional Franck–Condon Factor
246
Figure 8.3 Cross section of the resonance Raman scattering for a molecular system of ½Mo2 Cl8 4 with two accepting modes of frequencies vs1 ¼ 300; vs2 ¼ 250; v01 ¼ 350, and v02 ¼ 275 cm1 . The normal mode displacements have been chosen as
hÞ1=2 and k12 ¼ ð 0:2; 0:1 Þ in units of ðMm 2pc= the normal coordinate rotation is given by the angle j. The Lorentzian linewidth is fixed at C ¼ 100 cm1 for all resonant states and the detuning energy is DE ¼ 500 cm1 .
angle j. This is illustrated in Figure 8.3, where the cross sections for the first neighboring vibrational levels of the ground electronic state are shown. For the curves in Figure 8.3 we have based the calculations on the resonance Raman spectrum of the metal–metal bonded species ½Mo2 Cl8 4 with D4h symmetry taking the two totally symmetric fundamentals of ½Mo2 Cl8 4 , having frequencies of v01 ¼ 346 cm1 and v02 ¼ 277 cm1 [294]. In this complex, the eight halogen ions bonded to the two metal ions are situated nearly at the corners of a cube. v1 is the Mo–Mo stretching frequency and v2 is the Mo–Cl stretching frequency, both modes possessing ag symmetry. The bandwidths Cm1 m2 have been chosen constant and smaller than the vibrational interval ðC hvÞ. We see that if the parallel mode approximation breaks down, the resonance Raman cross section is strongly j dependent, where j describes the rotation of the two normal coordinates in the resonance electronic state jsi relative to the ground electronic state j0i. The cross section decreases rapidly in some region of j by many orders of magnitude. Thus, some vibrational modes may be seen only weakly in the ðmÞ Raman spectrum even though they have significant excited-state displacements k12 and frequency shifts. Others, however, are greatly intensified by the Duschinsky effect of mode mixing. They do this at the cost of the former vibrational modes. This effect,
8.4 Implementation of Theory and Results
together with other mechanisms (anharmonicity) that may influence the relative intensities in the resonance Raman spectrum, makes it generally difficult to estimate the excited-state distortion or displacement [219] from the intensity distribution of the resonance Raman spectrum. By comparing the curves for s00 ! 01 and s00 ! 10 with that for s00 ! 11, we see that the interference term in Equation 8.33 oscillates for the process 0; 0 ! 1; 1 twice as fast than for the former as the angle j varies in the interval ð0; pÞ. The curves for scattering to overtones 0; 0 ! n1 ; 0 or 0; 0 ! 0; n2 and to higher combination states 0; 0 ! n1 ; n2 exhibit a qualitatively similar behavior. The maxima are higher and the valleys are not as deep as for the curves shown in Figure 8.3. The position of the valley for the process 0; 0 ! n1 ; 0ð0; 0 ! 0; n2 Þ, and the positions of the valleys for the process 0; 0 ! n1 ; n2 appear again at 70 and 160 as in the case of the lowest combination state. As pointed out by Tannor and Heller [296], the Kramers–Heisenberg–Dirac (KHD) sum-over-state method that we have applied for two modes to demonstrate the Duschinsky mixing effect on the resonance Raman process becomes intractable if the number of modes, and the intermediate states in the sum (8.33) goes up. These authors, using the wave packet formulation of Raman scattering of Lee and Heller [295, 297], derived an expression for the Raman amplitude a ða2 ¼ sÞ in terms of a half-Fourier transform. This method avoids the summing over intermediate states fmm g by direct numerical evaluation of the Fourier transform. It is much faster for the case of scattering to fundamentals, overtones, and low combination final states. The last conclusion changes drastically if high resolution is desired. The computation time of the time-dependent method is then comparable with that of the KHD sumover-state method. For a detailed discussion the reader is referred to Ref. [296]. 8.4.2 Time-Delayed Two-Photon Processes: Duschinsky Mixing Effects
The study of the sequential two-photon process discussed in this section rests on a time-dependent formulation of photon absorption given by Cribb and Brickmann [298]. For this purpose, let us work following Figure 8.4, representing a cut through two-dimensional potential energy surfaces of a ground electronic state and intermediate and upper excited electronic states. At time t ¼ 0, the absorption of a photon has caused the initial ground-state vibrational wavefunction to be prepared on the intermediate states potential energy surface at position d, where the displacement vector d is now related to the normal coordinates of the dissociative excited state qd ¼ ðqd1 ; qd2 Þ qd ¼ Wqg þ d;
ð8:35Þ
qg ¼ W1 ðqd dÞ;
ð8:36Þ
or
g
g
where qg ¼ ðq1 ; q2 Þ are the normal coordinates of the ground electronic state. The dissociative state is modeled by a quasi-continuum; that is, a harmonic
j247
j 8 Multidimensional Franck–Condon Factor
248
hν2
hν1
Figure 8.4 Schematic illustration of a sequential two-photon process involving a dissociative intermediate electronic state and a bound excited state.
oscillator with very low frequency vd2 along the mode qd2 . Since the wavefunction is not an eigenfunction of the excited-state Hamiltonian, it becomes a moving wave packet on the upper surface. The temporal evolution of the system or the propagated semiclassical wave packet [299, 300] is written on the basis of eigenstates xdn ðqd Þ as yðqd ; tÞ ¼
X n
cn eiEn t=h xdn ðqd Þ;
ð8:37Þ
where xdn ðqd Þ ¼ xdn1 ðqd1 Þxdn2 ðqd2 Þ;
ð8:38Þ
cn ¼ ðxdn ðqd Þ yðqd ; 0ÞÞ
ð8:39Þ
and
8.4 Implementation of Theory and Results
represent the wave packet amplitude.2) Here, xdnm ðqdm Þðm ¼ 1; 2Þ are harmonic oscillator eigenstates for the two coordinates of the dissociative surface (one with very low frequency) and g
g
xg0 ðqg ; 0Þ ¼ xg01 ðq1 Þxg02 ðq2 Þ;
ð8:40Þ
g
where xg0m ðqm Þðm ¼ 1; 2Þ are the zeroth eigenstates of the ground electronic surface. En in Equation 8.37 represents the energy of the system in the state d. The time evolution is determined by the shape of the potential U of the dissociative state and the position of the wave packet at t ¼ 0. Node development is dominated by forces qU=qqd . Spreading of the wave packet is governed by the second derivatives 2 q2 U=qqd . The normal coordinates are rotated, so that although the center of the wave packet ðhq1 i; hq2 iÞ follows the classical equation of motion, the wave packet also appears to rotate as it evolves. The overall motion and spreading go on until the second photon interaction. This second photon excitation event causes a transition to the mth vibrational state of the excited (bound) electronic state, the probability of which is proportional to
2 e d Pm ðtÞ / xem ðq Þ yðq ; tÞ ; ð8:41Þ where
X iEn t=h cn e xem1 ðqe1 Þxem2 ðqe2 Þ xdn1 ðqd1 Þxdn2 ðqd2 Þ xem ðqe Þ yðqd ; tÞ ¼ n
¼
X
cn eiEn t=h J2
n
m1 n1
m2 n2
ð8:42Þ
Note that both xem1 xem2 Þ and xdn1 xdn2 Þ are only product states when different coordinate systems are used. These systems are related by equation like that of (8.36), with
k
cosje W1 ¼ sinje
k
sinje : cosje
ð8:43Þ
8.4.3 Results
We begin our discussion with the results of some numerical calculations [298]. The g respective frequencies vm and vem ðm ¼ 1; 2Þ of the ground and excited states, as well as the displacements dg and de of these states from the origin of the dissociative oscillator, are varied. For convenience, the frequencies are measured in multiples of vd2 , the distances in multiples of ðvd2 =hÞ1=2 , the time in multiples of ðvd2 Þ1 , and the energies in multiples of hvd2 . The corresponding dimensionless numbers are marked by a tilde. 2) We shall not concern ourselves here with the field coupling.
j249
j 8 Multidimensional Franck–Condon Factor
250
Figure 8.5 Two-photon Franck–Condon transition probability spectra for the system of ~ g ¼ ð6:0; 8:0Þ; electronic surfaces with (a) v ~ d ¼ ð5:0; 1:0Þ, d~g ¼ ð0:5; 6:0Þ; jg ¼ 45 , v ~ e ¼ ð4:0; 6:0Þ, d~e ¼ ð0:21; 5:53Þ, and with the v rotation angle je taking the values as indicated. The spectra are all at the delay time ~t ¼ 0:4 when
the position expectation value of the wave packet is located at the minimum of the excited electronic surface. After Ref. [298]. (b) As for ~ g ¼ ð6:0; 8:0Þ; d~g ¼ ð1:0; 8:0Þ; (a) except v ~ d ¼ ð5:0; 1:0Þ; v ~ e ¼ ð4:0; 6:0Þ, jg ¼ 45 ; v and d~e ¼ ð0:42; 7:37Þ.
In the first case (Figure 8.5a), the frequencies of the electronic surfaces are ~ g ¼ ð6:0; 8:0Þ; v ~ d ¼ ð5:0; 1:0Þ; v ~ e ¼ ð4:0; 6:0Þ v
8.4 Implementation of Theory and Results
Figure 8.5 (Continued)
and the positions (relative to the origin of the dissociative surface) are ~dg ¼ ð0:5; 6:0Þ; ~de ¼ ð0:21; 5:53Þ:
dg and ~ At ~t ¼ 0 the position of the wave packet is ~q1 ; ~q2 ¼ ~ de is chosen such ~ that at t ¼ 0:4 the wave packet is located in the minimum of the excited state ~q1 ; ~q2 ¼ ~de . The ground-state electronic surface is rotated by jg ¼ 45 with respect to the dissociative surface. In Figure 8.5a, we examine the effect of rotating the excited surface by je on the two-photon transition probability at a delay time of
j251
j 8 Multidimensional Franck–Condon Factor
252
~t ¼ 0:4. On examining Figure 8.5a, we see that at je ¼ 40 the transition probability spectrum PðtÞ manifests sharp peaks at energies corresponding to the eigenstates j0; 0i; j0; 1i, and j0; 2i (i.e., at 5.0, 11.0, and 17.0 energy units). Conversely, the transition probabilities to the j1; 0i; j2; 0i; j1; 1i, and j2; 1i levels (energies 9.0, 13.0, 15.0, and 19.0 units, respectively) are at a minimum. Upon further rotation, the spectrum changes quite dramatically until at je ¼ 120 , and the sequence of maxima and minima has shifted so that the transition to j0; 0i; j1; 0i, and j2; 0i levels is the largest and the transition to the j0; 1i level is very small. Before interpreting this, examine Figure 8.5b. Here, the frequencies of the electronic surfaces are the same as in Figure 8.5a, but the position of the ground electronic state, that is, of the wave packet at ~t ¼ 0 on the dissociative surface, is ~dg ¼ ð1:0; 8:0Þ. The location of the excited surface is ~ de ¼ð0:42; which
7:37Þ,
means that at ~t ¼ 0:4 the position of the wave packet is ~q1 ; ~q2 ¼ ~ de . The ground-state surface is rotated by jg ¼ 45 and the figure shows the transition probabilities at ~t ¼ 0:4 as the excited-state surface is rotated. Qualitatively, we see a development similar to that in Figure 8.5a. Certain transition probabilities reach a maximum at certain values of je ðje ¼ 60 Þ, and these decrease while another set grows to become maximum at another angle of rotation je ðje ¼ 140 Þ. At je ¼ 60 , the peaks correspond to transitions to the levels j0; 1i; j0; 2i; j0; 3i, and j0; 4i, while at je ¼ 140 they correspond to the levels j1; 0i; j2; 0i; j3; 0i; j4; 0i; j5; 0i, and j6; 0i. Thus, qualitatively, at certain angles (je ¼ 60 ) the progression in v2 ¼ 6:0 units dominates, whereas at je ¼ 140 the spectrum consists mainly of a single progression in v1 ¼ 4:0 units. These angles correspond to the parallel alignment of the normal modes of the excited-state surface with the axes of the propagated state. The difference between Figure 8.5a and b – that is, the fact that the largest transition probabilities are to levels about 20.0 units in Figure 8.5b, but only at 10.0 units in Figure 8.5a – is due only to the different momentum of the wave packet in the two cases. The frequencies of the surfaces are the same and the displacements of the propagated wave packet from the excited-state surface are the same ð ð0:0; 0:0ÞÞ. Therefore, these can have no effect. In Figure 8.5b, the wave packet has a larger momentum than in Figure 8.5a, and this results in a shift to higher energies in the transition spectrum. In Figure 8.6, the dependence of the spectrum on the delay time ~t between the two photons is investigated. The electronic surfaces are characterized by ~ g ¼ ð6:0; 8:0Þ; v ~ d ¼ ð5:1; 1:0Þ; v ~ e ¼ ð4:0; 6:0Þ; v
~dg ¼ ð1:0; 8:0Þ;
jg ¼ 45 ;
~de ¼ ð0:42; 7:37Þ;
je ¼ 60 :
Note that in Figure 8.6 the rotation angle je is that that results in the mode ~ e2 ð¼ 60 Þ at ~t ¼ 0:4 and also that the excited state is located on the progression in v wave packet trajectory so that h~ qi ¼ ~de at ~t ¼ 0:4. Up until ~t ¼ 0:4, there is a very clear e ~ 2 ¼ 6:0 units. These are all j0; m2 i levels of the excited state. After progression in v ~t ¼ 0:4, there is a region of no unique progression until ~t ¼ 0:8, when there is a ~ e1 ¼ 4:0 mode. This switch in the mode of the progression clearly switch to the v
8.4 Implementation of Theory and Results
Figure 8.6 Dependence of the two-photon Franck–Condon transition probability spectra on the delay time for the system of electronic
~ g ¼ ð6:0; 8:0Þ; d~g ¼ ð1:0; 8:0Þ; surfaces with v ~ d ¼ ð5:0; 1:0Þ; v ~ e ¼ ð4:0; 6:0Þ; jg ¼ 45 ; v d~e ¼ ð0:42; 7:37Þ; je ¼ 60 .
indicates that the effect of rotated normal modes has been to couple the degrees of freedom. Consequently, the wave packet acquires some effective rotational motion in addition to the classical evolution of position and momentum [298]. This can be clearly seen in Figure 8.7, where the real part of the wave packet is shown. Here, at ~t ¼ 0 the wave packet is simply the ground vibrational state of the electronic surface
j253
j 8 Multidimensional Franck–Condon Factor
254
Figure 8.7 The dependence of the real part of the wave packet yðq; tÞ, that is, ReðyÞ, on time for the system in Figure 8.6. Thus, the initial state is the ground vibrational state of the harmonic surface with frequencies ~ g ¼ ð6:0; 8:0Þ placed at d~g ¼ ð1:0; 8:0Þ in the v
coordinate system of the dissociative electronic surface and rotated by jg ¼ 45 with respect to those coordinates. The evolution times and the corresponding position expectation values of the normal modes are indicated. After Ref. [298].
~ g ¼ ð6:0; 8:0Þ placed at ~dg ¼ ð1:0; 8:0Þ and rotated by jg ¼ 45 relative to with v the axes of the dissociative surface. At subsequent times, as nodes develop due to the increasing momentum, the rotation becomes quite evident from the orientation of the peaks and valleys. At ~t ¼ 0:4, we have the case examined in Figure 8.5b, where the
8.5 The One-Dimensional Franck–Condon Factor (N ¼ 1)
critical angles for the excited state (leading to the most well-defined mode progressions) were je ¼ 60 and 140 . This corresponds to the alignment of the normal modes in the excited state with the orientation of the wave packet. At ~t ¼ 0:6, the wave packet has refocused in the q1 coordinate and displays only nodes in the q2 -coordinate oriented parallel to the normal modes of the dissociative surface. Examining Figure 8.6 again with the benefit of Figure 8.7, it can be seen that with the excited electronic surface rotated by je ¼ 60, the normal modes of that surface are at ~t ¼ 0:4 aligned almost parallel to the axes of the wave packet. Indeed, for times ~t ¼ 0 to about 0.5, the same mode of the excited surface must be in fairly close alignment with the wave packet axis. By ~t ¼ 0:8, however, the wave packet orientation is becoming almost perpendicular to what it was at ~t ¼ 0:4, so that the other mode of the excited electronic surface is now aligned with the wave packet axis. This must account for the switch in the mode of progression seen in Figure 8.6. (For the calculation of the position expectation valuesðh~q1 i; h~q2 iÞ indicated in Figure 8.7, see Appendix J). To close this section, we note that (i) if the excited state is displaced sufficiently from the ground electronic state, then at short delay times the shape of the transition probability will reach a maximum at relatively high energies. As the delay time increases, this shape will move to lower energies (provided that the intermediate state moves toward the minimum of the excited electronic surface), and at still longer delay times it moves back out to higher energies and eventually smears out. This behavior is quite general regardless of the relative rotations of the electronic surfaces. (ii) The line shape function obtained from delayed two-photon processes bears some resemblance to the behavior of the multidimensional intramolecular distribution noted in Section 4.3.3, which can be reduced to an effectively 1D or 2D distribution at certain critical rotation angles.
8.5 The One-Dimensional Franck–Condon Factor (N ¼ 1)
To complete this chapter, we finally consider the simple case N ¼ 1. To do this, it is necessary to go back to the definition of the generating function given by Equation 8.25. We have J1
m D ; b m m ¼ n
qm þ n F1 ðw; zÞ w¼0 ; ð2m þ n m!n!Þ1=2 qw m qzn 1
ð8:44Þ
z¼0
where the one-dimensional generating function F1 is now given by (Equation 8.9) F1 ðw; zÞ ¼ F1 ð0; 0Þexp½D11 þ D22 þ D12 þ D1 þ D2 þ w 2 z2 ;
ð8:45Þ
with D11 ¼ 2
bsm bsm
þ blm
w 2 2w 2 ¼ 2
bm 1 þ bm
w 2 2w 2 ;
ð8:46aÞ
j255
j 8 Multidimensional Franck–Condon Factor
256
D22 ¼ 2
D12 ¼ 4
blm bsm þ blm
z2 ¼
ðbsm blm Þ1=2
D1 ¼ 2
bsm þ blm
2z2 ; 1 þ bm
wz ¼
ðbsm Þ3=2 km bsm þ blm
4b1=2 m 1 þ bm
ð8:46bÞ
wz;
ð8:46cÞ
2bsm km 1=2
w þ 2ðbsm Þ1=2 km w ¼
1 þ bm
w;
ð8:46dÞ
and ðblm bsm Þ1=2 bsm km 1=2
D2 ¼ 2
bsm þ blm
s b1=2 m bm km 1=2
z ¼ 2
1 þ bm
z;
ð8:46eÞ
which follows from the detailed expressions (8.10) for N ¼ 1. In Equation 8.46, we m have set bm ¼ ðam Þ2 ¼ ðbsm =blm Þ (Equation 8.15). Similarly, from Equations 8.11–8.13, we have
F1 ð0; 0Þ ¼ 21=2 b1=4 m
h i bs k2 exp 12 1 þm bm m
ð1 þ bm Þ1=2
a
m ; ¼ ð1b2m Þ1=4 exp 2
ð8:47Þ
where am ¼ bsm k2m =ð1 þ bm Þ ¼ D2m =ð1 þ bm Þ. On substituting (8.46) into (8.45), we obtain ~ þ Bz ~ þ Cwz: F1 ðw; z; Dm ; bm Þ ¼ F1 ð0; 0Þexp½bm ðw 2 z2 Þ þ Aw
ð8:48Þ
In this expression, ~ ¼ 2Dm ¼ Dm ð1 þ bm Þ; A 1 þ bm C¼
4b1=2 m 1 þ bm
¼
2ð1b2m Þ1=2 ;
~ ¼ 2 B
b1=2 m Dm 1 þ bm
1bm bm ¼ : 1 þ bm
¼ Dm ð1b2m Þ1=2 ; ð8:49Þ
Note that an alternative way of writing Equation 8.49 has already been used in Equation 4.45. To calculate the derivatives of F1 , we write F1 ¼ G H for convenience, where G ¼ exp½bm ðw 2 z2 Þ;
ð8:50aÞ
and ~ þ Bz ~ þ CzÞw ¼ expðAwÞexp½ð ~ ~ þ Cwz ¼ expðBzÞexp½ð ~ ~ þ CwÞz: H ¼ exp½Aw A B ð8:50bÞ
8.5 The One-Dimensional Franck–Condon Factor (N ¼ 1)
Then the derivatives of F1 are i mi m qm Gðw; zÞHðw; zÞ X m q Gq H ¼ ; i qw i qw mi qw m i¼0
and iþr X n X m mi þ nr qn qm G H H n m q Gq ¼ : n m i r mi qznr r i qw qw qw qz qz r¼0 i¼0
ð8:51Þ
Now observing that ðqi þ r G=qwi qzr Þo ¼ 0 if i or r or both i and r are odd numbers, we see that q2r þ 2i G ð2iÞ!ð2rÞ! ¼ ð1Þi bimþ r : ð8:52Þ qw 2i qz2r w¼0 i!r! z¼0
With little bookkeeping for a b, we obtain b X qa þ b Hðw; zÞ Cðc þ b þ 1Þ ~ c þ lB ~ l Cbl ; ¼ b! A a b Cðc þ l þ 1Þl!ðblÞ! qw qz l¼0
ð8:53Þ
where C is the Eulers gamma function and c ¼ ab. To simplify this further, we set ~ B=C ~ A ¼ am in Equation 8.53. This gives us qa þ b Hðw; zÞ ~ ab C b b!Lab ðam Þ: ¼A ð8:54Þ b qw a qzb w¼0 z¼0
The last step follows directly from employment of definition (4.43). Substituting Equations 8.52 and 8.54 into Equation 8.51 and remembering that F1 ðw; zÞ ¼ F1 ð0; 0ÞG H, the general form (8.44) then becomes J1
1=4 1 m!n! 1=2 m ; am ; bm ¼ 1b2m exp am n 2 2m þ n 2 3 ½m=2 X X ½n=2 ð1Þi bimþ r mn2ðirÞ n2r mn2ðirÞ ~ ðn2rÞ!A 4 C Ln2r ðam Þ5: ðm2iÞ!i!ðn2rÞ!r! i¼0 r¼0 ð8:55aÞ
It is perhaps worth remembering that Equation 8.55a is obtained under the assumption that in Equation 8.54, a b. This implies that now m n and m2i n2r. If the last inequality is not satisfied for one or finitely limited values of i, then differentiation in (8.54) should be performed in reverse order, that is, first in respect to z and subsequently in respect to w. This leads to an expression for J1 similar to that of Equation 8.55a, but with the factor mn2ðirÞ
~ ðn2rÞ!A Cn2r Ln2r ðam Þ in Equation 8:55a replaced by ~ mn2ðriÞ Cm2i Lnm2ðriÞ ðam Þ: ðm2iÞ!B m2i mn2ðirÞ
ð8:56Þ
j257
j 8 Multidimensional Franck–Condon Factor
258
Analogously, if m n, then J1
1=4 1 m!n! 1=2 m ; am ; bm ¼ 1b2m exp am n 2 2m þ n 2 3 ½m=2 X ½n=2 X ð1Þi bimþ r nm2ðriÞ m2i nm2ðriÞ ~ ðm2iÞ!B 4 C Lm2i ðam Þ5; ðm2iÞ!i!ðn2rÞ!r! i¼0 r¼0 ð8:56bÞ
provided that n2r m2i holds for all nonnegative integers i and r. Otherwise, perform an exchange of the appropriate factors appearing in (8.55b) according to (8.56) but in the reverse order. When bm ¼ 1, the case with no frequency change, we have bm ¼ 0 and Equation 8.55a reduces to [301] ! 1=2 mn D2m Dm n! 1 2 m mn pffiffiffi ;D ;0 ¼ : ð8:57aÞ J1 exp Dm Ln n m 2 m! 4 2 If n > m, then J1
! 1=2 2 Dm nm nm Dm m! 1 2 m p ffiffi ffi ; ;D ;0 ¼ exp Dm Lm n m 2 n! 4 2
where Dm ¼ bsm 1=2 km (see Equation 8.14c).
ð8:57bÞ
j259
Appendices
j261
Appendix A: Some Identities Related to Greens Function
A.1 The Greens Function Technique
To calculate the transition probability, we need to know the energy dependence of the resolvent operator or Greens function in a manifold of states or in the representation appropriate to a set of wavefunctions of the zero-order Hamiltonian H0 jsi ¼ Es jsi;
ðA1Þ
where the behavior of the states jsi depends on the type of problem to be studied. The resolvent of the operator H ¼ H0 þ V (which we imagine to be decomposed into an unperturbed part H0 and a perturbation V) is given by the object GðzÞ ¼
1 ; zH
ðA2Þ
considered as a function of the complex variable z. It is a bound operator in the Hilbert space1 for every value of the variable z except at the eigenvalues of H. When the eigenvalues of H are discrete, Hjai ¼ Ea jai, the singularities of Ga ¼ hajGðEÞjai are poles on the E-axis at the position of these eigenvalues. Then Ga is analytic everywhere in the complex E-plane, except the poles on the real E-axis. When H has a continuum spectrum of eigenvalues, Hjli ¼ El jli, the situation is quite different. Here, let us suppose that the eigenvalues El of H are continuous over the range EM < E < 1. Then, Ga ðEÞ is analytic everywhere in the complex E-plane, except along the cut extending from EM to plus infinity on the real axis. This is illustrated in Figure A.1. The Greens operator is thus defined as limit of the resolvent when z approaches to real axis: G ðEÞ ¼ limþ e!0
1 : EH ie
ðA3Þ
The quantity e is a very small (and positive) number that determines the position of the poles of GðEÞ with respect to the real axis, but which we always take to zero in the 1 That is, jj Gg jj M jj g jj for all vectors g belonging to the Hilbert space. Here jj g jj ¼ ðg; gÞ1=2 is the norm of g and M is a constant.
j Appendix A: Some Identities Related to Greens Function
262
ε
z-plane
EM Single poles of G(z)
E
Branch cut of G(z)
Figure A.1 Analytic behavior of GðzÞ ¼ ðzHÞ1 . The singular points or lines are on the real z-axis (when H is Hermitian) and provide information about the eigenvalues and eigenfunctions of H.
end. These conclusions concerning the domain of analyticity of Ga ðEÞ are important and provide a very useful basis for discussing decay phenomena. Let us now suppose the state jsi to be represented by the approximate Hamiltonian H0 of Equation A1. If, for example, the state jsi and another state jbi of the manifold (A1) between the transitions are isolated from the remaining states of H0 , the problem is relatively simple. However, if the states are not isolated, the calculation of the transition probability is not simple. To reduce the complexity and to make clear the states of the system to be included in the calculation of the matrix elements of the Greens function, we use the Feshbach projection operator formalism. In this formalism, a projection operator associated with a model function or a set of states, the so-called close coupled states, is introduced X P¼ jsihsj; ðA4Þ s
where the sum over s depends on the problem to be considered. Since P is a projection operator, it is such that P 2 ¼ P:
ðA5Þ
Let us now introduce a second operator defined by the relation Q ¼ 1P
ðA6Þ
for the complementary part of the functional space spanned by P and which we can call the Q space. Q is also a projection operator, since Q 2 ¼ ð1PÞ2 ¼ I2P þ P 2 ¼ IP ¼ Q:
ðA7Þ
From Equations A5 and A7, we also deduce that the operators P and Q are orthogonal, so Q P ¼ P Q ¼ 0:
ðA8Þ
In the language of these projection operators, it is clear that for the calculations of the above-mentioned matrix elements, we need to know the projections of the Greens function QGP and PGP. The first projection gives us the matrix element of G
Appendix A
between a state outside the set of states and a state inside the set of states, which we wish to treat on an equal basis. The second projection operator connects states that we treat on an equal footing. To derive the above projections of G, we start with the identity (see Equation A2) ðEHÞGðEÞ ¼ 1:
ðA9Þ
Multiplying this identity from the right by P and introducing in (A9) the relation P þ Q ¼ 1, we get ðEHÞPGðEÞP þ ðEHÞQGðEÞP ¼ P
ðA10Þ
and then taking the left projection of this equation onto first P and then Q, we have PðEHÞPðPGPÞPHQðQGPÞ ¼ P;
ðA11aÞ
QHPðPGPÞ þ QðEHÞQðQGPÞ ¼ 0:
ðA11bÞ
Here we have introduced the identities P2 ¼ P and Q 2 ¼ Q. Assuming that the operator QðEHÞQ possesses an inverse in the space spanned by Q, Equations A11a and A11b may be formally decoupled by first solving (A11b) for QGP, QGP ¼ ðEQHQÞ1 QHPðPGPÞ;
ðA12Þ
and inserting this result into Equation A11a, so that ½ðEPHPÞPHQðEQHQÞ1 QHPPGP ¼ P:
ðA13Þ
Equation A13 may be rewritten as ½EPH0 PPRPPGP ¼ P;
ðA14aÞ
PGP ¼ ½EPH0 PPRP1 P;
ðA14bÞ
or
for the time evolution of P states. The operator R introduced in Equations A14 is the so-called level shift operator given by [80,81] R ¼ V þ VQðEQHQÞ1 QV;
ðA15Þ
which is of real interest. The operator has complex diagonal matrix elements, the imaginary parts of which are of prime interest to nonradiative decay processes and will play an important role in our consideration. Similarly, from Equation A12, we have for the time evolution of the P ! Q excitation QGðEÞP ¼ ðEQHQÞ1 QHPðEPH0 PPRPÞ1 :
ðA16aÞ
Equation A16a may be written in a more convenient form (for calculating transition probabilities) as QGðEÞP ¼ ðEQH0 QÞ1 QRðEÞPðEPH0 PPRPÞ1 :
ðA16bÞ
j263
j Appendix A: Some Identities Related to Greens Function
264
This can be verified by using the relationship ðEQH0 QÞ1 QRP ¼ ðEQHQÞ1 QVP ¼ ðEQHQÞ1 QHP;
ðA17Þ
which follows from the definition of R, QRP ¼ QVP þ QVQðEOHQÞ1 QVP ¼ ðEQH0 QÞðEQHQÞ1 QVP: ðA18Þ
It is interesting to note that the operator appearing in Equations A14 and A16, Heff ¼ PH0 P þ PRP;
ðA19Þ
is the effective Hamiltonian for the states of P. A.2 Evaluation of the Diagonal Matrix Element of Gss
To understand how the result (6.24) and (6.25) is achieved, we turn to the derivation of the last term appearing in Equation 6.21 for a system, as was the case in Section 2.1: D
E ys ðEPH0 PPRðEÞPÞ1 ys ¼
1 s Rss ; EE
ðA20Þ
where Rss is understood that R is to operate on the state ys . It is easy to see that Rss satisfies the equation X X ~ ll0 Vl0 s þ ~ k^e;k0^e0 Wk0^e0 ;s ¼ RI þ RII ; Rss ðEÞ ¼ Vsl G Ws;k^e G ðA21Þ ss ss l;l0
k;^e
with ~ ¼ ðEQHQÞ1 : G
ðA22Þ
Making use of the Dyson equation, we have ~ ~ ¼ ðEQHQÞ1 ¼ ðEH0 QVQÞ1 ¼ G0 þ G0 QVQ G; G
ðA23Þ
where G0 ¼ ðEH0 Þ1 ;
and the interaction responsible for the transition ys ! yl ; y0;k;^e is V ¼ Hv þ Hint . Let us first consider the first term of (A21). For this case, we write ~ ll0 ¼ G
X dll0 1 ~ k^e;l0 þ Wl;k^e G EEl þ ie EEl þ ie k;^e
ðA24aÞ
and ~ k^e;l0 ¼ G
1 ~ ll0 ; Wk^e;l G EEk^e þ ie
ðA24bÞ
Appendix A
j265
where we have shifted the pole of GðEÞ below the real E-axis by an infinitesimal positive quantity e. Substituting (A24b) into (A24a) gives ~ ll0 ¼ G
X dll0 1 1 ~ ll0 þ Wl;k^e Wk^e;l G EEl þ ie EEl þ ie k;^e EEk^e þ ie
and after little manipulation dll0
~ ll0 ¼ G
EEl þ ie
2 ; P Wl;k^e k^e EEk^e þ ie
ðA25Þ
where Ek^e ¼ E0 þ kc. Going back to the first term in (A21) and letting e ! 0 þ , the expression for RIss as a function of E becomes " # X X X Wl;k^e 2 2 I ¼ Rss ðEÞ ¼ jVsl j = EEl jVsl j2 =½EEl Dl þ iCl ðEÞ=2; EE k^e l k;^e l ðA26aÞ
or RIss ðEÞ ¼
X l
lÞ iX i jVsl j2 ðEE jVsl j2 Cl ðEÞ I 2 2 2 2 ¼ Ds 2 Ds ðEÞ; 2 ðEE l Þ þ ½Cl ðEÞ=2 ðEE l Þ þ ½Cl ðEÞ=2 l
ðA26bÞ
where Re RIss ¼ DIs ðEÞ and Im RIss ðEÞ ¼ ð1=2ÞDs ðEÞ [81]. In Equation A26b, the l ¼ El þ Dl . In deriving RI , we have tacitly level shift term Dl has been included in E ss assumed that the states yl have been allowed to have very small widths Cl due to highly forbidden radiative transition to the ground state y0 . In practice, the width Cl may be modified from intermolecular perturbation with the medium. The radiation matter interaction Hint of the molecule with the radiation field is weak in the sense that the virtual transition involving the emission of photons contribute very little to the decay rate. This means that we may evaluate the matrix II element RII ss in lowest order perturbation theory, to give Rss ¼ iCs =2, where X Xð Ws;k^e 2 dðEs E0 kcÞ ¼ 2p Ws;k^e 2 d r ðkcÞ; Cs ¼ 2p ðA27Þ ph ^e
^e
Es E0 ¼ hns0 kc;
ðA28Þ
is the energy of the emitted photon and d rph ðkcÞ ¼
k2 ð2pÞ3 c
VdVk
ðA29Þ
is the number of photon states of a given polarization in the volume V per unit energy directed into the solid angle dVk . The real level shift DII s gives exceedingly small
j Appendix A: Some Identities Related to Greens Function
266
contribution to the energy Es and may ordinarily be neglected [81]. This permits us to adopt Equation A20 to Equation A.12, which is equivalent to Gs ðEÞ ¼
1 s þ iðDs þ Cs Þ=2 ; EE
ðA30Þ
where the real parts of Re Rss ¼ DIs þ DII s have been absorbed in the term s ¼ Es þ DI þ DII . In this case, Gs ðEÞ is analytic everywhere in the complex EE s s plane, except the pole (poles) on the half plane of complex E. The question of the number of poles depends on whether Ds ðEÞ þ Cs ðEÞ (which itself is a function of E) is a smooth function of E or not.
j267
Appendix B: The Coefficients of the Recurrence ð1Þ ! ð2Þ m1 ; m2 D12 D12 b1 b2 Equation for I2 ; n1 ; n2 Dð12Þ Dð12Þ b12 b21 1
2
The expressions of coefficients of the recurrence Equations 4.50, 4.51, 4.54 and 4.55 may be obtained in a straightforward manner by expansion of the functions (4.47) through (4.49). We begin with the function 1)
B21 B2 Defining a0 pq;rs ¼
X
am1 m2 ;n1 n2 bm0 1 m0 2 ;n0 1 n0 2 ;
p; q; r; s ¼ 0; 1; 2;
ðB1Þ
m1 þ m0 1 ¼p m2 þ m0 2 ¼q n1 þ n0 1 ¼r n2 þ n0 2 ¼s
we may obtain the coefficients cij;kl in the expansion of B21 B2 by summing X cij;kl ¼ a0 m1 m2 ;n1 n2 am0 1 m0 2 ;n0 1 n0 2 ; i; j; k; l ¼ 0; 1; 2; 3: ðB2Þ m1 þ m0 1 ¼i m2 þ m0 2 ¼j n1 þ n0 1 ¼k n2 þ n0 2 ¼l
2)
B1 ðq=qw1 ÞðB1 B2 Þ Substituting Equations 3.33 and 3.34 and the expansion of Equation 4.47 to the identity B1
q q qB1 ðB1 B2 Þ ¼ ðB2 B2 ÞB1 B2 qw1 qw1 1 qw1
and differentiating, rearranging, and comparing terms of the same powers in w1 w2 z1 z2 , we obtain X ð1Þ gij;kl ¼ ði þ 1Þci þ 1;j;kl a0 i m2 ;n1 n2 a1m0 2 ;n0 1 n0 2 ; i ¼ 0; 1; 2; ðB3Þ m2 þ m0 2 ¼j n1 þ n0 1 ¼k n2 þ n0 2 ¼l
j Appendix B: The Coefficients of the Recurrence Equation
268
or written explicitly ð1Þ
g0j;kl ¼ c1j;kl
X m;n
ð1Þ
g1j;kl ¼ 2c2j;kl ð1Þ
g2j;kl ¼ 3c3j;kl
a0 0m2 ;n1 n2 a1m0 2 ;n0 1 n0 2 ;
X m;n
X m;n
ðB3aÞ
a0 1m2 ;n1 n2 a1m0 2 ;n0 1 n0 2 ;
ðB3bÞ
a0 2m2 ;n1 n2 a1m0 2 ;n0 1 n0 2 ¼ 2c3j;kl ;
ðB3cÞ
where the indices ðm; nÞ run over a set of m2 ; n1 ; n2 ; m0 2 ; n0 1 ; n0 2 values as indicated in (B3). qB1 qA1 3) A1 B1 B2 qw1 qw1 If we multiply the expansion 2 X qB1 qA1 ð1Þ q A1 B1 ¼ s w zr zs ; qw1 qw1 q;r;s¼0 0q;rs 2 1 2
q; r; s ¼ 0; 1; 2;
where ð1Þ
s0q;rs ¼
X
ða1m2 ;n1 n2 d0m0 2 ;n0 1 n0 2 a0m2 ;n1 n2 d1m0 2 ;n0 1 n0 2 Þ;
ðB4Þ
m2 þ m0 2 ¼q n1 þ n0 1 ¼r n2 þ n0 2 ¼s
by the function (3.34), we obtain the expression (4.49) with ð1Þ
dij;kl ¼
X
s0m2 ;n1 n2 bim0 2 ;n0 1 n0 2 ;
i ¼ 0; 1:
ðB5Þ
0
m2 þ m 2 ¼j n1 þ n0 1 ¼k n2 þ n0 2 ¼l
The coefficients appearing in Equation 4.51 can be treated similarly by differentiating the function in 1, 2 and 3 in respect to w2 . Alternatively, it is simpler to invoke the symmetry of I2 in respect to the interchange 1 , 2 (Equation 3.66), which yields the relationships Fcij;kl ¼ cji;lk ¼ cij;kl ð1Þ
Fgij;kl ¼ ði þ 1Þcj;i þ 1;lk
X 0
m2 þ m 2 ¼j 0
n1 þ n 1 ¼k n2 þ n0 2 ¼l
and by renaming i , j and k , l,
a0 m2 i;n2 n1 am0 2 1;n0 2 n0 1
ðB6Þ
Appendix B: The Coefficients of the Recurrence Equation
X
ð1Þ
Fgij;kl ¼ ð j þ 1Þcij þ 1;kl
ð2Þ
a0 m2 j;n2 n1 am0 2 1;n0 2 n0 1 ¼ gij;kl ;
j ¼ 0; 1; 2;
ðB7Þ
m2 þ m0 2 ¼i n1 þ n0 1 ¼l n2 þ n0 2 ¼k
ð1Þ
that is, the only distinction to gij;kl is that now the second index j plays the same role as ð1Þ the first index i of gij;kl . Similarly, we have X ð2Þ ð2Þ dij;kl ¼ sm1 0;n1 n2 bm0 1 j;n0 1 n0 2 ; j ¼ 0; 1; ðB8Þ m1 þ m0 1 ¼i n1 þ n0 1 ¼k n2 þ n0 2 ¼l
where
X
ð2Þ
sp0;rs ¼
ðam1 1;n1 n2 dm0 1 0;n0 1 n0 2 am1 0;n1 n2 dm0 1 1;n0 1 n0 2 Þ:
ðB9Þ
m1 þ m0 1 ¼p n1 þ n0 1 ¼r n2 þ n0 2 ¼s
The counterparts of (B3) and (B5) for the zero-temperature limit (see Equations 4.54 and 4.55) are similarly defined: X ð1Þ g00;kl ¼ ðk þ 1Þc00;k þ 1;l a0 00;kn2 a00;1n0 2 ; k ¼ 0; 1; 2; l ¼ 0; 1; 2; 3; n2 þ n0 2 ¼l
ðB10Þ X
ð1Þ
d00;kl ¼
n2
þ n0
2 ¼l
ð1Þ
s00;0n2 b00;kn0 2 ;
k ¼ 0; 1;
ðB11Þ
where X
ð1Þ
s00;0s ¼
ða00;1n2 d00;0n0 2 a00;0n2 d00;1n0 2 Þ;
ðB12Þ
n2 þ n0 2 ¼s
and finally ð2Þ
g00;kl ¼ ðl þ 1Þc00;k;l þ 1 X
ð2Þ
d00;kl ¼
with ð2Þ
s00;r0 ¼
n1
þ n0
1 ¼k
X n1 þ n0 1 ¼r
ð2Þ
X
a0 00;n1 l a00;n0 1 1 ;
ðB13Þ
l ¼ 0; 1;
ðB14Þ
n1 þ n0 1 ¼k
s00;n1 0 b00;n0 1 l ;
ða00;n1 1 d00;n0 1 0 a00;n1 0 d00;n0 1 1 Þ:
ðB15Þ
j269
j271
Appendix C: The Coefficients of the Recurrence ! m1 ; m2 ; . . . ; mN i1 i2 ip Equations for IN g; fbsm ; blm g fk n1 ; n2 ; . . . ; nN j1 j2 jq Now we express the various c 0 s; g 0 s; and d0 s appearing in the recurrence equations in Section 4.4.6 in terms of coefficients dm;n and am;n given by Equations 4.65–4.67. For this reason, it seems appropriate to refer to Equations B1–B15 of Appendix B. Based on these equations and employing the corresponding equations involving derivatives with respect to the remaining complex variables wi , we have generally X
cm1 m2 mN ;n1 n2 nN ¼
a0 m01 m02 m0N ;n01 n02 n0N am001 m002 m00N ;n001 n002 n00N ;
m01 þ m001 ¼m1 ;...;m0N þ m00N ¼mN n01 þ n001 ¼n1 ;...;n0N þ n00N ¼nN
mi ; ni ¼ 0; 1; 2; 3;
ðC1Þ
where a0
X
m01 m02 m0N ;n01 n02 n0N ¼
am001 m002 m00N ;n001 n01 n00N bm0001 m0002 m000N ;n0001 n0002 n000N ;
0 00 000 0 m001 þ m000 1 ¼m1 ;...;mN þ mN ¼mN 0 00 000 0 n001 þ n000 1 ¼n1 ;...;nN þ n1 ¼nN
m0i ; n0i ¼ 0; 1; 2:
ðC2Þ
Further, ðiÞ
gm
1
mi1 kmi þ 1 mN ;n1 nN
m01
X
þ m001 ¼m1 ;...;m0i1
¼
ðk þ 1Þcm1 mi1 k þ 1mi þ 1 mN ;n1 nN
a0 m01 m0i1 km0i þ 1 m0N ;n01 n02 n0N am001 m00i1 1m00i þ 1 m00N ;n001 n002 n00N ;
þ m00i1 ¼mi1
m0i þ 1 þ m00i þ 1 ¼mi þ 1 ;...;m0N þ m00N ¼mN n01 þ n001 ¼n1 ;...;n0N þ n00N ¼nN
k ¼ 0; 1; 2;
and
Transitions in Molecular Systems. Hans J. Kupka Copyright Ó 2010 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim ISBN: 978-3-527-41013-2
ðC3Þ
j Appendix C: The Coefficients of the Recurrence Equations
272
ðiÞ
dm
1
mi1 kmi þ 1 mN ;n1 nN
X
¼
sm0 m0i1 0m0i þ 1 m0N ;n01 n0N ðiÞ bm001 m00i1 km00i þ 1 m00N ;n001 n00N ;
k ¼ 0; 1;
ðC4Þ
m0 þ m00 ¼m n0 þ n00 ¼n
where ðiÞ
sm1 mi1 0mi þ 1 mN ;n1 nN ¼ X ðam01 m0i1 1m0i þ 1 m0N ;n01 n0N dm001 m00i1 0m00i þ 1 m00N ;n001 n00N m0 þ m00 ¼m n0 þ n00 ¼n
am01 m0i1 0m0i þ 1 m0N ;n01 n0N dm001 m00i1 1m00i þ 1 m00N ;n001 n00N Þ
X
and
ðC5Þ
is an abbreviation for the summation written out explicitly in
m0 þ m00 ¼m n0 þ n00 ¼n
Equation C3. ðiÞ ðiÞ A similar derivation gives for the coefficients g0 0;n1 nN and d0 0;n1 nN appearing in Equation 4.97 for the zero-temperature limit. This is defined by the equations ðiÞ
g0 0;n1 ni1 kni þ 1 nN ¼ ðk þ 1Þc0 0;n1 ni1 k þ 1ni þ 1 nN X
a0 0 0;n01 n0i1 kn0i þ 1 n0N a0 0;n001 n00i1 1n00i þ 1 n00N
ðC6Þ
n01 þ n001 ¼n1 ;...;n0i1 þ n00i1 ¼ni1 n0i þ 1 þ n00i þ 1 ¼ni þ 1 ;...;n0N þ n00N ¼nN
and X
ðiÞ
d0 0;n1 ni1 kni þ 1 nN ¼
n0
ðiÞ
þ n00 ¼n
s0 0;n0 n0 1
iþ1
0n0i1 n0N b0 0;n1 ni1 kni þ 1 nN ; 00
00
00
00
ðC7Þ
where ðiÞ
s0 0;n1 ni1 0ni þ 1 nN
¼
X n0 þ n00 ¼n
ða0 0;n01 n0i1 1n0i þ 1 n0N d0 0;n001 n00i1 0n00i þ 1 n00N
ðC8Þ
a0 0;n01 n0i1 0n0i þ 1 n0N d0 0;n001 n00i1 1n00i þ 1 n00N Þ:
These results come from Equations 4.64–4.67 by setting w1 ¼ w2 ¼ ¼ wN ¼ 0 and differentiating the GF (4.64) with respect to zi , where i ¼ 1; 2; . . . ; N.
j273
Appendix D: Solution of a Class of Integrals In Chapter 5, we encountered a series of integrals for which the solution was simply stated. In this appendix, we shall derive the solutions. We begin with the following: a) The integral Jg ðtÞ. We use Equation 3.18 to write out Equation 5.21 in detail:
Jg ðtÞ
¼
ðbsg blg Þ1=2 ðh2 Þ p½ð1wg2 Þð1z2g Þ1=2 1 ð
1
ð
8 9 < 1 h i= g þ ðqsg qsg Þ2 w 1 dqlg dqlg exp bsg ðqsg þ qsg Þ2 w : 4 ;
9 8 < 1 h i= wg þ ðqsg qsg Þ w 1 bsg ðqsg þ qsg Þ g ; : 2 8 9 < 1 h i= 2 2 exp blg ðqlg þ qlg Þ zg þ ðqlg qlg Þ z1 g : 4 ; 9 8 < 1 h i = l l bg ðqlg þ qlg Þzg ðqlg qlg Þz1 g qg : ; : 2
ðD1Þ
Let us now specialize (D1) to the coordinate system given by Equations 3.70 and 3.71. This gives us Jg ðtÞ ¼
ðbsg blg Þ3=2 ðh2 Þ s 2 ebg kg w g pffiffiffi 2 2p½ð1wg2 Þð1z2g Þ1=2 1 ð
1
2
3 pffiffiffi s 1 s l 2 g þ bg zg Þqg 2bg kg w g qg 5 dqg exp4 ðbg w 2
Transitions in Molecular Systems. Hans J. Kupka Copyright Ó 2010 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim ISBN: 978-3-527-41013-2
j Appendix D: Solution of a Class of Integrals
274
1 ð
1
2
3 1 s l 1 z1 dqg exp4 ðbg w q2g 5 g þ bg g Þ 2
2
g zg Þq2g qg g zg q3 þ ð w 1 w g z1 zg w g g þw p ffiffi ffi 6 pffiffiffi g 6 þ 2kg w g zg q2g þ 2kg ð qg w g zg w g z1 g Þqg 6 1 1 1 1 2 6 þ ð w w w Þq z z z q g g g g g g 4 pffiffiffi g g g z1 2kg w w 1 q2g z1 q3g : g g g
# ðD2Þ
Equation (D2) presents a sum of products of Gaussian integrals of the type 1 ð
Pn ¼
xn eax
2
þ bx
ðD3Þ
dx;
1
s g þ blg zg Þ where pffiffiffi s a ¼ ð1=2Þðbg w g. 2bg kg w In particular, b P1 ¼ G; 2a
or
l 1 1 a ¼ ð1=2Þðbsg w zg Þ g þ bg
and
b¼
ðD4aÞ
P2 ¼
1 b2 þ 2 G; 2a 4a
" P3 ¼
ðD4bÞ
# b 3 3 b G; þ 2a 2 2a2
ðD4cÞ
and so on, where rffiffiffi p G¼ expðb2 =4aÞ: a
ðD5Þ
In such terms, we easily obtain Equation 5.22. Some of the terms in Equation (D2) containing qng vanishes, if n is an odd number. b) The integral Dg ðtÞ Similarly, we may write Dg ðtÞ ¼
ðbsg blg3 Þ1=2 ðihÞ 2p½ð1wg2 Þð1z2g Þ1=2
s 2
ebg kg w g
3 pffiffiffi s 1 s l 2 g þ bg zg Þqg 2bg kg qg 5 dqg exp4 ðbg w 2 1 2 3 1 ð 1 s l 1 1 2 g þ bg zg Þqg 5 dqg exp4 ðbg w 2 1 h i qg þ z1 q2g : zg q2g þ ðzg z1 g Þqg g 1 ð
2
ðD6Þ
Appendix D: Solution of a Class of Integrals
Only the first and third terms in the bracket of Equation D6 contribute. Then, carrying out the integration using the formula (D4b) twice, we obtain Equation 5.35. c) The integral Bg ðtÞ In a similar fashion and by dropping the vanishing terms, we found Bg ðtÞ
¼
l 1=2 ðbs3 ðihÞ g bg Þ
s 2
2p½ð1wg2 Þð1z2g Þ1=2 1 ð
1 1 ð
1
ebg kg w g
2
3 p ffiffi ffi 1 s l s g þ bg zg Þq2g 2bg kg w g qg 5 dqg exp4 ðbg w 2 2
3 1 s l 1 1 2 g þ bg zg Þqg 5 dqg exp4 ðbg w 2
h i pffiffiffi 1 g qg þ w g q2g þ 2kg w q2g : w g
ðD7Þ
This is a relation similar to Equation D6. Carrying out the integration over qg and qg leads to the result (5.40). ~ m ðtÞ d) The expressions Hm ðtÞ and H To evaluate these integrals, it is convenient to begin with the integral of the form ð 1 1 dq1 dq2 exp qt xq þ yt q q ¼ 2pðdet xÞ1=2 exp yt x1 y x1 y: ðD8Þ 2 2 Without bothering to define new symbols, we may use for x ¼ jxij j21 the 2 2 symmetric matrices such as those occurring in the integrand of Equation 3.24. The others q ¼ colðq1 ; q2 Þ and y ¼ colðy1 ; y2 Þ are column vectors, as we have already used in Section 3.2 and in the integral of (3.24). We observe incidentally that Equation D8 is a rather straightforward generalization of Equation 3.25, which we have previously used to derive the generating function G2 ; we shall subsequently see that there is indeed an intimate relationship between G2 ðw1 ; w2 ; z1 ; z2 Þ and Hm ðw1 ; w2 ; z1 ; z2 Þ. To show this, we write according to (3.18) through (3.24) Hm ðw1 ; w2 ; z1 ; z2 Þ ¼
ðbs1 bs2 bl1 bl2 Þ1=2 p2 ½ð1w12 Þð1w22 Þð1z21 Þð1z22 Þ1=2 h i ð1Þ2 ð2Þ2 1 þ bs2 k12 2Þ w exp ðbs1 k12 w 8 2 9 3 1 ð < = 1 1 dq1 dq2 exp4 qt x1 q þ yt q5 pffiffiffi ðqm þ qm Þ : ; 2 2 1
ð
2
3 1 5; t x2 q dq1 dq2 exp4 q 2
ðD9Þ
j275
j Appendix D: Solution of a Class of Integrals
276
where x1 and x2 denote the two 2 2 matrices appearing in Equation 3.24. q and q ¼ colðq1 ; q2 Þ obtained for the original are the column vectors q ¼ colðq1 ; q2 Þ and q (3.22). With the underqlm s and qlm s, m ¼ 1; 2, according to the transformation pffiffiffi standing that in our decomposition of q0 m ¼ ð1= 2Þðqm þ qm Þ it is only the qm term that gets a contribution, we can carry out the integration by using the formula (D8) twice. This leads to ! ! ð1Þ 1 þ w21 bs2 kð2Þ 2 H1 ðw1 ;w2 ; z1 ; z2 Þ w11 bs1 k12 w 12 w ¼ ð1Þx11 G2 ðw1 ;w2 ;z1 ; z2 Þ ð1Þ H2 ðw1 ;w2 ; z1 ; z2 Þ 1 þ w22 bs2 kð2Þ w12 bs1 k12 w w 2 12 ðD10Þ
and after a cumbersome algebra, to Hm ðw1 ;w2 ;z1 ; z2 Þ ¼ Hmð0Þ ðw1 ; w2 ; z1 ;z2 ÞG2 ðw1 ;w2 ; z1 ; z2 Þ; m ¼ 1; 2;
ðD11Þ
ð0Þ
with Hm given by Equations 5.27 and 5.28. ~ m ðtÞ ðm ¼ 1; 2Þ, recalling In a quite similar manner, we obtain the expression for H that (see Equations 3.22b and 3.23) ! s ð1Þ 1 w11 w12 q1 q1 þ q1 k12 p ffiffi ffi ðD12Þ ¼ þ ð2Þ : qs2 q2 þ q2 2 w21 w22 k12 We may therefore substitute qsm in Equation D9 instead of qlm and use Equation D12 to obtain 1 ðw1 ; w2 ; z1 ; z2 Þ H
¼
ð0Þ
ð0Þ
½w11 H1 ðw1 ; w2 ; z1 ; z2 Þ þ w12 H2 ðw1 ; w2 ; z1 ; z2 Þ ð1Þ
þ k12 G2 ðw1 ; w2 ; z1 ; z2 Þ; and 2 ðw1 ; w2 ; z1 ; z2 Þ ¼ ½w21 H ð0Þ ðw1 ; w2 ; z1 ; z2 Þ þ w22 H2ð0Þ ðw1 ; w2 ; z1 ; z2 Þ H 1 ð2Þ
þ k12 G2 ðw1 ; w2 ; z1 ; z2 Þ;
ðD13Þ
omitting, as before, terms of qm that do not contribute. After a little algebra and the use of Equations 5.27 and 5.28, we are led to expressions (5.31) and (5.32). This completes our derivations.
j277
Appendix E: Quantization of the Radiation Field If we view the field in empty space, then by means of the Coulomb gauge we can eliminate the scalar potential from the calculations. Aðr; tÞ is the vector potential, Eðr; tÞ is the electric field, and Bðr; tÞ is the magnetic induction. The fields are given in terms of vector potential by [145] r2 A
1 q2 A ¼ 0; c2 qt2
E¼
1 qA ; c qt
div A ¼ 0;
B ¼ r A:
ðE1Þ
ðE2Þ
The initial and boundary conditions for A define themselves, from those to which E and B are subordinated. Since the equations that satisfy the vector potential A are linear, A can be expanded in a series of plane waves. This expression is [145] Aðr; tÞ ¼
X h 1=2 ak^e Ak^e ðrÞeiv^eðkÞt þ ak^e Ak^e ðrÞeiv^eðkÞt : 2vk^e k;^e
ðE3Þ
This is called development by modes. ak^e and ak^e are dimensionless complex numbers. The sum on k here extends over all plane wave momentum states k in the box V. The sum on ^e extends over the two allowed directions of polarization of a photon having a momentum k. The functions Ak^e satisfy the equations r2 Ak^e ðrÞ þ
v^2e ðkÞ c2
Ak^e ðrÞ ¼ 0 ðhve^ðkÞ ¼ ckÞ;
ðE4Þ
r Ak^e ðrÞ ¼ 0
and form a complete orthogonal system. Considering the case of radiation in a cube V of length L, imposing periodicity requirements instead of boundary conditions, one obtains rffiffiffiffiffiffiffiffiffiffiffiffi 4phc2 Ak^e ðrÞ ¼ ^e expðikr=hÞ; ðE5Þ L3 Transitions in Molecular Systems. Hans J. Kupka Copyright 2010 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim ISBN: 978-3-527-41013-2
j Appendix E: Quantization of the Radiation Field
278
where ^e is the polarization unity vector. The normalization of the expression (E5) is determined from an evaluation of the Poynting flux S ¼ ðc=4pÞE B. The field quantization can be performed by regarding the amplitudes ak^e and ak^e as þ operators ak^e and ak^ e , which satisfy the (canonical) commutation relations ½ak^e ak0^e0
¼
þ þ ½ak^ e ak0^e0 ¼ 0
½ak^e akþ0^e0
¼
dkk0 d^e^e0
The energy of the electromagnetic field is expressed as ð X 1 1X þ þ H ¼ ðE 2 þ B2 Þdr ¼ Hk^e ¼ hv^e ðkÞðak^ e ak^e þ ak^e ak^e Þ: 2 2 k;^e k;^e
ðE6Þ
ðE7Þ
This is nothing more than the sum of N independent oscillator Hamiltonians, one for each wave vector k and polarization ^e. Every mode then corresponds to a harmonic oscillator of which is known that the quantization leads to the following results: Hk^e jnk^e i ¼
1 nk^e þ hv^e ðkÞjnk^e i; 2
ak^e j0k^e i ¼ 0;
ðE8Þ ðE9Þ
ak^e jnk^e i ¼ ðnk^e Þ1=2 jnk^e 1i;
ðE10Þ
1=2 þ jnk^e þ 1i; ak^ e jnk^e i ¼ ðnk^e þ 1Þ
ðE11Þ
þ ak^ e ak^e jnk^e i ¼ nk^e jnk^e i;
ðE12Þ
jnk^e i ¼
þ nk^e ðak^ eÞ
ðnk^e !Þ1=2
j0k^e i;
ðE13Þ
where the ground state of the energy Hk^e is denoted by j0k^e i and nk^e is the number of photons in a momentum state k having polarization parallel to ^e (and, of course, k ^e ¼ 0 since the field is transverse). Those eigenstates of the energy are stationary and are known as state vectors. They form a complete orthonormal system that spans the space of photon occupation numbers or Fock space. When a Hamiltonian H separates into a sum of commuting sub-Hamiltonians Hk , its eigenstates are simply products of eigenstates of each of the separate subHamiltonian, and the corresponding eigenvalues are the sum of the individual eigenvalues of the sub-Hamiltonians. We can therefore specify an eigenstate of H by giving a set of quantum numbers nk^e , one for each of the N independent oscillator Hamiltonians Hk^e , or for each of the photons nk^e of type ^e with wave vector k and frequency v^e ðkÞ: j ¼ jnk1^e1 ; nk2^e2 ; . . . ; nk^e ; . . .i:
ðE14Þ
Appendix E: Quantization of the Radiation Field þ Equations E10 and E11 lead to the interpretation of ak^e and ak^ e as the respective operators for absorption and creation of photons in the state jk; ^ei with the energy hv^e ðkÞ. The development of the field is then determined by the equation
ih
q jji ¼ Hjji: qt
ðE15Þ
The initial conditions are introduced by specification of a vector jj0 i at a time t0 . For a realistic description of an actual excitation process, Jortner and Mukamel [146] introduced on the basis of Equation E14 a photon wave packet X Xk^eA ¼ ank^e1 nk^e2 nk^e jnk1^e1 nk2^e2 nk^e i; ðE16Þ fnki ^ei g
which is characterized by the energies Ei ¼ ki (where we have used the units c; h ¼ 1). For moderately weak fields, nki^ei ¼ 0 or 1 for all i and under these conditions, we may consider an initial state of the field j ð0Þ consisting of a wave packet of one-photon states X jð0Þ ¼ ak jk^ei; ðE17Þ k
P where ak is the initial amplitude of the state jk^ei, while the summation k represents the integration over photon energies over special directions and summation over all polarization directions.
j279
j281
Appendix F: The Molecular Eigenstates
Following here the treatment of Ref. [11], the molecular eigenstates are defined as a superposition of zero-order BO states by the Ansatz yn ¼
m X s¼1
ans js þ
1 X i¼1
bni ji ;
ðF1Þ
where the states of energy Es ðs ¼ 1; 2; . . . ; mÞ carry oscillator strength to the ground state. These states are superimposed on a dense manifold of vibronic states fji g that do not carry oscillator strength. For simplicity, it will be assumed that the latter states are equally spaced, and let e be the spacing between these levels. The matrix elements between the zero-order states are hjs jHel jjt i ¼ Es dst ;
ðF2Þ
hji jHel jjj i ¼ Ei dij ;
ðF3Þ
hjs jHel jji i ¼ hjs jHv jji i ¼ vsi ¼ vs ;
ðF4Þ
where we have again assumed that all the vibronic coupling matrix element vsi are equal. The secular equations that determine the values of the expansion coefficients in (F1) are X ans Es þ bni vs ¼ En ans ; ðF5Þ i
X s
ans vs þ bni Ei ¼ En bni ;
where En are the new eigenvalues. The last equation can be solved for bni and one gets X bni ¼ ðEn Ei Þ1 ans vs : s
Transitions in Molecular Systems. Hans J. Kupka Copyright 2010 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim ISBN: 978-3-527-41013-2
ðF6Þ
ðF7Þ
j Appendix F: The Molecular Eigenstates
282
Substituting the result in Equation F5 yields P n a vt X ans þ t t vs ðEn Ei Þ1 ¼ 0; Es En i
ðF8aÞ
or ½vs =ðEn Es Þ
X t
ant vt
X i
ðEn Ei Þ1 ¼ ans :
ðF8bÞ
Multiplication by vs and summation over s leads to the result X X X n X at vt ðEn Ei Þ1 ¼ ans vs ; v2s =ðEn Es Þ s
t
ðF9Þ
s
i
or alternatively, X s
" #1 X v2s =ðEn Es Þ ¼ ðEn Ei Þ1 ;
ðF10Þ
i
which is a equation for En. The sum on the right-hand side of the equation is known ½11, so one gets !1 X X v2 s ¼ ðEn Ei Þ1 ¼ ðp=eÞ cot g½ðp=eÞðEn E0 Þ: ðF11Þ E E n s s i The values of the coefficients ans are determined from the normalization condition hyn jyn i ¼ 1 ¼ "
X i
X 2 X 2 an þ bn ¼ s i s
1 En Ei
i
!2
X t
!2 ant vt
# X ns 2 X 1 2 : þ En Es En Ei s i
ðF12Þ
The last sum on the right-hand side of Equation F12 can be expressed in the form p p2 h p i X 1 2 p2 ¼ 2 cos ec2 ðEn E0 Þ ¼ 2 1 þ cot g 2 ðEn E0 Þ : En Ei e e e e i ðF13Þ
Using the result of Equation F11, we get X i
1 En Ei
2
X v2 p2 s ¼ 2 þ e En Es s
!2 :
Substitution of Equations F10 and F14 into Equation F12 leads to
ðF14Þ
Appendix F: The Molecular Eigenstates
X t
!2 ant vt
" ¼
X vt 2 p2 þ1þ 2 En Et e t
X t
v2s En Et
!2 #1
X t
v2t En Et
!2 : ðF15Þ
Using Equations F11 and F15, one gets from (F8b) the following expression for the coefficient ans : n 2 as ¼
vs En Es
2 "X t
vt En Et
2 þ1þ
p2 e2
In the case of one resonance ðm ¼ 1Þ, we get 2 1 n 2 : as ¼ a2n ¼ v2s ðEn Es Þ2 þ v2s þ pv2s =e
X t
v2t En Et
!2 #1 :
ðF16Þ
ðF17Þ
These equations describe the probability of finding the vibronic states js in the new state yn . Furthermore, Equation F17 describes a Lorentzian as a function of En and a half width given by 2 1=2 Ds ¼ v2s þ pv2s =e :
ðF18Þ
j283
j285
Appendix G: The Effective Hamiltonian and Its Properties
Consider a physically acceptable system of the complex-level structure that involves the Born–Oppenheimer basis, consisting of the ground electronic state j g i ¼ j0i and a single doorway state jsi that is coupled via nonadiabatic intramolecular interactions Hvib to a background of fjlig states, and where both the states jsi and the manifold fjlig are characterized by the radiative and nonradiative decay widths cs and cl , respectively (see Figure 6.2). The effective Hamiltonian responsible for this system is Es ics =2 Vsl Vsl0 Vsl El icl =2 0 : ðG1Þ Heff ¼ Vsl0 0 El0 icl0 =2 . . . . .. .. .. .. In the above basis, the Hamiltonian Heff is off-diagonal, while the damping matrix is diagonal. From the basis definition (see Equation A19), it is evident that the effective Hamiltonian is non-Hermitian. This can be rationalized by noting that we consider only a subspace of the Hilbert space, consisting of the above discrete zero-order basis set. In fact, the effective Hamiltonian of Equation G1 can be written as a sum Heff ¼ Hel iC=2;
ðG2Þ
where Hel is a Hermitian matrix and iC=2 is an anti-Hermitian matrix. Furthermore, when the effective Hamiltonian is nondiagonal within the basis of zero-order states, these states cannot be considered to decay independently. Thus, the time evolution operator expðiHeff tÞ in the P subspace will contain off-diagonal contributions. We shall now transform the Heff matrix to a representation in which it is diagonal (as was done, for instance, in Section 7.5.5). This leads to a basis fj jig obtained by the transformation
where
D1 Heff D ¼ L;
ðG3Þ
j1 s l ¼ D j2 : . . .. ..
ðG4Þ
Transitions in Molecular Systems. Hans J. Kupka Copyright Ó 2010 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim ISBN: 978-3-527-41013-2
j Appendix G: The Effective Hamiltonian and Its Properties
286
D in Equation G3 is a nonunitary matrix. When a basis set is chosen such that Hel is a real matrix (as in the case above), Heff is a complex symmetry matrix, which can be diagonalized by an orthogonal transformation D. The matrix elements of the diagonal matrix L are in general complex Ljj0 ¼ ðEj icj =2Þdjj0 ;
ðG5Þ
with a negative imaginary part cj =2 and in general we cannot find any orthogonal set of eigenvectors. While the eigenvectors are not orthogonal, they have an orthogonality relation with a different set of vectors, which must be defined. In the most cases, our eigenvectors have been column vectors x, which are multiplied to the right of a matrix A (Heff in our case), that is, A x ¼ l x;
ðG6Þ
where l are the eigenvalues determined by detjAl1j ¼ 0:
ðG7Þ
These are termed right eigenvectors. We could also, however, try to find row vectors x, which multiply A to the left and satisfy x A ¼ l x:
ðG8Þ
These are called left eigenvectors. By taking the transpose of this equation, we can see that every left eigenvector is the transpose of a right eigenvector of the transpose of A. Now by taking into account that the determinant of A in Equation G7 equals the determinant of the transpose of A, we also see that the left and right eigenvalues of A are identical. To pursue this matter a little further, we arrive to the conclusion that if the eigenvalues l are nondegenerate, each left eigenvector is orthogonal to all right eigenvectors, and vice versa. To return now to the question of the orthogonality relation of our eigenvectors j ji, we may quite generally write jj ji ¼ djj0 ; ðG9Þ where jj are the defined left eigenvectors. This complementary basis j is defined by the transformation X þ j ¼ ðD Þjn jni; n ¼ s; l; l0 ; . . . : ðG10Þ n
The corresponding projection operator P can be written in terms of j ji and j as X P¼ ðG11Þ j ji jj j
and the time evolution operator X X P expðiHeff tÞP ¼ j jiexpðiLjj tÞh jj ¼ j jiexpðiEj tcj t=2Þ jj j
ðG12Þ
j
is expressed as a sum of independently decaying levels characterizing the molecular system. A rigorous discussion to this subject may be found in Refs [146, 149].
j287
Appendix H: The Mechanism of Nonradiative Energy Transfer
H.1 Single-Step Resonance Energy Transfer
To proceed with our discussion about the host-sensitized energy transfer in the system of pentacene in p-terphenyl, we review the simplest of energy transfers. This is the transfer in a system that consists of a molecule or ion S (sensitizer) and a molecule (ion) A (activator). If any possible interaction (i.e., exchange interaction) between S and A is disregarded, the system may be represented by the product of the wavefunction of S and the wavefunction of A. In particular, two states of the system are of interest: a) State ys ya with molecule S in the excited state and molecule A in the ground state. b) State ya ys with molecule S in the ground state and molecule A in the excited state. Initially the sensitizer S is in an excited state and the activator A is in the ground state, while after energy transfer the sensitizer is in the ground state and the activator in the excited state (see Figure H.1). The transfer rate between these states is described by 2 wsa ¼ ð2p=hÞMif rf ðEi Ef Þ;
ðH1Þ
where Mif is the matrix element between initial and final states of the system and rf is the density of final states. The transfer matrix element is related to the Coulomb interaction of the electrons and nuclei and can be expanded in a series of multipole–multipole interactions about the sensitizer–activator separation Rsa . For neutral molecules, the leading term in this expansion is the electric dipole–dipole interaction first described by F€orster [302–305]: DD Hint ¼
1 ðms Rsa Þðma Rsa Þ ; m m 3 eR3sa s a R2sa
Transitions in Molecular Systems. Hans J. Kupka Copyright Ó 2010 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim ISBN: 978-3-527-41013-2
ðH2Þ
j Appendix H: The Mechanism of Nonradiative Energy Transfer
288
|Ψs*>
|Ψa*>
Wsa
|Ψ s >
| Ψa >
Figure H.1 Resonant energy transfer between an excited sensitizer and unexcited activator molecule (ion).
where e is the dielectric constant of the medium and ms and ma are the two electric dipoles of S and A. Later Dexter expanded the treatment to include higher order electromagnetic and exchange interactions [306]. In the case of resonance electric dipole–dipole transfer, the relevant matrix element Mif is DD w w x 0 x 0 Mif ¼ xsm xan ws wa Hint a s am sn 1 ws jms jws tsa wa jma jwa ðxsm xan jxam0 xsn0 Þ ¼ ðH3Þ 3 eRsa ¼ JðRsa Þðxsm xan jxam0 xsn0 Þ;
where for the special case of a homogeneous mixed p-terphenyl crystal, the dipoles ms ¼ ma ¼ m are parallel to the short M-axis of pentacene and Rsa is taken along the b0 sa Þ, where R sa is the unit vector crystallographic axis. Hence, tsa ¼ 13 cos2 ðm R along the Rsa distance. The transition energies are not sharp but rather have finite widths due to thermal vibrations in the crystal. Thus, the density of states can be treated as function of energy, rðEi Ef Þ ¼
1 C ; p ðEi Ef Þ2 þ C2
ðH4Þ
where C ¼ hc;
Ei ¼ hVs þ
Ef ¼ hVa þ
X mm
X mm
hmm0 vam þ
hmm vsm þ X nm
X nm
hnm vam
and ðH5Þ
hn0m vsm :
Substituting (H3) through (H5) into (H1) and summing over the vibrational quantum numbers, the probability of resonant energy transfer can be written as wsa ¼
2p 2 1 X X J h2 p mm ;nm mm0 ;n0m INs
c X X ðmm vsm þ nm vam Þ ðmm0 vam þ n0m vsm Þ Vs Va þ m
m1 ; m2 ; . . . ; mN a m10 ; m20 ; . . . ; mN0 IN ; n01 ; n02 ; . . . ; n0N n1 ; n2 ; . . . ; nN
!2 þ c2
m
ðH6Þ
H.2 Phonon-Assisted Energy Transfer
or in compact form ð 2p wsa ¼ 2 J 2 dv Fs ðvVs ÞFa ðvVa Þ; h
ðH7Þ
where Fs and Fa are the spectral line shape functions for the sensitizer and activator, respectively.1) From (H7) we see that a nonzero overlap is essential for resonance F€orster energy transfer. The transfer rate (H7) can be expressed in more conventional units wsa ¼ ðtF Þ1 ðR0 =Rsa Þ6 ;
ðH8Þ
where tF is the fluorescence decay time (intrinsic lifetime in the absence of activator) of the sensitizer and R0 is a critical transfer distance given by [302, 303] R60 ¼
ð 9000 gt2sa ln 10 f ð~nÞeð~nÞ d~n 128p6 n4 NA ~n4
~n ¼
v : 2pc
ðH9Þ
Here g is the quantum efficiency of the sensitizer (g ¼ tF =tsF ¼ 1=3 for pentacene) in the O4 site of p-terphenyl at 4 K,2) n is the index of refraction (n ¼ 1:7 for the p-terphenyl crystal), and NA is the Avogadros number. The integral in (H9) is calculated from the normalized fluorescence spectrum f ð~ nÞ and the decadic molar extinction coefficient eð~nÞ of pentacene at O4 site. The critical interaction distance is the sensitizer–activator separation for which the transfer rate is equal to the intrinsic decay time. Although derived for low temperatures, Equation H9 is also valid for arbitrary temperatures. In fact, the temperature dependence of the resonant energy transfer rate is contained in the spectral overlap integral.
H.2 Phonon-Assisted Energy Transfer
The rate of resonant energy transfer described above critically depends on the energy match between the sensitizer and activator transitions. This is reflected in the dependence of wsa on the spectral overlap integral. Lattice vibrations affect the widths and position of spectral transitions and, thus, the line shape function appearing in the overlap integral. If there is significant energy mismatch DEsa ¼ h ðVs Va Þ between sensitizer and activator transitions as shown in Figure H.2, the spectral overlap and, thus, the resonant energy transfer rate can 1) In writing (H7), we have made use of the fact that a convolution of two Lorentzians of widths cs and ca centered at V0s and V0a , respectively, is 1 cs þ ca a Lorentzian of the p ðV0s V0a Þ2 þ ðcs þ ca Þ2 width c ¼ cs þ ca . 2) The quantum yield g for pentacene in the O4 site of p-terphenyl is given by g ¼ tF =tsF ¼ 10=30, where tsF ¼ 30 ns is the
natural fluorescence lifetime in the absence of relevant radiationless or vibronic processes. It must be emphasized that the fluorescence lifetimes tF of pentacene are different in the (inequivalent) substitutional guest sites of the host crystal. The spectra of the four sites differ also in their intensity distributions and in their phonon sideband structures.
j289
j Appendix H: The Mechanism of Nonradiative Energy Transfer
290
|Ψs*>
∆Esa
|Ψa*> Wsa
|Ψ s >
| Ψa >
Figure H.2 Phonon-assisted energy transfer for molecules (ions) with a transition energy mismatch of DEsa .
be negligibly small. In this circumstance, the energy transfer can occur through phonon-assisted processes [307–312]. The interaction Hamiltonian Hint consists of DD two parts, one describing the dipole–dipole interaction Hint as discussed above and one describing the vibronic interaction Hv ¼
X
Vk ðiÞqk ;
ðH10Þ
i¼s;a
where Vk ðiÞ 6¼ 0 only in a small region located mainly at the positions of the sensitizer S and of the activator A and qk is the promoting mode displacement. The wavefunctions for the initial and final states must now include the vibrational factor for the promoting mode (phonon) that is emitted or absorbed: jyi i ¼ ws wa xsm xan ;
ðH11Þ
E yf ¼ ws wa xsn xam :
ðH12Þ
Since the energy of the sensitizer (excited state) is greater than the energy of the activator (excited state), the transition takes place only in the direction S ! A with the emission of a phonon. By including Hv , the phonon-assisted energy transfer is a DD DD second-order process in respect to H0 ¼ Hint þ Hv (first order in Hint and first order in Hv ), so the relevant matrix element can now be expressed by [310] Mifk ¼
D E DD y ; nk þ 1 hy ; nk þ 1jHv ð jÞjy ; nk i X yf ; nk þ 1Hint i i i Es ðEs h vk Þ ED E DD y ; nk X yf ; nk þ 1jHv ð jÞjyf ; nk yf ; nk Hint i
j¼s;a
þ
j¼s;a
ðH13Þ
D
Es Ea
;
where jyi ; nk þ 1i is an intermediate state. Using the sum in equation H13 accounts for the possibility of the phonon process occuring at either the sensitizer or activator site
H.2 Phonon-Assisted Energy Transfer
Mifk ¼
DD w w ws wa Hint s a ws jVk ðsÞjws xs;nk þ 1 jqk jxs;nk Es ðEs hvk Þ þ hwa jVk ðaÞjwa i xa;nk þ 1 jqk jxa;nk xs;n0 xa;m 0 jxs;m0 xa;n0 w w HDD w w þ s a int s a hws jVk ðsÞjws i xs;nk þ 1 jqk jxs;nk Es;0 Ea;0 þ wa jVk ðaÞjwa xa;nk þ 1 jqk jxa;nk xs;n0 xa;m 0 xs;m0 xa;n0 ; ðH14Þ
where the plus or minus sign refers to the case of phonon emitted or phonon absorbed, respectively. Setting DEsa ¼ Es;0 Ea;0 ¼ hvk for conservation of energy, Equation H14 simplifies to DD w w ws wa Hint s a k Mif ¼ hws jVk jws i ws jVk jws hwa jVk jwa i wa jVk jwa hvk 0 11=2 h ðn þ 1Þ k A ðxsn0 xam 0 jxsm0 xan0 Þ @ 2vk 0 11=2 J h ðn þ 1Þ k A ðxsn0 xam 0 jxsm0 xan0 Þ: ¼ ð f gÞ@ hvk 2vk ðH15Þ
Here again we find that the promoting mode contribute to the transition via hws jVk jws i and hwa jVk jwa iand that the contribution to the vibrational overlap is given by ðhðnk þ 1Þ=2vk Þ1=2 ðxsn0 xam 0 jxsm0 xan0 Þ with nk ¼ 0. The comparison with Equation H3 that applies to the case of resonant energy transfer and which Ei and Ef are given by Equation H5 should be noted. The difference that arises from the additional vibronic interaction is manifested not only in the electronic part of the matrix element Mifk but also in a diminished initial energy gap hðVs vk Þ in the density of states function (H4). If we make these modifications in Equation H1, we will immediately recover the appropriate expression for the phonon-assisted energy transfer: ð p J 2 sa ¼ w ð f gÞ2 FS ðvVs ÞFA ðvVa vk Þdv; ðH16Þ hvk hvk where the spectral line shape functions for emission and absorption FS ðvÞ and FA ðvÞ are centered at VS and Va þ vk , respectively.
j291
j293
Appendix I: Evaluation of the Coefficients bmn , cmn , and bm in the Recurrence Equations 8.28 and 8.29 One must evaluate the derivatives q2 D11 =qwm qwn ; q2 D22 =qzm qzn , and qD1 =qwm by noting that they are the coefficients of the quadratic and linear terms in w and z in the forms (8.16), (8.18), and (8.22), respectively. By differentiating of Equation 8.16 with respect to wm and wg , we obtain with the help of Equation 8.17 for the case m 6¼ g: bmn ¼ bnm ¼ 2 ¼ B
(
1 q2 D11 2 qwm qwn X
ð1Þm þ n W
1pN
1 m1;m þ 1 N
a1 p1;p þ 1 N W þ
1 m1; m þ 1 N 1 p1; p þ 1 N
1 n1; n þ 1 N n1;n þ 1 N a11 p1;p þ 1 N 1 p1; p þ 1 N X X ð1Þr þ s
1i1 < ir1 <m
i1 ir1 ir þ 1 iN1 ai1 ir1 ir þ 1 iN1 j1 jp1 jp þ 1 jq1 jq þ 1 jN j1 jp1 jp þ 1 jq1 jq þ 1 jN i1 is1 is þ 1 iN1 is1 is þ 1 iN1 W aij11 jp1 jp þ 1 jq1 jq þ 1 jN j1 jp1 jp þ 1 jq1 jq þ 1 jN X m n þ W amt W ant g: t t 1tN W
ðI1Þ
Note that the sum in the second row of the right-hand side of Equation I1 is restricted to those sets of indices 1 i1 < < ir1 < m < ir þ 1 < < is1 < n < is þ 1 < < iN1 N, which involve both the numbers m and n. Similarly, we have bmm
1 q2 D11 2 ¼ ¼ 2 qwm2 B
(
X
W
1pN
2 1 m1;m þ 1 N a1 p1;p þ 1 N þ
1 m1; m þ 1 N 1 p1; p þ 1 N X
2
X
1i1 < ir1 <m
Transitions in Molecular Systems. Hans J. Kupka Copyright Ó 2010 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim ISBN: 978-3-527-41013-2
j Appendix I: Evaluation of the Coefficients b
294
mn,
cmn, and bm in the Recurrence Equations
2
i1 ir1 ir þ 1 iN1 j1 jp1 jp þ 1 jq1 jq þ 1 jN
W
þ þ
X X
W
n6¼m 1tN
ir1 ir þ 1 iN1 aij11 jp1 jp þ 1 jq1 jq þ 1 jN
2 n ðant Þ2 þ 1g: t
2
ðI2Þ
To obtain the expressions for amn, we can proceed as we did above with the exception that now Equation 8.22 must be differentiated with respect to zm and zn . Alternatively, it is simpler, however, to evaluate these coefficients recalling the symmetry of D11 and D22 with respect to the interchange wm , zm discussed at the end of Section 8.1. In view of this symmetry, the coefficients amn can be obtained directly from Equations I1 and I2 by multiplying their right-hand side by 1 and interchanging the top and bottom sets of indices on the quantities in the former. Finally, according to Equation 8.22, the coefficients bm are given by 8 ð12 NÞ qD1 2 < X ð12 NÞ qXp bm ¼ ¼ Dp qwm B :1pN qwm X
þ
X
ði ir1 mir þ 1 iN1 Þ
1i1 < ir1 <m
qXjp j1q
ði i Þ Dj1 pj2 q jN1
X
þ þ
qwm
Djp 1jq
X
1ip
ði i Þ qXj1 jp2 q jN1
qwm
) ðmÞ þ D12 N
:
I.1 Application
We illustrate the workings of the formulas given above for the case N ¼ 3: ( 2 2 2 2 23 23 23 2 23 2 23 2 b11 ¼ ða23 Þ þ W ða13 Þ þ W ða23 W 12 Þ 13 12 23 B þW
2 2 2 2 2 2 3 2 ða23 Þ2 þ W ða22 Þ2 þ W ða21 Þ2 þ W 2 1 3 3
ða33 Þ2 b12 ¼
) 2 2 3 3 3 2 3 2 þW ða2 Þ þ W ða1 Þ þ 1 ; 2 1
2 13 23 13 23 13 13 a13 a a a23 W W W W 23 23 13 13 23 23 13 13 B
13 23 1 2 13 23 1 W a12 W a12 W a3 W a23 12 12 3 3
ðI3Þ
) 1 2 1 2 1 2 1 a2 W a2 W a1 W a21 ; W 2 2 1 1 b13 ¼
I.1 Application
2 23 12 23 12 23 12 a a a23 a12 W þ W W W 23 23 13 13 23 13 13 23 B
23 1 3 12 a23 a13 W a33 a12 W W 12 12 12 3 3 12 ) 1 3 1 3 1 3 1 a2 W a2 W a1 W a31 ; W 2 2 1 1
þW
b22
( 2 2 2 2 13 13 13 2 2 13 2 ¼ ða13 Þ þ W ða Þ þ W ða13 W 23 13 12 Þ 13 12 23 B 2 2 2 2 1 1 1 3 ða13 Þ2 þ W ða12 Þ2 þ W ða11 Þ2 þ W ða33 Þ2 3 2 1 3 ) 2 2 3 3 3 2 3 2 þW ða2 Þ þ W ða1 Þ þ 1 ; 2 1
þW
b23 ¼
2 13 12 13 12 a13 a12 a13 a12 W W W W 23 23 13 13 23 13 13 23 B
13 2 3 12 13 2 a a a33 a12 W W W 12 12 3 12 3 3 12 ) 2 3 2 3 2 3 2 W a2 W a2 W a1 W a31 ; 2 2 1 1
W
b33
( 2 2 2 2 12 12 12 2 ¼ ða12 Þ2 þ W ða12 Þ2 þ W ða12 W 23 13 12 Þ 13 12 23 B 2 2 2 1 2 1 1 2 2 2 þW ða3 Þ þ W ða3 Þ þ W ða12 Þ2 3 3 2 þW
) 2 2 2 2 1 2 ða22 Þ2 þ W ða11 Þ2 þ W ða21 Þ2 þ 1 : 2 1 1
The coefficients cmn are calculated directly from Equation 8.21, 4 123 23 12 2 a123 a23 a12 a23 W c11 ¼ W þW W 123 23 13 123 23 13 3 B 13 3 12 2 3 12 þW a13 W a þ W a W a22 13 3 12 13 3 12 2 ) 13 3 1 13 3 a12 W a2 þ W a11 ; þW 12 2 1
j295
j Appendix I: Evaluation of the Coefficients b
296
mn,
cmn, and bm in the Recurrence Equations
4 23 12 2 123 a23 a12 a21 a123 W W W W 123 13 12 13 12 1 123 B
c12 ¼
2 13 3 12 2 13 a a a31 a12 W W W 23 3 12 3 12 1 23 ) 13 3 1 13 3 a23 W a3 þ W a12 ; þW 23 3 2
þW
c13 ¼
4 23 12 2 123 a23 a12 a22 W W W a123 W 123 12 23 12 23 2 123 B 2 13 3 12 2 13 a a a32 a12 W W W 13 1 23 1 23 2 13 ) 13 3 1 13 3 a13 W a1 þ W a13 ; W 13 1 3
W
4 13 12 1 123 13 12 a a a13 a123 W W W W 123 23 13 23 13 3 123 B
c21 ¼
1 23 3 12 12 1 23 a2 þ W a13 W a33 a12 W W 2 13 3 12 ) 23 3 2 23 3 a12 W a2 þ W a21 ; þW 12 2 1
c22 ¼
4 13 12 1 123 a13 a12 a11 a123 W þW W W 123 13 12 13 12 1 123 B 1 23 3 12 1 23 a a a31 a12 W W W 23 3 12 3 12 1 23 ) 23 3 2 3 a23 a a22 ; þW W þ W 23 3 23 3 2
W
c23 ¼
4 13 12 1 123 a13 a12 a11 a123 W þW W W 123 12 13 12 13 1 123 B
23 3 12 1 a23 a31 þ W a12 a12 W W 13 23 13 1 23 2 ) 23 3 2 23 3 a23 W a2 þ W a23 ; W 23 2 3 W
c31 ¼
4 12 13 1 123 12 13 a a a13 a123 W W W W 123 23 13 23 13 3 123 B
I.1 Application
13 1 23 2 1 23 a13 a a a23 W W W W 12 2 13 12 2 13 3 ) 23 3 3 23 3 3 a a W 12 W 2 2 þ W 1 a1 ; 12 c32
4 12 13 1 123 123 12 13 a13 þ W a12 W a11 ¼ a123 W W 13 12 1 123 B 1 23 2 13 1 23 a a a21 a13 W þ W W 23 3 12 3 12 1 23 ) 23 2 3 23 2 W a23 W a3 þ W a32 ; 23 3 2
W
4 12 13 1 123 123 12 13 a12 þ W a13 W a11 a123 W ¼ W 12 13 1 123 B
c33
1 23 2 13 1 23 a a a21 W þ W W a13 23 2 13 2 13 1 23 ) 23 2 3 23 2 a23 W a2 þ W a33 : þW 23 2 3
þW
We now return to Equation I3 for the bm coefficients and carry out the sum over the indices in Equation I3. We then find by using Equation 8.17 2 23 23 23 ð123Þ 23 ð123Þ 23 ð123Þ b1 ¼ a13 D2 þ W a13 W a23 D1 W 12 D3 13 12 23 B þW
2 2 2 ð12Þ ð12Þ ð12Þ a23 D12 W a22 D13 þ W a21 D23 3 2 1
) 3 3 3 ð1Þ 3 ð13Þ 3 ð13Þ 3 ð13Þ a3 D12 W a2 D13 þ W a1 D23 þ D123 ; þW 3 2 1 b2 ¼
2 13 13 13 ð123Þ ð123Þ 13 ð123Þ D þ W a D W a13 W a13 23 1 13 2 12 D3 13 12 23 B 1 1 1 ð12Þ 1 ð12Þ 1 ð12Þ a2 D13 W a11 D23 W a3 D12 þ W 2 1 3
) 3 3 3 ð2Þ 3 ð23Þ 3 ð23Þ 3 ð23Þ a3 D12 W a2 D13 þ W a1 D23 þ D123 ; þW 3 2 1 b3 ¼
2 12 12 12 ð123Þ ð123Þ 12 ð123Þ a a12 a12 D W D þ W W 23 1 13 2 12 D3 13 12 23 B
j297
j Appendix I: Evaluation of the Coefficients b
298
mn,
cmn, and bm in the Recurrence Equations
1 1 1 ð13Þ ð12Þ ð13Þ a13 D12 þ W a12 D13 W a11 D23 W 3 2 1
) 2 2 2 ð3Þ 2 ð23Þ 2 ð23Þ 2 ð23Þ a3 D12 þ W a2 D13 W a1 D23 þ D123 : W 3 2 1
j299
Appendix J: Evaluation of the Position Expectation Values of xsm(qs)
The expression ðhq1 i; hq2 iÞ for the position expectation values, as used in Figure 8.7, to describe the evolution of the wave packet in time may be obtained in a straightforward manner using the form of xsm ðqs Þ (here in place of yðq; tÞ), when it is m1 ; m2 ; . . . ; mN l expressed in the q coordinate set. Taking the integral JN to be the n1 ; n2 ; . . . ; nN s coefficients in the expansion of the excited vibrational wavefunction xsm ðq Þ, that is, X m1 ; m2 ; . . . ; mN xsm ðqs Þ ¼ JN ðJ1Þ xln ðql Þ; n ; n ; . . . ; n 1 2 N n we can calculate the position expectation values of xsm ðqs Þ, ðhq1 i; hq2 i; . . . ; hqN iÞ in the system of coordinates fqlm g. To simplify the writing in the subsequent formal manipulations, let us restrict (without loss of generality) to the case of three dimensions N ¼ 3. Then, we have for the first normal mode hq1 i ¼ xsm1 ; m2 ;m3 ðqs Þjq1 jxsm1 ;m2 ;m3 ðqs Þ P m1 ; m2 ; m3 m1 ; m2 ; m3 ¼ J 0 J3 n 1 ; n1 n01 ; n02 ; n03 n1 ; n2 ; n3 n2 ; n02 n3 ; n03 ðJ2Þ xln1 ;n2 ;n3 ðql Þql1 xln01 ;n02 ;n03 ðql Þ ; and analogously for the remaining coordinates ql2 and ql3 . Writing the wavefunctions on the right-hand side of Equation J2 as products of single-mode wavefunctions, we obtain 1=2 1=2 xln1 ;n2 ;n3 ðql Þql1 xln01 ;n02 ;n03 ðql Þ ¼ xln1 ðbl1 ql1 Þql1 xln01 ðbl1 ql1 Þ dn2 n02 dn3L n0 3 : ðJ3Þ
Transitions in Molecular Systems. Hans J. Kupka Copyright Ó 2010 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim ISBN: 978-3-527-41013-2
j Appendix J: Evaluation of the Position Expectation Values of x
s sm(q )
300
Now according to the discussion preceding Equation 3.83, sffiffiffiffiffiffiffiffi 1=2 1=2 1=2 1=2 h qffiffiffiffiffi0 xln1 ðbl1 ql1 Þql1 xln01 ðbl1 ql1 Þ ¼ n1 xln1 ðbl1 ql1 Þxln01 1 ðbl1 ql1 Þ 2v1 qffiffiffiffiffiffiffiffiffiffiffiffiffi 1=2 1=2 þ n01 þ 1 xln1 ðbl1 ql1 Þxln01 þ 1 ðbl1 ql1 Þ :
ðJ4Þ
With the use of these equalities, Equation J2 reduces to hql1 i ¼
h 2v1
1=2 X
pffiffiffiffiffi þ n1 J3
J3
n1 ;n2 ;n3
m1 ; m2 ; m3 n1 ; n2 ; n3
m1 ; m2 ; m3 n1 1; n2 ; n3
p ffiffiffiffiffiffiffiffiffiffiffiffiffi m1 ; m2 ; m3 n1 þ 1 J3 n1 þ 1; n2 ; n3
:
ðJ5Þ
On the other hand, Equations 4.57 and 4.70 are also generally sufficient to enable us to infer ðhq1 i; hq2 i; hq3 iÞ ¼ kð123Þ :
ðJ6Þ
j301
Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect When we described in Chapter 7 the case of decaying states by nonradiative interaction, we included the pseudo Jahn-Teller effect as a supplementary concept. It was observed that the coupling of a triplet T1 state with a higher lying triplet Ti states in the system of diazaphenantrenes represents, in some sense, a pseudo-Jahn–Teller effect, the latter occurring when the energy separation between these states is small or vanishing. As we shall see, some aspects of the pseudo-Jahn–Teller effect bear a close formal relationship to those of the Jahn–Teller effect and to the conical interaction, as described in Chapter 7. We consider three electronic states: j0 , a totally symmetric ground state, and j1 and j2 , the two excited states that differ in symmetry in the group of molecular Hamiltonians, H ¼ Te ðrÞ þ TN ðqÞ þ Uðr; qÞ;
ðK1Þ
which transforms as the totally symmetric representation. The functions j0 ðrÞ; j1 ðrÞ; and j2 ðrÞ are taken in the CA or the Longuet-Higgins basis. To make the discussion simple, we denote the state j0 ðr; q0 Þ by j0 ðrÞ and the two excited states j1 ðr; q0 Þ and j2 ðr; q0 Þ by j1 ðrÞ and j2 ðrÞ, respectively. Therefore, the functions jk ðrÞ depend only on the electronic coordinates, however, the exact form depends on the choice of q0 (see Section 1.1.3). We shall assume that the vibronic problem arises in the states j1 and j2 . They are therefore determined by the set of coupled Equation 1.20 that is now written explicitly as X TN xj ðqÞ þ Ujk xk ðqÞ ¼ Exj ðqÞ; j; k ¼ 1; 2; ðK2Þ k
where
and
D E ð Ujj ¼ Ej þ jj ðrÞjDU jjj ðrÞ ¼ drjj ðrÞ½Te ðrÞ þ Uðr; qÞjj ðrÞ D E ð Ujk ¼ jj ðrÞjDU jjk ðrÞ ¼ dr jj ðrÞ½Te ðrÞ þ Uðr; qÞjk ðrÞ;
Transitions in Molecular Systems. Hans J. Kupka Copyright 2010 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim ISBN: 978-3-527-41013-2
ðK3aÞ
j 6¼ k:
ðK3bÞ
j Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
302
The vibrational functions x0 ðqÞ of the ground state are determined by ½TN ðqÞ þ U00 ðqÞx0 ðqÞ ¼ E0 x0 ðqÞ;
ðK4Þ
since we have assumed that the term U0k ðqÞ may be neglected. Following the customary procedure, U00 ðqÞ becomes after a suitable choice of coordinates qm ! X q2 U U00 ðqÞ ¼ E0 þ q2m : qq2m m q0
This x0 ðqÞ is simply a product of harmonic oscillator functions each depending on one qm . For further consideration, we write Equation K2 as a matrix equation 0
0
0
H x ¼ Ex ;
ðK5Þ
where 0
H ¼
TN ðqÞ þ
1 1 ½U11 ðqÞ þ U22 ðqÞ 1 þ ½U11 ðqÞU22 ðqÞs3 þ U12 ðqÞs1 ; 2 2 ðK6aÞ
with x ðqÞ 0 1 x ðqÞ ¼ x ðqÞ 2
ðK6bÞ
and 0 ; 1
1 1¼ 0
0 1 s1 ¼ 1 0 ;
1 0 s3 ¼ 0 1 :
ðK7Þ
The sk are the familiar Pauli spin matrices. They obey the commutation relations sk sl sl sk ¼ 2ism or sk sl ¼ sl sk ¼ ism ;
ðK8Þ
with ðk; l; mÞ cyclic ð1; 2; 3Þ:
We here follow a treatment of Fulton and Gouterman [313] and express Equation K5 (see also Ref. [314]) more concisely by introducing a unitary transformation S obeying 0
H ¼ SH S þ ; S ¼ 21=2 ðs1 þ s3 Þ:
It is easy to show that Ss3 S þ ¼ s1
ðK9Þ ðK10Þ
Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
and Ss1 S þ ¼ s3 :
ðK11Þ
This yields the following eigenvalue equation: Hx ¼ Ex;
and eigenfunctions 0
x ¼ Sx ;
ðK12Þ
1 1 H ¼ TN þ ðU11 þ U22 Þ 1 þ ðU11 U22 Þs1 þ U12 s3 : 2 2
ðK13Þ
where
The corresponding solutions (Equation K11) are x1 þ x2 x ¼ 21=2 x x : 1 2
ðK14Þ
The fact that j1 and j2 are of different symmetry guarantee [313], for most molecular point groups, the existence of a Hermitian symmetry operator G having the properties ½G; TN ¼ ½G; U11 ¼ ½G; U22 ¼ ½G; U12 þ ¼ 0;
ðK15Þ
G2 ¼ 1;
ðK16Þ
where ½A; B ¼ AB BA. The properties of G given by (K15) and (K16) together with those of the matrices sk (K8) imply that ½Gs1 ; H ¼ 0;
ðK17Þ
which, in turn, implies that Gs1 may be diagonalized simultaneously with H and ðGs1 Þ2 ¼ 1:
ðK18Þ
From (K18) it follows that the eigenvalues of Gs1 are 1. These properties, as we shall show below, allow the reduction of the matrix eigenvalue Equation K12 to onedimensional form. For such reason, we write Equation K13 in the form H ¼ ½TN þ U0 1 þ Ua s3 þ Us s1 ;
ðK19Þ
where 1 U0 ¼ ðU11 þ U22 Þ; 3
ðK20aÞ
1 Us ¼ ðU11 U22 Þ; 2
ðK20bÞ
Ua ¼ U12 :
ðK20cÞ
j303
j Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
304
It may easily be verified that the relations (K15) provide the relations ½G; TN ¼ ½G; U0 ¼ ½G; Us ¼ ½G; Ua þ ¼ 0;
ðK21Þ
complemented by the equation G2 ¼ 1:
ðK22Þ
The problem of separating the matrix eigenvalue Equation K12 with the condition (K17) and (K18) to two one-dimensional equations is quite straightforward and may be carried out with the aid of the projection operators P þ and P defined as 1 P ¼ ð1 Gs1 Þ: 2
ðK23Þ
This may be seen by observing that the operator (K23) acting on an arbitrary vector 0 00 x ¼ colðx ; x Þ project out eigenstates of Gs1 , that is, Gs1 x ¼ x ; x ¼ P x:
ðK24Þ
Since Gs1 commutes with H, all solution of (K12) can be obtained as either x þ or x. However, the following identities show that the latter contain only one independent component each: 0 0 0 00 00 1 1 G x00 ¼ 1 x þ0 Gx00 ¼ 1 x 0þ Gx 00 ¼ x þ ; Pþx ¼ 2 G 1 x 2 Gx þ x 2 Gðx þ Gx Þ 0 0 00 1 x0 Gx00 1 1 G ¼ ¼ x ; x00 ¼ 1 x Gx P x ¼ 0 00 0 00 2 G 1 x 2 Gx þ x 2 Gðx Gx Þ and Gs1 x
þ
Gs1 x
0 G 1 x0 þ Gx0 1 x0 þ Gx00 ¼ ¼ ¼ xþ ; G 0 2 Gðx0 þ Gx00 Þ 2 Gðx0 þ Gx00 Þ 0 G 1 x0 Gx00 1 ðx0 Gx00 Þ ¼ ¼ ¼ x : G 0 2 Gðx0 Gx00 Þ 2 Gðx0 Gx00 Þ
Hence, one component of x þ may be generated from the other by means of the symmetry operator G. We may, therefore, represent any solution of (K12) in one of the two forms: þ x or x ¼ x : ðK25Þ xþ ¼ Gx þ Gx Indeed, to correct our discussion, we note that 1 0 xþ 1 0 xþ H þ x þ ¼ ½TN þ U0 0 1 Gx þ þ U0 0 1 Gx þ 0 1 xþ þ þ þ Us 1 0 Gx þ ¼ E x ;
Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
which gives us H þ x þ ¼ ½TN þ U0 x þ þ Ua x þ þ Us Gx þ ¼ E þ x þ ;
ðK26aÞ
GH þ x þ ¼ G½TN þ U0 x þ þ GUa x þ þ GUs Gx þ ¼ GE þ x þ :
ðK26bÞ
or
Since the second equation is obtained from the first by multiplying it with G, it is redundant and may be neglected. Similarly, we have H x ¼ ½TN þ U0 x þ U0 x Us Gx ¼ E x :
ðK27Þ
In Equations K26 and K27, we have written E þ and E since, in general, the spectra of H þ and H do not coincide. The curious aspect of these equations resides in the operator G, the symmetry properties of which are given by Equation K21. Thus, we solve the augmented problems (K26) and K27 and choose the eigenfunctions of the original Equation K12 (by inserting Equation K25 into Equation K14) in the form1) x1 1 x þ þ Gx þ ¼ ðK28aÞ x 2 x þ Gx þ 2 or x 1 x Gx 1¼ x 2 x þ Gx : 2
ðK28bÞ
These give the total wavefunctions in the two-state approximation (see Equation 1.19) Y þ ðr; qÞ ¼
1 1 j ðrÞ½x þ ðqÞ þ Gx þ ðqÞ þ j2 ðrÞ½x þ ðqÞGx þ ðqÞ; 2 1 2
Y ðr; qÞ ¼
1 1 j ðrÞ½x ðqÞGx ðqÞ þ j2 ðrÞ½x ðqÞ þ Gx ðqÞ: 2 1 2
ðK29Þ
We shall now discuss the solution of these equations in two extreme cases, which may be solved by ordinary techniques. Case a Us ¼ 0 Under this condition, H þ is equal to H and the energy levels are at least doubly degenerate. We conclude then that x þ ¼ x , which in turn implies that the wavefunctions in these doubly degenerate states are Y¼
1 1 j ðx þ þ Gx þ Þ þ j2 ðx þ Gx þ Þ; 2 1 2
Y¼
1 1 j ðx þ Gx þ Þ þ j2 ðx þ þ Gx þ Þ: 2 1 2
1) In Equation K28, the functions x þ and x are assumed to be normalized to unity.
ðK30Þ
j305
j Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
306
The functions x þ may be found by ordinary techniques, expanding U0 and Ua in terms of normal coordinates, since the operator G in Equation K26a is absent. Case b Ua ¼ 0 In this case that Ua vanishes, it follows from (K21) that G commutes with both Hamiltonians H . Therefore, the solutions x þ and x may be chosen to be eigenfunctions of G with eigenvalues 1. It may be seen from Equations K26–K28 that for solutions Gx þ ¼ þ x þ ;
Gx ¼ x ;
ðK31Þ
we have x2 ¼ 0
and ðTN þ U0 þ Us Þx1 ¼ Ex1 :
The molecular wavefunctions are Y ¼ j1 x1 :
ðK32Þ
Similarly, it may be shown that for solutions Gx þ ¼ x þ ;
Gx ¼ þ x ;
ðK33Þ
we have x1 ¼ 0
and ðTN þ U0 Us Þx2 ¼ Ex2 :
The molecular wavefunctions are Y ¼ j2 x2 :
ðK34Þ
In this case also, the operator G has been removed from the Hamiltonian, so the solution x2 may be obtained by the usual techniques. Equations K26a and K27 give the Hamiltonians for the treatment of vibronic coupling of two electronic states of different symmetry in the harmonic approximation under very general cases, however, special circumstances permit considerably further simplifications. This may be done by writing the Hamiltonians (K26a) and (K27) in the original forms (using the definition given by Equation K20) as H ¼ TN þ
1 1 ðU11 þ U22 Þ ðU11 U22 ÞG þ U12 : 2 2
ðK35Þ
Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
We may now expand the terms Ujk in terms of the symmetry coordinates appropriate to the problem: Ujk ¼ Ek djk þ
X m
ljkm qm þ
1 X jk f qm qn : 2 m;n mn
ðK36Þ
22 In these equations, terms l11 m and lm are nonvanishing for totally symmetric 11 22 and fmn are nonvanishing coordinates only (see Equation 1.30); similarly, terms fmn for qm qn that transform as the totally symmetric representation. The terms l12 m are nonvanishing for coordinates qm having the symmetry of the product j1 j2 (see Equation 1.31). The leading terms for j ¼ k in (K35) are simply the electronic energy E1 and E2 of the states j1 and j2 . Continuing to follow Fulton and Gouterman, we make two physical assumptions: X 1 X 11 22 11 22 ðaÞ ðlm lm Þqm þ ðfmn fmn Þqm qn jE1 E2 j; m 2 m;n
where the qm s extends over the range of nuclear vibrations, X X 12 12 ðbÞ fmn qm qn lm qm : m;n m Assumption (a) is satisfied if the two states j1 and j2 are so similar that any difference in their individual equilibrium configurations and force constants may be neglected. This assumption may be expected to hold in many problems of interest (see, for example, the discussion about the np. --pp. vibronic interaction in DAP at the end of Section 7.2.3). If this assumption fails, the problem becomes considerably more difficult. The second assumption requires that the linear coupling terms dominate over the quadratic ones. For simplicity, we assume further that ðcÞ
l12 m ¼ 0;
ii fmg ¼ 0;
m 6¼ g;
although these assumptions may be relaxed without difficulty. The assumption (c) means that the vibronic coupling occurs in only one of the normal coordinates, the asymmetric vibration mode qg . With this assumption, the Hamiltonians become H ¼ TN þ
1 1X 1X 1 lm qm þ fmn qm qn ðE1 E2 ÞG þ l12 ðE1 þ E2 Þ þ g qg ; 2 2 m 2 m;n 2 ðK37Þ
where 1 lm ¼ ðl11 þ l22 m Þ; 2 m 1 fmn ¼ ðfmn11 þ fmn22 Þ; 2
ðK38Þ
j307
j Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
308
and qg is a nontotally symmetric coordinate. The commutation relations given in (K21) are satisfied in the case of Hamiltonians (K37) by Gqg ¼ qg ; Gqn ¼ qn ;
n 6¼ g;
ðK39Þ
which demonstrates that G reflects qg but leaves the other (totally symmetric) coordinates qm unchanged. Since qg is a nontotally symmetric coordinate, after a suitable transformation (which transforms lm from the expression of the Hamiltonian operator (K37)) the latter may be written as a sum of two commuting operators H0 þ Hg . ! h2 X 0 q2 1X0 1 H0 ¼ þ ln q2n þ ðE1 E2 Þ; 2 2 qqn 2 n 2 n Hg ¼
2 h 2
!
q2 1 1 þ lg q2g ðE1 E1 ÞG þ l12 g qg ; qq2g 2 2
ðK40Þ
where the prime on the summation indicates that the sum is restricted to normal P modes n 6¼ g. H0 is simply a sum of harmonic oscillator Hamiltonians H0 ¼ n Hn , the solution of which is given by the product of eigenfunctions in each mode qn (see Equation 1.50). The vibronic coupling, therefore, manifests itself only in Hg , the eigenvalues of which are now presented by perturbation calculations in two interesting cases. Case a 12 ðE1 E2 Þ l12 g qg This case arises when the states j1 and j2 are nearly degenerate. It represents a pseudo Jahn–Teller effect. In this case, we write 1 Hg ¼ Hg0 ðE1 E2 ÞG; 2
ðK41Þ
where Hg0 ¼
2 2 h q 1 þ lg q2g þ l12 g qg 2 qq2g 2
ðK42Þ
is treated as the unperturbed Hamiltonian and ð1=2Þ ðE1 E2 Þ G is the perturbating term. It is easy to verify that the eigenstates of Hg0 are 1 1 Hg0 xn ðqg þ kg Þ ¼ hvg n þ k ðK43Þ l12 g xn ðqg þ kg Þ; 2 2 g 2 where we have introduced the notation kg ¼ l12 g =lg with lg ¼ vg . The first-order 1 corrections to the energy are given by the quantities 2 ðE1 E2 Þ
xn ðqg þ kg ÞjGjxn ðqg þ kg Þ . To evaluate these matrix elements of the reflection operator G, we note that
Gxn ðqg þ kg Þ ¼ xn ðqg þ kg Þ
ðK44Þ
Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
and
xn ðqg þ kg ÞjGjxn ðqg þ kg Þ ¼ xn ðqg þ kg Þxn ðqg þ kg Þ :
ðK45Þ
0
Substituting ðqg þ kg Þ ¼ q g on the right-hand side of Equation K45, we find
0 0 xn ðqg þ kg ÞjGjxn ðqg þ kg Þ ¼ xn ðq g þ 2kg Þxn ðq g Þ 0 0 n ¼ ð1Þn xn ðq g þ 2kg Þxn ðq g Þ ¼ ð1Þn J1 ; 2D2g ; 0 ; n where J1 is the FC integral given in Equation 8.57 with Dg ¼ ðvg = hÞ1=2 kg being the dimensionless nuclear displacement parameter of the coupling mode. This equation permits us to express the eigenvalues of Hg as 1 1 1 kg l12 Eg ¼ hvg n þ ð1Þn ðE1 E2 ÞexpðD2g ÞL0n ð2D2g Þ: ðK46Þ 2 2 g 2 Figure K.1 illustrates the displaced oscillator potential and indicates the energy levels for E1 ¼ E2 and e ¼ 0:25 and Dg ¼ 0:71, where e is half of the energy gap ¼ ðE1 E2 Þ=2hvg in units of hvg . It is interesting to note that for a coupling between the states j1 and j2 of such size, the energy levels exhibit not a simple pattern, which becomes even more pronounced in the intermediate case, when e Dg .
–
3
+
Energy
– +
2
+ –
1 +
0
–
–3
–2
–1
0
Figure K.1 The displaced potential energy curve and energy levels (in units of h vg ) calculated as function of the dimensionless hÞ1=2 qg for Dg ¼ 0:71. The coordinate ðvg = energy levels for are shown by dotted lines,
1
2
while those for e ¼ 0.25 by solid lines. The levels for ¼ 0 are doubly degenerate. The plus and minus character of the levels for ¼ 0.25 is indicated. After Ref. 313.
j309
j Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
310
The intensities for 0 ! m transition can be obtained rather simply for the case E1 ¼ E2 . If only transitions to the state j1 are allowed, the intensities are proportional to 2 m ; ag ; bg ; jM1 j2 x0 ðqg Þx1m ðqg þ kg Þ ¼ jM1 j2 I1 0
ðK47Þ
where M1 ¼ hj0 jer jj1 i is the electronic matrix element of radiation matter interaction in the dipole approximation and I1 is the intramolecular distribution given in Section 4.2.5. The result is the appearance of a progression in a nontotally symmetric mode. Case b 12 ðE1 E2 Þ l12 g qg This situation occurs for widely separated electronic states and leads to the familiar phenomenon of vibrational borrowing due to asymmetric modes. In this case, we write the Hamiltonian as
þ l12 qg ; Hg ¼ H g g
ðK48Þ
2 2 q 1 1 ¼ h þ lg q2g ðE1 E2 ÞG H g 2 qq2g 2 2
ðK49Þ
where
is the unperturbed Hamiltonian and l12 g qg is the perturbation. The result of letting H g operate on the wavefunction xn ðqg Þ is H g xn ðqg Þ ¼
"
# 1 1 nþ hvg ðE1 E2 ÞG x n ðqg Þ; 2 2
ðK50aÞ
explicitly demonstrating that x n ðqg Þ are eigenstates of H g and 1 1 En ¼ n þ hvg ð1Þn ðE1 E2 Þ 2 2
ðK50bÞ
are the corresponding eigenvalues. The perturbation l12 qg is a linear operator and g
introduces no first-order correction to E g , since xn jqg jxn ¼ 0. For the perturbation l12 g qg in the second-order perturbation calculation, we obtain
X 1 1 2 xn qg xm xm qg xn En ¼ n þ ðl12 Þ : hvg ðÞn ðE1 E2 Þ þ g E 2 2 E m6¼n n
m
ðK51aÞ
Remarking that
xn qg xm ¼
sffiffiffiffiffiffi" rffiffiffiffiffiffiffiffiffiffiffi rffiffiffi# h nþ1 n dm;n þ 1 þ dm;n1 ; vg 2 2
Energy
Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
6
–
5
+
4
–
3
+
2 1
+
0
–
–1
+ –
–2 –3
–2
–1
0
1
2
Figure K.2 The potential energy curves and the energy levels in the region of states j1 and j2 (in units of hvg ) calculated as functions of the dimensionless coordinate ðvg =hÞ1=2 qg
3 for ¼ 2. The dotted lines are for Dg ¼ 0; the solid lines for Dg ¼ 0:71. The plus and minus character of the levels is indicated. After Ref. 313.
we find the second-order correction for En, which is En
2 2 ð1Þn ðl12 ðl12 1 g Þ ð2n þ 1Þ g Þ ¼ nþ : hvg ð1Þn ðE1 E2 Þ
2lg ð142 Þ lg ð142 Þ 2 ðK51bÞ
Assigning the eigenvalues (K51b) correspondingly to the states j1 and j2 (by combining the plus and minus character with the even and odd n number of the levels), they may then be written as ! 2 2 2ðl12 ðl12 1 1 g Þ g Þ ð1Þ þ En ¼ n hvg 1 þ E Þ h v ðE g 1 2 2lg ð12Þ lg ð142 Þhvg 2 2 and Enð2Þ
¼ n hvg 1 þ
2 2ðl12 g Þ
lg ð142 Þhg
!
2 ðl12 1 1 g Þ þ h vg ðE1 E2 Þ : 2 2 2lg ð1 þ 2Þ
ðK52Þ
j311
j Appendix K: Vibronic Coupling Between Two Electronic States: The Pseudo-Jahn–Teller Effect
312
ð1Þ
In this manner, the En levels are in the region of the electronic energy of j1 , while ð2Þ the En levels are in the region of j2 . In the special case of l12 g ¼ 0, the states corresponding to these energy levels, j1 and j2 , are completely uncoupled. The effect of small l12 g term couples the states slightly with a concomitant increase in frequency of the higher energy state and a decrease in that of the lower energy. This result is illustrated in Figure K.2. The final step in our procedure is to determine the relative intensities of electronic transitions from the ground state j0 to the vibrational levels of the states j1 and j2 . The relative intensities of these transitions may be found by calculating the first-order corrections to the states. If the transition to j1 is allowed, the 0–0 transition associated with this level is essentially unchanged in intensity by small value of l12 g [313]. The 0–1 transition, which is in the region of j2 , is allowed with an intensity proportional to 2 2 ðl12 hvg ðV12 vg Þ2 , where hV12 ¼ ðE1 E2 Þ;2) higher transitions are not g Þ jM1 j =2 allowed to this order of approximation. This illustrates the familiar phenomenon of vibrational borrowing by forbidden electronic states. In other words, the 0–1 transition in the region of j2 steals intensity from the allowed transition to the state j1 .3) An extension of this method to the solution of the dimeric case is straightforward and given in a great detail in Ref. [313].
2) It is to be noted that the argument leading to this result need to be restricted to the case that the normal coordinate qg and the corresponding force constant lg are the same in the excited states as in the ground state (no frequency change).
3) For an excellent review of this subject, see 2 Equation 7.21b. The coupling factor Vslg in Equation 7.21b is comparable with 2 2 jM1 j2 ðl12 g Þ =ðV12 vg Þ .
j313
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to classical photodissociation models. J. Chem. Phys., 68, 2066; Heller, E.J. (1978) Photofragmentation of symmetric triatomic molecules: time dependent picture. J. Chem. Phys., 68, 3891. Kulander, K.C. and Heller, E.J. (1978) Time dependent formulation of polyatomic photofragmentation: application to H3þ . J. Chem. Phys., 69, 2439. Katriel, J. (1970) Second quantization and the general two-centre harmonic oscillator integrals. J. Phys. B At. Mol. Opt. Phys., 3, 1315. F€orster, Th. (1948) Zwischenmolekulare Energiewanderung und Fluoreszenz. Ann. Phys., 2, 55. F€orster, Th. (1949) Experimentelle und theoretische Untersuchung des zwischenmolekularen Übergangs von Elektronenanregungsenergie. Z. Naturforsch., Teil, 4a, 321. Davydow, A.S. (1971) Theory of Molecular Excitons, Plenum Press, New York. Powell, R.C. (1970) Thermal and samplesize effects on the fluorescence lifetime and energy transfer in tetracene-doped anthracene. Phys. Rev, B2, 2090. Dexter, D.L. (1953) A Theory of sensitized luminescence in solids. J. Chem Phys., 21, 836. Di Bartolo, B. (1968) Optical Interactions in Solids, John Wiley & Sons, Inc., New York. Powell, R.C. and Blasse, G. (1980) Energy transfer in concentrated systems in Structure and Bonding, vol. 42, SpringerVerlag, Berlin, Heidelberg, New York, p. 43. Orbach, R. (1967) Optic Properties of Ions in Crystals (eds H.M. Crosswhite and H.W. Moss), Interscience, New York, p. 445. Orbach, R. (1975) Optical Properties of Ions in Solid (ed. B. Di Batolo), Plenum Press, New York, p. 355. Holstein, T., Lyo, S.K. and Orbach, R. (1976) Phonon-assisted energy transport in inhomogeneously broadened systems. Phys. Rev.Lett., 36, 891.
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j References
326
312 Miyakawa, T. and Dexter, D.L. (1970)
Phonon sidebands, multiphonon relaxation of excited states, and phononassisted energy transfer between ions in solids. Phys. Rev., B1, 2961. 313 Fulton, R.L. and Gouterman, M. (1961) Vibronic coupling. I. Mathematical treatment for two electronic states.
J. Chem. Phys., 35, 1059; Fulton, R.L. and Gouterman, M. (1964) Vibronic coupling II. Spectra of Dimers. J. Chem. Phys., 41, 2280 314 Witkowski, A. and Moffitt, W. (1960) Electronic spectra of dimers: derivation of the fundamental vibronic equation. J. Chem. Phys., 33, 872.
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Index a accepting modes 32, 33, 36, 37, 54, 69, 75, 99, 101–103, 107, 114, 116, 123, 127, 128, 160, 162, 168, 176, 181, 184, 188, 189, 245 acetophenone 187 activation energy 105, 210 activator 211, 287, 289, 290 addition theorem 57, 60, 61, 65, 226 adiabatic separation – adiabatic approximation 3–5, 14 – adiabatic basis 5, 6 – adiabatic correction 4 – adiabatic potential surface 4, 29 – adiabatic representation 28 – adiabatic states 1, 15, 33 – adiabatic surfaces 17, 18 – crude adiabatic state 29 analytical continuation 69 angular momentum 217 – rotational angular momentum operator 218 anthracene 165 aromatic hydrocarbons 35, 36, 183, 184, 186, 188, 189 asymmetric skeletal vibration 181 atom-diatom scattering 219, 220, 221
b bifurcation point 42 Binet–Cauchy formula 232 body-fixed (BF) reference frame 212 Born–Oppenheimer (BO) basis 1 – BO representation 27 – Born–Huang approximation 4 – Born–Oppenheimer coupling 5, 130 – Born–Oppenheimer state 146 – Born–Oppenheimer wavefunction 180
boundary condition 219–222 Bragg diffraction grating 194 branch cut 135, 143 Bridgman technique 193 butterfly vibration 184
c carbonyl compounds 189 C–C stretch 168 center of mass 1, 217 center of mass (C.M.) 212 Chauchy product 59, 62 chelate rings 170 closed coupled equations 217 closely coupled states 140 [Co(CN)2(tn)2]Cl3H2O complex 155, 166 coherent-state method of Glauber 227 commutation relations 302 compound matrix 86, 96, 238 Condon approximation 28, 111, 112, 226 conical intersections 1, 6, 16–19, 211, 212, 214, 216 contact transformation perturbation operator 228 convolution 60, 65, 226 – convolution form 61 – convolution of one-dimensional distributions 72 Coulomb gauge 277 Cr (III)-alkylamine complexes 188, 190 Cr (III)-amine complexes 187, 188 critical interaction distance 200 critical transfer distance 289 cross-frequency parameters 46, 79, 94, 119, 127, 162, 225 crude BO approximation 7
j Index
328
crude adiabatic electronic wavefunction 180 crude BO wavefunctions 112, 113
– of mode mixing 246 Dyson equation 264
d
e
damping matrix 140 Debye-Waller factor 109 density of states 25, 31, 32, 34, 55, 70, 134, 142, 149, 180, 288 – density of photon states 134, 137 – density of states weighted vibrational overlap factor 112, 123, 126, 226, 181, 182 – density of states weighted with the intramolecular distribution 54 – density of vibronic states 138, 189 – density-of-states weighted ID 188 dephasing process 145, 152 – dephasing time 152 – inhomogeneous dephasing 152, 153 – intramolecular dephasing 150, 151, 165 – pure dephasing T2 processes 145 – pure dephasing time 152 detuning energy 245 deuterons 187, 190 d function 25, 26, 116 – delta Dirac distribution 215 – d-function of Dirac 17, 158 diabatic representation 13, 15, 17 – diabatic basis 15, 16, 18 – diabatic energies 18 – diabatic functions 15 – diabatic states 20 – diabatic surfaces 18 diazaphenantrenes (DAPs) 171 – monoprotonated 2,4-DAP 176 – unprotonated 1,5-DAP, 2,5-DAP, 3,5-DAP 172, 176 diffraction efficiency 195, 196, 208, 210 dihedral angles 165 dipole-dipole coupling 194 – dipole-dipole interaction 147, 199, 200, 205, 290 – phonon-assisted dipole-dipole coupling 198 displaced potential surface model 103 dissociation coordinate 211 doorway states 22, 29 Duschinsky effect 1, 9, 11, 12, 13, 240 – Duschinsky mixing effect 11, 113, 225, 244, 247 – Duschinsky mode mixing 242 – Duschinsky rotation 11, 55, 72, 155, 228, 238 – – matrices 182, 11, 82, 104, 176
effective Hamiltonian 140, 155, 201, 264, 285 – generalized effective Hamiltonian 146, 147 effective temperature 105 energy conservation 112, 181, 189 energy gap law 51, 106 energy transfer 155, 191, 194, 195, 197, 198, 200, 211, 287 – energy transfer to the traps 202 – excitation energy transfer 204 – Forster energy transfer 200 – nonresonant energy transfer 201, 204 – phonon-assisted energy transfer 202, 289, 291 – resonant energy transfer 200, 203, 204, 208, 288, 291 – resonant energy transfer rate 289 – single-step energy transfer 203 ESR spectra 178 Eulers gamma function 257 excess of electronic energy 54 excitation probability densities 208 excited-state geometry 169
f false origins 166, 184 fast vibrational relaxation limit 32 Fermi Golden Rule 26 – Fermi Golden width 24 fix point theorem 126 Fock space 278 Fourier integrals 36, 119, 127 – Fourier transform 247 – Fourier transformation 34, 158, 226 Franck–Condon (FC) factor 21, 29, 138, 225–227 – FC integral 225, 227, 229, 233, 241, 244 – multidimensional FC integrals 228 – polyatomic FC factors 227 – Raman FC factors 245 frequency effect 69
g Gaussian 108 Gaussian distribution 150 – Gaussian integrals 274 – multiple Gaussian integral 231 generalized displacement parameters 126 generalized functions 25, 158, 215
Index generating function (GF) 34, 36, 41, 42, 45, 47, 48, 57, 60, 63, 72, 75, 82, 89, 103, 225, 238, 255 – generating function KZ(t) for the promoting mode(s) 53, 63, 115 – multidimensional GF 93, 228 – promoting mode generating functions 115 – single-mode generating function 35, 49, 103, 117, 122, 157, 158 – two-dimensional generating function 39, 122 grating constant 197, 208, 210 Greens function 21–23, 26, 261, 262 Greens operator 26, 261
h
H2Oþ 155, 211, 212, 218 Hamiltonians 1, 3, 13, 14, 17, 18, 26, 27, 129, 139, 261, 301, 306–308, 310 harmonic restoring force 169 heat bath 52, 161 Hermitian symmetry operator 303 Herzberg–Teller approximation 6, 9 – Herzberg–Teller adiabatic approximation 1, 9 – Herzberg–Teller expansion 180, 182 – Herzberg–Teller mixing 9 homographic transformation 58 hopping mechanism 197
i inert medium 32 in-plane ring deformation mode 176 interactive displacement parameters 91, 93, 94, 176, 233, 238 – reciprocal displacement 96 – – parameters 93, 176, 241 intermediate case 31, 137, 138, 144 intermolecular dephasing 165 internal conversion 21, 142, 144, 145 intersystem crossing 21, 145, 172, 174, 180, 183, 184, 187, 188, 191 intramolecular distribution 36, 55, 108, 188, 225, 310 – multidimensional distributions 70, 92, 190 – multidimensional ID 55, 57, 162, 255 – one-dimensional distribution 57, 60, 79, 168 – one-dimensional IDs 54, 165, 189 – two-dimensional ID 54 – two-dimensional probability distribution 42 invariance of I2 77 – invariance of IN 91
irreversibility 70 irreversible decay 36, 136 isotope effect 190
j Jacobian 211, 217 Jacobi coordinates 212, 213 Jahn–Teller effects 5 – pseudo Jahn–Teller effect 5, 301, 308 – pseudo Jahn–Teller interaction 183
k Kramers–Heisenberg–Dirac (KHD) sum-over state method 247
l Laguerre polynomial 68 Laporte-forbidden d–d and f–f transitions 9 Legendre polynomials 219 Leibnitzs formula 63 level anticrossing-type interference 142 level shift operator 23, 25, 263 – level shift 24 – principal part 24 lHospitals rule 6 lifetime 26, 136, 141, 144, 151, 152, 155, 190, 195–197, 200, 202, 204, 210, 216 – fluorescence decay time 289 – measurements 172, 178, 191 – of triplet state 186 – phosphorescence lifetime 178 – triplet lifetime 179 limit of zero temperature 58 linear interaction terms 69 line shape function for radiative transitions 155 Longuet–Higgins basis 301 Longuet–Higgins space 7 Lorentzians 25, 134, 179 – Lorentzian distribution 51, 158, 181 – Lorentzian function 51 – Lorentzian profile 226 – Lorentzian shape 17 – shape Lorentzian 152
m magnetic induction 277 mirror images 46, 65 minors 86 mixed quadratic interaction terms 97 MNDO geometry optimization 164 [Mo2Cl8]4 246 mode mixing 57, 94, 97, 99, 101, 162, 228, 233, 245
j329
j Index
330
– mode scrambling 161 – mode selection 99 molecular eigenstate (ME) 129, 130, 131, 137–139, 141, 144, 281 molecular point groups 303 multistep migration 155, 191 multivalued function 18
n naphthalene 165, 186, 187, 190 nitrogen heterocyclic compounds 183, 191 nonadiabatic coupling 6, 17, 112, 211, 214 – nonadiabatic interaction 17, 202, 218 – nonadiabatic operator 28 nonbonding electrons 155, 171 nuclear inertia tensor 2
o operation F (flip) 47, 77 operators – annihilation 130 – creation 130 optical interference pattern 194 optical mode 52 out-of-plane coordinate 180, 189 – out-of-plane vibration 184
p parallel-mode approximation 93, 94, 99, 233, 246 partition function 34 Pauli spin matrices 302 pentacene 184, 191, 192, 193, 194, 198, 208, 210 – pentacene guest in p-terphenyl 184 – p-terphenyl-pentacene crystals 195 phase destructive events 152, 210 phosphorescence quantum yield 178, 179 phosphorescence spectra 155, 166, 172, 174, 179, 181 photon numbers 130, 278 point group 16, 17, 82, 165 Poisson distribution 67, 69, 108 polyvalent 58 position expectation values 255, 299 Poynting flux 278 predissociation 155 – 2B2 state of H2Oþ 211 progressional mode 168, 186 projection operators 129, 132, 133, 139, 262 – Feshbach projection formalism 23, 262 promoting mode 32, 33, 35, 36, 48, 49, 53, 101, 105, 107, 115–117, 121–123, 127, 128,
157–160, 160, 166, 176, 181, 184–186, 188, 191, 290, 291 promoting mode factors Kh(t) and Ih(t) 48 The propensity rule for the promoting mode 54 p-terphenyl 166, 192, 198, 200, 210 – crystalline p-terphenyl 192 – monoclinic p-terphenyl 193 – p-terphenyl (PT) crystal 162, 165, 205 – – host crystal 209 – p-terphenyl-pentacene crystals 195 – triclinic p-terphenyl 193
q
q-centroid 33, 112, 115, 121, 123, 125, 126, 127, 128 – q-centroid approximation 111, 112, 113, 131 – q-centroid configuration 126, 128 quadratic interaction terms 58, 69, 106 quantum yield 136 – ISC quantum yield 178
r radiation-matter interaction 130, 310 radiative damping matrix 137, 140 rare earth ions 187 Rayleigh–Schrodinger (RS) perturbation 8 Rayleigh–Schrodinger expansion 113 r-centroid method 112 ReCl62 166 recurrence equations 57, 66, 72, 75, 77, 78, 94, 227, 228, 239, 240, 241, 242 – recurrence formula 65 – recurrence procedure 79, 95 – recurrence relation 59, 76, 94, 238 redshift 211 reduced masses 164, 165, 214, 217, 218 regular sequence of good functions 25 Renner effect 5 residue 135, 136 resolvent operator 261 resonance Raman 225, 246 – Raman scattering 247 – resonance Raman intensities 227 – resonance Raman scattering 246 resonance Raman process 244, 245 resonance Raman spectrum 247 Riemann sheet 134, 135 ring deformational mode 168 – C–C/N–C stretching modes 176 – C–H stretching modes 181, 190 – – N–H stretching modes 181, 189 Robinson–Frosch formula 51 rotation matrix 99, 176, 225, 238
Index
s Schrödinger equation 1, 2, 3, 21, 27 sensitizer 211, 287, 288, 289, 290 separable modes 12, 71, 72 – nonseparable modes 12, 41, 121, 122, 160, 226 – – normal modes 225 sequential two-photon process 247 Shpolskii matrices 32 similarity criteria 29 single-valued function 16 site symmetry 165 skeletal modes 189 small molecule cases 51 small molecule limit 149 small molecules 138 spherical Bessel function 222 spherical harmonic function 219, 220 spherical Neumann functions 222 spin-allowed 185 – spin-forbidden transition 185 spin-orbit interaction 173 – spin-orbit coupling 181, 184 spin relaxation 173 statistical limit 31, 32, 51, 52, 54, 134, 136, 137, 142, 144, 189 Stokes shift 104 – anti-Stokes sidebands 185, 186 – Duschinsky Mixing Effect 244 – Stokes sidebands 185, 186 strong coupling limit 102, 104 – weak coupling limit 104, 106 strongly coupled states 69, 186 – weakly coupled states 69, 70 strongly coupled to medium 108
– torsional levels 166 transient grating decay 195, 196, 204 – transient grating signal 202, 208 transfer velocity 204 transient grating methods 194 transient population gratings 195, 199, 210 transition operator 21, 24, 26 trapping process 197, 198, 203 triplet state population 178 – lifetime of triplet state 186 – triplet lifetime 178 two-state approximation 305
u uncertainty principle 25, 131, 145 unitary transformation 302 univalent 58
v vector potential 130, 277 vibrational borrowing 5, 185, 312 vibrational relaxation 109 vibronic coupling 5, 9, 12, 172, 184 – np-pp vibronic interaction 172 – np-pp vibronic coupling 183 – spin-orbit coupling 173 – vibronically induced transition 159 – vibronic induced optical transitions 50 – vibronic interaction 172, 173 – – energies 189
w wave packet 248, 249, 254, 255 – position of 252 Wigner–Weisskopf approximation 202
t
z
torsional mode 165 – torsional energies 165
zero-temperature limit 42, 51, 97, 126, 128, 179, 189, 228, 242
j331