Springer Series on
At()lDs+I:»laslDas
15
Springer Series on
AtolUs+PlasDI.as Editors: G. Ecker
P. Lambropoulos
I. I. Sobel'man
H. Walther
Managing Editor: H. K. V Lotsch
Polarized Electrons 2nd Edition By J. Kessler
11
Resonance Phenomena in Electron-Atom Collisions By V. I. Lengyel, V. T. Navrotsky and E. P. Sabad
2
Multiphoton Processes Editors: P. Lambropoulos and S. J. Smith
12
3
Atomic Many-Body Theory 2nd Edition By I. Lindgren and J. Morrison
Atomic Spectra and Radiative Transitions 2nd Edition By I. I. Sobel' man
13
Multiphoton Processes in Atoms By N. B. Delone and V. P. Krainov
14
Atoms in Plasmas By V. S. Lisitsa
15
Pulsed Electrical Discharge in Vacuum By G. A. Mesyats and D. I. Proskurovsky
Excitation of Atoms and Broadening of Spectral Lines By I. I. Sobel'man, L. Vainshtein and E. Yukov
16
Atomic and Molecular Spectroscopy 2nd Edition Basic Aspects and Practical Applications By S. Svanberg
Reference Data on Multicharged Ions By V. G. Pal'chikov and V. P. Shevelko
17
Lectures on Non-linear Plasma Kinetics By V. N. Tsytovich
4
5
6
Elementary Processes in Hydrogen-Helium Plasmas Cross Sections and Reaction Rate Coefficients By R. K. Janev, W. D. Langer, K. Evans, Jr. and D. E. Post, Jr.
7
Interference of Atomic States By E. B. Alexandrov, M. P. Chaika and G. I. Khvostenko
8
Plasma Physics 2nd Edition Basic Theory with Fusion Applications By K. Nishikawa and M. Wakatani
9
Plasma Spectroscopy The Influence of Microwave and Laser Fields By E. Oks
10
Film Deposition by Plasma Techniques By M. Konuma
Igor I. Sobel'man Leonid A.Vainshtein Evgenii A.Yukov
Excitation of Atoms and Broadening of Spectral Lines Second Edition With 21 Figures
Springer
Professor Dr. Igor I. Sobel'man Professor Leonid A. Vainshtein Dr. Evgenii A. Yukov P. N. Lebedev Physical Institute, Russian Academy of Sciences, Leninsky Prospect 53, 117924 Moscow, Russia
Series Editors: Professor Dr. Gunter Ecker
Professor Igor I. Sobel'man
Ruhr-Universitat Bochum, Lehrstuhl Theoretische Physik I, UniversitatsstraBe 150, 0-44801 Bochum, Germany
Lebedev Physical Institute, Russian Academy of Sciences, Leninsky Prospekt 53, 117924 Moscow, Russia
Professor Peter Lambropoulos, Ph. D.
Professor Dr. Herbert Walther
Max-Planck-Institut flir Quantenoptik 0-85748 Garching, Germany, and Foundation for Research and Technology Hellas (FO.R.T.H.), Institute of Electronic Structure & Laser (IESL) University of Crete, PO Box 1527, Heraklion, Crete 71110, Greece
Universitat Miinchen, Sektion Physik, Am Coulombwall 1, 0-85748 Garching/Miinchen, Germany
Managing Editor: Dr. Helmut K. V. Lotsch Springer-Verlag, Tiergartenstrasse 17, 0-69121 Heidelberg, Germany
Library of Congress Cataloging-in-Publication Data. Sobel' man. I. I. (lgor'Il"ich), 1927[Vvedenie v teoriiu atoml1j'kh spectrov. English] Excitation of atoms and broadening of spectral lines I Igor I. Sobel' man, Leonid A. Vainshtein, Evgenii A. Yukov.2nd ed. p.em. - (Springer series on atoms + plasma; 15) Inc1udes bibliographical references and index. ISBN 3-540-58686-5 (Berlin: acid-free paper). ISBN 0-387-85686-5 (New York: acid-free paper) I, Cross sections (Nuclear physics) 2. Spectral line broadening. 3. Nuc1ear excitation. 4. Atomic spectroscopy. l. Va1nshte1n, L. A. (Leonid Abramovich), 1928-. ll. lUkov, E. A. (Evgeni1 Aleksandrovich), 1945-. Ill. Title. IV. Series. QC794.6.C7S62 I 3 1995 539.7'54-dc20 95-211 CIP The first edition appeared as Springer Series in Chemical Physics, Vol. 7
ISBN 3-540-58686-5 Springer-Verlag Berlin Heidelberg New York This work is subject to copyright. All rights are reserved, whether the whole or part of the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation. broadcasting, reproduction on microfilms or in any other way, and storage in data bank.s. Duplication of this publication or parts thereof is permitted only under the provisions of the German Copyright Law of September 9, 1965, in its current version, and permission for use must alw'ays be obtained from Springer-Verlag. Violations are liable for prosecution under the German Copyright Law. © Springer-Verlag Berlin Heidelberg 1981, 1995 The use of general descriptive names, registered names, trademarks, etc. in this publication does not imply, even in the absence of a specific statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. Typesetting: Macmillan India Ltd., Bangalore, India Production: PRODUserv Springer Produktions-Gesel1schaft, Berlin SPIN 10089022 54/3020 - 543 2 I 0 - Printed on acid-free paper
Preface to the Second Edition
In this new edition - as in the first one of 1981 - the main goal is to present the theory of elementary processes responsible for the excitation and formation of atomic spectra. No attempt has been made to give a systematic and detailed treatment of the general theory of atomic collisions. Instead, stress is placed on efficient and comparatively simple approximate methods for the calculation of cross sections and rate coefficients. New results of importance and new understanding of many problems have appeared in recent years and require a significant revision of the original book. The formulas for cross sections given in Chaps. 2 and 3 are derived and represented using the unified approach which is symmetrical with respect to orbital and spin quantum numbers. This allows us to give the final results in a more general form which is simpler and more convenient for computer programming. Chapter 4 in which the collisions between heavy particles are considered, is slightly simplified and corrected. The references to recent sources and reviews on the subject are given. The approximation of cross sections and rate coefficients by analytic formulas (Sect. 5.1) is considerably changed in this edition. All the numerical data given in Chap. 6, except Tables 6.2 and 6.3, are new. They have been calculated using the updated version of the computer code ATOM, which has substantially been extended and corrected during recent years. Chapter 7 devoted to the broadening of spectral lines is ~lightly revised. In addition, references are added which communicate the progress in the field. The authors are very grateful to Dr. Helmut Lotsch of Springer Verlag for encouragement and advices. Moscow, April 1995
1 Sobelman L. Vainshtein E. Yukov
Preface to the First Edition
New applications of atomic spectroscopy in laser physics, laser spectroscopy, laser frequency and wavelength measurements, plasma physics, astrophysics, and some other related problems have been developed very intensively in the last years. As a result, the approximate methods of calculation of the transition probabilities and cross sections necessary for all these applications have become of vastly increased importance. At the same time, some new problems have arisen in the theory of spectral line broadening such as the shape of nonlinear resonances in the spectra of gas lasers, interference effects, and some other problems connected with various spectroscopic methods of plasma diagnostics. This book is devoted to the systematic treatment of the theory of the elementary processes responsible for the excitation of atomic spectra and the theory of spectral line broadening. The choice of problems is significantly different from that traditional for books on the theory of atomic collisions. The main goal of the book is to present the most efficient and useful of comparatively simple approximate methods for the calculation and estimation of cross sections. Numerous tables containing the results of approximate cross section calculations for the most important elementary processes are included in the book. Comprehensive presentation of the theory of atomic collisions is out of the scope of this book and can be found elsewhere. However, the fundamentals of the general theory of collisions which are necessary for formulation of approximate methods are given in Chapter 2. In dealing with the theory of spectral line broadening special attention is paid to the general approach to the problem based on the method of density matrix and quantum kinetic equation. This approach is of interest for some modem applications of broadening theory e.g. such as high-resolution laser spectroscopy. We consider this book as complementary to I. Sobelman's Atomic Spectra and Radiative Transitions (first volume of present book-series). We wish to express our sincere gratitude to I.L. Beigman, who helped us to prepare Sects. 3.5,5.4, to L.P. Presnyakov, who assisted us in Sects. 3.4,4.1-3. We are grateful also to Prof H.-W. Drawin, Prof. H.R. Griem, Dr. V.S. Lisitsa and Prof. J.-P. Toennies, who have read the manuscript, for many valuable comments. In conclusion we are particularly grateful to H.W. Drawin, H. Griem and J.P. Toennies for the final reading of the manuscript and their helpful suggestions. Moscow, April 1980
l. Sobelman L. Vainshtein E. Yukov
Contents
1 Elementary Processes Giving Rise to Spectra . .................. . 1.1 Cross Sections and Rate Coefficients . . . . . . . . . . . . . . . . 1.2 Populations of Atomic Levels in a Plasma; Rates of Direct and Reverse Processes . . . . . . . . . . . . . . . . . . . . . . . . . . 1.2.1 Thennodynamic Equilibrium. . . . . . . . . . . . . . . . . . 1.2.2 Rates of Direct and Reverse Processes. . . . . . . . . . . 1.2.3 The Simplest Model. . . . . . . . . . . . . . . . . . . . . . . . 1.2.4 Coronal Limit . . . . . . . . . . . . . . . . . . . . . . . . . . . .
....... . . . . .
. . . . .
. . . . .
. . . . .
. . . . .
.. .. .. .. ..
3 3 5 6 7
2 Theory of Atomic Collisions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..
9
2.1 Fundamentals of Scattering Theory . . . . . . . . . . . . . . . . . . . . . . .. 2.1.1 Elastic Scattering in a Central Field. . . . . . . . . . . . . . . . . . .. 2.1.2 Wave Functions I/It,I/I; . ........................... 2.1.3 Quasi-Classical Approximation . . . . . . . . . . . . . . . . . . . . . .. 2.1.4 Inelastic Scattering . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2 Theory of Electron - Atom Collisions. . . . . . . . . . . . . . . . . . . . . .. 2.2.1 General Fonnulas for Cross Sections ................... 2.2.2 S-matrix and Collision Strength. . . . . . . . . . . . . . . . . . . . . . . 2.2.3 Radial Equations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.4 Integral Radial Equations . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.2.5 Polarization Potential . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3 First-Order Approximation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3.1 General Fonnulas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2.3.2 List of Fonnulas for (J and Q-Factors . . . . . . . . . . . . . . . . . .
9 9 11 13 15 17 17 22 23 26 27 29 29 31
3 Approximate Methods for Calculating Cross Sections. . . . . . . . . . . . . . 36 3.1 Born Approximation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.1.1 Collisions of Fast Electrons with Atoms; Multipole Expansion . 3.1.2 Bethe Fonnula . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.1.3 Brief Description of Born Cross Sections ................ 3.1.4 Ionization and Three-Body Recombination ............... 3.2 Some Refinements of the Born Approximation ................ 3.2.1 Distortion of Incident and Scattered Waves; Excitation of Ions. 3.2.2 Allowance for Exchange . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.2.3 Normalization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.2.4 Concluding Remarks: Generalized Born Approximation ......
36 36 40 41 45 47 48 50 54 57
VIII
Contents
3.3 More Accurate Methods of Calculation of Excitation Cross Sections 3.3.1 Transitions Via Virtual States. . . . . . . . . . . . . . . . . . . . . .. 3.3.2 Use of the K matrix .. . . . . . . . . . . . . . . . . . . . . . . . . . .. 3.3.3 Polarization Potential. . . . . . . . . . . . . . . . . . . . . . . . . . . .. 3.3.4 Close-Coupling Method. . . . . . . . . . . . . . . . . . . . . . . . . .. 3.4 Excitation of Highly Charged Atoms. . . . . . . . . . . . . . . . . . . . .. 3.4.1 Coulomb Green's Function. . . . . . . . . . . . . . . . . . . . . . . .. 3.4.2 Potential and Resonance Scattering . . . . . . . . . . . . . . . . . .. 3.4.3 Discussion and Examples. . . . . . . . . . . . . . . . . . . . . . . . .. 3.5 Transitions Between Highly Excited Levels. . . . . . . . . . . . . . . . .. 3.5.1 Born Approximation. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 3.5.2 Transitions Between Highly Excited Levels in the Quasi-Classical Approximation . . . . . . . . . . . . . . . . . . . . .. 3.5.3 Transitions Between Adjacent Levels An = 1 . . . . . . . . . . ..
58 59 62 63 64 66 68 69 72 74 74
4 Collisions Between Heavy Particles. . . . . . . . . . . . . . . . . . . . . . . . .. 4.1 ImPflct-Parameter Method. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 4.1.1 General Formulas. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 4.1.2 Two-State Approximation. . . . . . . . . . . . . . . . . . . . . . . . .. 4.2 Transitions Caused by a Multipole Interaction. . . . . . . . . . . . . . .. 4.2.1 Two-State Approximation. . . . . . . . . . . . . . . . . . . . . . . . .. 4.2.2 Two-Levels and Rotating-Axis Approximations. . . . . . . . . .. 4.2.3 Treatment of the Coulomb Repulsion of Nuclei. . . . . . . . . .. 4.3 Charge Exchange .................................... 4.3.1 Special Features of Charge Exchange Processes. . . . . . . . . .. 4.3.2 Resonance Charge Exchange ........................ 4.3.3 Contribution of Inner Shells. . . . . . . . . . . . . . . . . . . . . . .. 4.3.4 Charge Exchange in the Case of Multicharged Ions. . . . . . ..
88 88 88 90 93 93 98 100 101 101 102 103 106
5 Some Problems of Excitation Kinetics. . . . . . . . . . . . . . . . . . . . . . .. 5.1 Rate Coefficients for Elementary Processes in a Plasma. Approximation of Cross Sections and Rate Coefficients by Analytic Formulas ........................... ; . . . .. 5.1.1 Excitation of Atoms and Ions. . . . . . . . . . . . . . . . . . . . . .. 5.1.2 Ionization. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 5.1.3 Recombination.................................. 5.1.4 Semiempirical Formulas for the Rates of Excitation, Ionization and Dielectronic Recombination . . . . . . . . . . . . .. 5.2 Dielectronic Recombination. . . . . . . . . . . . . . . . . . . . . . . . . . . .. 5.2.1 Electron Capture and Underthreshold Resonances (Simplified Model) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 5.2.2 General Case. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 5.2.3 Formulas for Autoionization Probability ...... '. . . . . . . . ..
108
80 83
108 108 112 113 116 120 120 124 126
Contents 5.2.4 Some Inaccuracies of the Simplified Model. . . . . . . . . . . . .. 5.2.5 Numerical Calculations and Analytical Approximation Formulas ........................... 5.3 Satellites of Resonance Lines in Spectra of Highly Charged Atoms. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 5.3.1 Excitation by Means of DR ....................... , 5.3.2 Direct Inner-Shell Excitation. . . . . . . . . . . . . . . . .. ..... 5.4 Populations of Excited Levels in a Plasma. . . . . . . . . . . . . . . . .. 5.4.1 Populations of the Hydrogen Levels at Low Plasma Density.. 5.4.2 Intermediate Density. Collisional-Radiative Model of a Plasma 5.4.3 Quasi-Stationary Approach for Hydrogen. . . . . . . . . . . . . .. 5.4.4 Hydrogenlike Ions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 5.4.5 Population Densities of Highly Excited Levels at High Density; Steady-Flow Regime. . . . . . . . . . . . . . . . . . . . . .. 6 Tables and Formulas for the Estimation of Effective Cross Sections. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 6.1 Tables of Numerical Results. . . . . . . . . . . . . . . . . . . . . . . . . . .. 6.1.1 Methods of Calculations and Survey of the Tables . . . . . . .. 6.1.2 Excitation Cross Sections for Neutral Hydrogen. Transitions no - nl . . . . . . . . . . . . . • . . . . . . . . . . . . . . . . 6.1.3 Born Cross Sections Calculated in the Bates - Damgaard Approximation for Atomic Wave Functions ............. 6.1.4 Normalized Cross Sections for Specific Atoms and Ions. . . .. 6.1.5 Transitions Between Closely Spaced Levels . . . . . . . . . . . .. 6.1.6 Ionization Cross Sections . . . . . . . . . . . . . . . . . . . . . . . . .. 6.1. 7 Dielectronic Recombination Rate Coefficients . . . . . . . . . . .. 6.2 Formulas Defining the Angular Factors ..................... 6.2.1 Rules for the Addition of Cross Sections ............... 6.2.2 LS Coupling; Qk for Transitions between Levels LSJ ..... , 6.2.3 LS Coupling; Qk for Transitions between Terms LS . . . . . .. 6.2.4 j/ Coupling. . . . . . . . . . . . . . . . . . . . . . . . ........... , 6.3 3nj Symbols and Fractional Parentage Coefficients. . . . . . . . . . . .. 7 Broadening of Spectral Lines .............................. 7.1 Model of a Classical Oscillator . . . . . . . . . . . . . . . . . . . . . . . . .. 7.1.1 Formulation of the Problem ........................ 7.1.2 Impact Broadening ............................... 7.1.3 Quasi-Static Broadening ........................... 7.1.4 Relationship and Limits of Applicability of the Impact and Quasi-Static Approximations. . . . . . . . . . . . . . . . . . . . . . .. 7.1.5 Doppler Effect. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ... 7.1.6 Convolution of the Doppler and Lorentzian Distributions ....
IX 127 130 130 130 134 136 137 140 141 148 150
154 154 1S4 157 158 203 218 218 223 225 225 225 227 229 231 237 237 237 239 241 242 245 250
X
Contents 7.2 General Theory of Impact Broadening . . . . . . . . . . . . . . . . . . . .. 7.2.1 Density Matrix Method in the Quasi-Classical Approximation. 7.2.2 Degeneracy of Levels ............................. 7.2.3 Quantum Theory ................................ 7.2.4 Quantum Kinetic Equation Method ................... 7.2.5 Absorption Spectrum . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 7.2.6 Interference Effects: Narrowing of Spectral Lines .......... 7.3 Broadening of Lines of the Hydrogen Spectrum in a Plasma ...... 7.3.1 Preliminary Estimates. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.3.2 Ion Broadening: Holtsmark Theory ................... 7.3.3 Correction for Thermal Motion ...................... 7.3.4 Electron Broadening. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 7.3.5 Combined Effect of Electrons and Ions ................. 7.3.6 New Approaches to the Theory of Stark Broadening ....... 7.3.7 Highly Excited States ............................. 7.4 Line Broadening of Nonhydrogenlike Spectra in a Plasma ....... 7.4.1 Preliminary Estimates. . . . . . . . . . . . . . . . . . . . . . . . . . . .. 7.4.2 Electron Broadening .............................. 7.5 Broadening by Uncharged Particles . . . . . . . . . . . . . . . . . . . . . .. 7.5.1 Perturbation by Foreign Gas Atoms (Van der Waals Interaction) . . . . . . . . . . . . . . . . . . . . . . .. 7.5.2 Self-Broadening ................................. 7.6 Spectroscopic Methods of Investigating Elastic Scattering of Slow Electrons . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 7.6.1 Perturbation of Highly Excited States .................. 7.6.2 Fermi Formula ................................ ,
251 251 256 259 263 268 269 273 273 274 279 279 283 284 284 286 286 286 289 289 291 293 293 296
References. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 297
List of Symbols . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 306 Subject Index. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 308
1 Elementary Processes Giving Rise to Spectra
In this chapter, the most important elementary processes responsible for the excitation and ionization of atoms and ions are listed, and their relative role in various plasmas is briefly discussed. Throughout this book, fr is the nuclear charge, Z is the ion charge, and z is the charge of atomic core, i.e., the charge of the atom or ion without the optical electron. For a neutral atom z = 1; for a singly ionized atom, z = 2, and so on. An ion with charge Z = z - 1 will be denoted XZ • We shall usually use the word "atom" to mean both the neutral atom with z = 1 and ions with z > 1. As a, rule plasma is supposed to be optically thin.
1.1 Cross Sections and Rate Coefficients The intensity of the spectral line corresponding to the transition from the level k to the level i in an atom Xz is given by (1.1.1) where A~), Wki, are the probability and frequency of the transition, respectively, N~z) is the number of atoms Xz in the level kper unit volume, and {" is Planck's constant divided by 2n. Usually electrons play the main role in excitation ,and ionization processes in plasmas. Interaction with heavy particles, (protons and ions) is important only for transitions between levels with very small energy splitting and also in some cases of transient plasma. The processes of main interest are the following: Excitation and deexcitation: (1.1.2) where the asterisk denotes the excited state. Ionization and three-body recombination:
Xz + e +:t Xz+l
+e +e.
(1.1.3 )
Radiative ionization and recombination:
Xz
+ {"w +:t Xz+l + e.
(1.1.4)
Dielectronic recombination and autoionization:
Xz+1
+e
+:t X;*
-+
X; +{"w .
I. I. Sobel'man et al., Excitation of Atoms and Broadening of Spectral Lines © Springer-Verlag Berlin Heidelberg 1995
(1.1.5)
2
1 Elementary Processes Giving Rise to Spectra
Free-free emission and absorption:
Xz + e +2 Xz
+ e + hOJ .
(1.1.6)
Emission and absorption in spectral line:
X;
+2Xz +hOJ.
(1.1.7)
Each of the processes (1.1.2-7) is a pair of direct and reverse reactions. The probabilities (cross sections) of such processes are connected by simple formulas (see Sect. 1.2). All these processes can be separated into two groups, radiative [processes (1.1.4,6, 7)] and nonradiative [processes (1.1.2,3 )]. In the case of dielectronic recombination (1.1.5) there are two stages: firstly, the nonradiative attachment of an electron and the excitation of the ion takes place; then there are two possibilities, nonradiative decay (autoionization), or radiative transition into a "stable" state below the ionization limit. This latter process provides the net recombination. The number of radiative transitions (1.1.7) per second for one atom X; is the transition probability Aki[s-'], which does not depend on the plasma characteristics. ' In the case of processes (1.1.2-6) the number of excitations suffered by one atom or ion per second is proportional to the electron density Ne and the velocity of the electron, v, W
= Neva [s-'],
(1.1.8)
where a [cm2 ] is the excitation cross section. If the electrons in a plasma have an energy distribution ~(e), i.e., the number density of electrons in the energy interval (e, e + de) is dNe = Ne~(e)d~,
(1.1.8) has to be rewritten in the form W = Ne(va) , 00
(va)
=
I
va(~)~(~)d~.
(1.1.9)
.1E
Here LJE is the threshold energy of excitation, and (va) is called the excitation rate coefficient (for one atom X z and unit electron density). The same definition is used for cross sections of other processes, in which there are two particles in the initial and final states. Deexcitation (1.1.2), and radiative ionization and recombination (1.1.4) are processes of this kind. For example, the probability of radiative ionization is 00
Wv =
I
Nwca(OJ)dOJ,
Ez/" 1 The
radiative transition probabilities were discussed in detail in [1.1].
1.2 Populations of Atomic Levels in a Plasma
3
where N w is the photon density at frequency w, and Ez is the threshold ionization energy. If there are three particles in the final state, the energy can be arbitrarily distributed between them. For transitions with a definite energy for one of the particles, the cross section can be defined in a similar way, but it should have the dimensions of cm2 erg- 1 instead of cm2 . The cross section of free-free emission (1.1.6) and the "differential cross section" of ionization (1.1.3) are examples. The total ionization cross section i.e., differential cross-section integrated over the energy of the ejected electron, is of most interest in applications. This cross section is defined as 8-Ez
O"i($) $'
=
J
O"j($;$',$")d$',
o
+ $" = $
(1.1.10)
- Ez ,
where $' and $" are the energies of the ejected and scattered electrons. One can see that the dimensions of the ionization cross section (1.1.10) are cm2 • In some cases there are three particles in the initial state of the reaction: the ion X z and two electrons (three-body recombination) or the ion, an electron, and a photon (free-free absorbtion). Here the transition probability is proportional to the fluxes of both particles. For example, for three-body recombination we have
Wr =N;Kr Kr
= JJ V1V2 ff($J)ff(C2 )O"r($\,C2; C)dC 1 d$2
(1.1.11)
The dimensions of O"r in this case are [cm4 s]. The case of dielectronic recombination will be discussed in Sect. 5.2.
1.2 Populations of Atomic Levels in a Plasma; Rates of Direct and Reverse Processes In this section we discuss briefly the simplest cases of level populations distribution in a plasma, in order to show in which way the populations are linked with the cross sections of elementary processes. Our consideration is confined to the case of homogeneous unifonn and stationary plasmas. A more detailed treatment of level populations in a plasma is given in Sect. 5.4 (see also the review article by Drawin in [1.2], where transient phenomena are also discussed).
1.2.1 Thermodynamic Equilibrium If some volume of plasma is in thennodynamic equilibrium, the following distributions are valid.
4
1 Elementary Processes Giving Rise to Spectra
i) Maxwell distribution of energies of free electrons: dNe = NeffM(8)dtf,
ffM(8) = 2n- I/2 T-3/2tf l / 2 exp( -tf/T) ,
(1.2.1)
where T is the electron temperature in energy units (1 eV = 11605 K 8066 em-I). ii) Boltzmann distribution of atoms over energy levels Ek Nk
gk . = -exp (-PkO) , !Yo go
PtO =
AT
Ek -Eo T '
=
(1.2.2)
where gk and go are statistical weights of the levels k and o. iii) Saha distribution of atoms over degrees of ionization: (1.2.3)
S= 2
T ( m ) 2nli,2
3/2
z3
_I
Ne
= 4n3/2 •
£>3/2
u
a~Ne '
(1.2.4)
where Ez is the ionization energy of the atom Xz, e = T/z2Ry is the temperature in Rydberg units (1 Ry=13.6eV=I57894K), ao = 1i,2/me'l = 0.529· lO- scm is the Bohr radius, and gz is the partition function for atom Xz: gz = Ekg~Z) exp( -PkO).
In fact PkO ~ 1 for all levels with principal quantum number different from that of the ground state. The three distributions (1.2.1-3) are wholly determined by the plasma density Ne and temperature T. The factor S in (1.2.3) corresponds to the statistical weight of free electrons; one can see that usually S ~ 1. In cool plasmas only neutral atoms XI are present. With increasing temperature, the density of ions N(z)(z > 1) increases up to a maximum value and then decreases due to the further ionization Xz --+ Xz+ I. SO atoms Xz predominate in a plasma only in the temperature interval Tz-I ~ T ~ Tz, where Tz is the temperature at which N(z+l) = N(z). From (1.2.3) we obtain
i
= In
(g~:1
.S) ~
l.
(1.2.5)
For Nc = 1013 - 1017 , Ez/T ~ 20. Thus the density of atoms X z is large enough only when T ~Ez. Since for most levels the excitation energies EkO are of the order of Ez , according to (1.2.2) populations of excited levels are very low compared to the density of atoms in the ground state. For highly charged atoms (in fact for z ~ 4) important exclusion from this rule apply to the levels no I with the same principal quantum number no as the ground
1.2 Populations of Atomic Levels in a Plasma
5
state. The spacing of the levels nolo and nol is of the order of AElol '" Ez/z, and for high z, Piol < 1.
1.2.2 Rates of Direct and Reverse Processes At thermodynamic equilibrium, detailed balance holds for any pair of collisional processes that are inverse to each other. Let us consider a pair of atomic levels denoted by j and k. According to the principle of detailed balance the rate of collisional excitation of the j-k transition is equal to the rate of collisional deexcitation,
NjNe(vUjk}
= NkNe(VUkj} .
(1.2.6)
Using (1.2.2) we obtain
gj(VUjk} = gk(VUkj} exp (-P),
P = AE/T
(1.2.7)
In the case of ionization, the same argument gives (1.2.8) Here Kr = ((V\V2Ur}) is the rate coefficient of three-body recombination. Equations (1.2.7, 8) do not include the level populations and consequently they do not depend on the existence of thermodynamic equilibrium. It is only necessary that the energies of the electrons have a Maxwellian distribution with temperature T. We shall now derive the formula connecting the cross sections of excitation and deexcitation. Equation (1.2.7) can be rewritten in the form
or
This equation has to be true for any value of T. Hence it follows that
gj(8 + AE)ujk(8 + AE) = gk8 u(8).
(1.2.9)
This equation is usually called the Klein - Rosseland formula. In the particular case 8~AE, it reduces to the simple equality gjUjk = gkUkj. Equation (1.2.9) does not depend on any particular characteristics of the plasma; thus it provides the general relation between excitation and deexcitation cross sections. A similar
6
1 Elementary Processes Giving Rise to Spectra
relation can be obtained for the recombination cross section and the differential cross section of ionization. To connect the rates of radiative ionization O"iv and recombination O"rv, it is convenient to consider the atom to be in total thermodynamic equilibrium with the plasma and blackbody radiation. Then we obtain, recalling that C denotes the speed of light in vacuum, gz(CO"iv)
=2(
mT 2nl,}
)3/2 gz+IKv .
(1.2.10)
Here (CO"iv) is the average over frequencies of the radiation field, and Kv = (vO"rv) is the average over electron energies. By the method similar to that used in deriving the formula (1.2.9), we find gz • q 20"i.{W)
hw
=
tff
= gz+l
• k 2 • O"r.{tff),
+ Ez ,
(1.2.11)
where q and k are the wave numbers of the photon and electron respectively. Equation (1.2.11) can be rewritten in the form gZO"iv(W)
=
2mc 2tff h 2w2 gz+IO"rv(tff).
( 1.2.12)
Formulas (1.2.11,12) are known as the Milne formulas.
1.2.3 The Simplest Model Thermodynamic equilibrium takes place for sufficiently high densities Ne . For moderate or low densities, the thermodynamic distributions (1.2.2, 3) do not hold; nor does the relation (1.2.6). Under these conditions the level population depends on the balance of all processes of excitation, radiation and so on. The general solution of the level-populations problem is very difficult because one has to consider an infinite set of equations including all levels and processes. In the general case, the level populations differ greatly from those in thermodynamic equilibrium. However the distribution of the energies of the free electrons is as a rule almost Maxwellian. We shall suppose below that the Maxwellian distribution (1.2.1) as well as the formulas (1.2.7,8) hold. To provide a qualitative description of the transition from thermodynamic distribution at high density to other distributions at intermediate and low density, we consider the simplest model including collisional excitation j - t k and deexcitation k - t j, the radiative decay of the upper level k to the lower level j, and also the radiative decay of the upper level k to some other levels (i.e., we assume Ak ?: Akj)' The equation of balance will have the form NjNe(VO")k)
= NkNe (VO"k)) + NkAk ,
1.2 Populations of Atomic Levels in a Plasma
7
where Ak = Ln Akn is the total probability of radiative decay from level 2. Using (1.2.7) we obtain Nk = gk • exp ( - I1kj ) Nj gj 1 +R
(1.2.13 )
Equation (1.2.13) gives the level population in the framework of the two-level model for an arbitrary electron density N e • The factor R describes the deviation from the thermodynamical limit. It can be shown that (vakj) does not depend strongly on T so the main temperature dependence is given by the factor exp( - I1kj), which is the same as in the Boltzmann formula. If the level k is the ionization limit we obtain the equation for ionization equilibrium. In the case of ionization equilibrium one has to consider three recombination processes: three-body (which is proportional to N;), radiative, and dielectronic (both of which are proportional to Ne ). We thus obtain the equation (1.2.14)
(1.2.15) where K r , Kv and Kd are the rate coefficients of three-body, radiative, and dielectronic recombination. If R ~ 1 in (1.2.13) or (1.2.14) the ratios Nk/Nj and N(z+l)/N(z) are strongly dependent on the cross sections of atomic translations in contrast to the case of thermodynamical equilibrium. 1.2.4 Coronal Limit
Let us now consider the case which is the opposite limit to the thermodynamical distributions, namely the low-density limit. This condition holds very well in the solar corona, where the electron density (Ne ~ 108 - 109 cm- 3 ) is much less than in any laboratory plasma. For this reason the low-density limit is called the coronal limit. In the limit Ne ----+ 0, using (1.2.7) again, we obtain Nk Nj
(vajk) Ak
= Ne - - .
(1.2.16)
The intensity of the spectral line due to the k-n transition is lkn
Akn . Ak
= NjNe(vajk)hw-
(1.2.17)
The ratio Akn/Ak is called the branching ratio. In the absence of branching, when only one radiative transition is possible, Akn = Ak, and the intensity does not
8
1 Elementary Processes Giving Rise to Spectra
depend on the transition probability. This is an important feature of the coronal limit. According to (1.2.13) the coronal limit is applicable at electron densities ( 1.2.18) As will be shown below Ak ex LJE2 ex z4, (vO') ex LJE- 3/2 ex z-3, so that Ne* ex LJE7/2 ex z7. At z = 1 Ne* ~ 10 16 cm- 3 , at z ~ 10 Ne* ~ 1023 cm- 3 • In other words in a high-temperature plasma with highly charged atoms, the coronal limit usually holds at least for the levels with allowed radiative decay to the ground state. In laboratory plasmas for densities greater than 10 14 cm3 the metastable levels can be collisionally coupled with other levels. In the solar corona (Ne ~ 109 cm- 3 ) even for metastable levels the coronal limit usually holds. Similarly, from (1.2.14,15) we obtain the equation for ionization equilibrium in the coronal limit:
(VO'i) Kv
+ Kd
( 1.2.19)
The ionization degree in this case does not depend on N e , in contrast to the case of thermodynamical distribution.
2 Theory of Atomic Collisions
In this chapter the fundamentals of the general theory of electron collisions with atoms and ions are considered. The treatment begins with the simplest case of scattering in a central field. The quasi-classical (impact parameter) approximation for scattering phases 1](p) and their connection with quantum phases 1]). are obtained. Formulas expressing the cross sections in terms of unitary S matrices are given. The general system of integrodifferential equations for the problem of electron collision with a complex atom is dealt with (Sect. 2.2). These equations are reduced to the integral radial equations with the polarization potential, which simplifies the formulation of different approximate methods of calculation. In the last section of the chapter, the first-order approximation is considered. The final formulas are given which are used further in approximate calculations. In this book the main interest lies in formulation and analysis of the approximate calculation methods for excitation and ionization cross sections. For this reason, only those questions of the collision theory are touched upon which are quite necessary for this purpose. Comprehensive representation of the general collision theory can be found in modem textbooks such as [2.1-3].
2.1
Fundamentals of Scattering Theory
2.1.1
Elastic Scattering in a Central Field
The scattering of particles is usually described by the ratio of the number of particles scattered in an element of solid angle dO per second to the flux density of incident particles, i.e., to the number of particles incident on 1 cm2 per second. This ratio da is measured in cm2 , and is identified as the differential scattering cross section. Let the particles fall on the scattering center along the z axis with velocity v. The free motion of particles is described by the wave function tfJ = v- 1/2exp(ikz) where k = pili = mv/Ii. The wave function is normalized so that the flux density of particles is equal to vltfJ21 = 1. The diverging spherical wave f(fJ) exp(ikr)/r corresponds to scattered particles far away from the scattering centre. Thus at large distance, tfJ can be written in the form
tfJ ~ v- 1/2exp (ikz) + v- 1/2 f( fJ) r-1exp (ikzr) .
I. I. Sobel'man et al., Excitation of Atoms and Broadening of Spectral Lines © Springer-Verlag Berlin Heidelberg 1995
(2.1.1 )
10
2 Theory of Atomic Collisions
The number of particles scattered per second into a solid angle dO equals
Since the flux density of incident particles is 1, we have da
=
(2.1.2)
If(19)1 2dO.
Therefore to calculate da it is necessary to find the function f( {)), which is determined by the asymptotic wave function (2.1.1). The function f({)) is called the scattering amplitude. The Schrodinger equation for a particle in a centrally symmetric field has the solution RI(r)P/(COS{)), where PI is the Legendre polynomial and RI is the solution of the radial equation (2.1.3 ) where tff
= li,2k2/2m is the electron energy
rRI ~ k- 1/ 2 sin(kr - nl12
+ '1J),
(r -- 00) .
(2.1.4)
The phases '11 in the asymptotic expression for RI are defined by the potential U(r) in the whole range 0 S; r < 00. To determine these phases it is necessary to find the solution of (2.1.3) for all values of r. The wave function", can be expanded in terms of the functions RIPI in a so-called partial wave expansion:
'" = EAIRI(r)P/(cos{)) ~ EA l k- 1/2r- 1sin(kr -n112 + '11) PI (cos 19) I
=
I
exp(ikr) Al 2' E /L P/( cos {)) exp [i('11 - InI2)] lr
I
y
k
exp ( -ikr) Al . 2' E /LP/(COS{)) exp[-1('11 -lnI2)]. lr I yk
(2.1.5)
The analogous expansion of the plane wave in (2.1.1) is exp(ikz)
= Ei/(21 + 1) PI (cos 19)jl(kr) ,
(2.1.6)
I
where j[(x)
=
If
. ( x - -In) . 2xJI+1/2(X) ~ -1 sm x--+(X) X 2
Substituting (2.l.5-7) in (2.1.1) we find Al
=
If; ~
i/(21
+ 1) exp(i'1I)'
(2.1.7)
2.1 Fundamentals of Scattering Theory
11
and therefore m ) 1/2
t/I ~ ( fi,k
1 .1 2ikr~) (21 + I)P/(cos1?)
x [-exp(-ikr
+ i/n/2) + exp(2it/l) exp(ikr -
i/n/2)] ,
/(1?) = (2ik)-IL:(21 + 1) [exp(2il1l) - I]P/(cos1?).
(2.1.8) (2.1.9)
1
We shall now substitute (2.1.9) in (2.1.2) and integrate over the angles dO. Since
fP/(cos1?)P11(cos1?) sin 1? d1?
= {)ll' 21: 1 '
(2.1.10)
for the total cross section of elastic scattering we have (1
= 4nk- 2 L:(21 + 1) sin2 111 •
(2.1.11)
1
Comparing (2.1.9) and (2.1.11), it is easy to see that cross section of elastic scattering can be related to the amplitude of forward scattering /(0) by (1
= 4nk- Ilm {f(0)} = -2nik- I[/(0) -
1*(0)] .
(2.1.12)
This relation is called the optical theorem. It is a general relation which is valid also for noncentral fields.
2.1.2 Wave Functions flit, flit We shall introduce the wave function t/I:, which describes the plane wave exp(ik • r) and the scattered spherical wave. In contrast to (2.1.1) we normalize this function according to
t/lt
~ exp(ik. r)
r-+oo
+ /(1?) exp(ikr)/r.
(2.1.13)
For an arbitrary direction of the wave vector k, cos1? = (k . r)/kr. Using (2.1.8) we obtain
~
2.1k L:i/(21 + I)P/(cos1?) {-exp[-i(kr -In/2)] 1 r I
+
exp (2il1l) exp [i(kr - In/2)]} .
(2.1.14)
12
2 Theory of Atomic Collisions
Replacing exp (i"r) in I/It by exp (-i"r) we define the function
1/1;
=
~
1/1;,
~2Y(21 + 1) exp(-i"r)Pr(cos'l?)Rr(r)
vk r
-.I-Eir(21 + 1) Pr(cos 'I?){ - exp( -2i"r) exp [-i(kr - In/2)] 21kr r
+ exp[i(kr -In/2)]} .
(2.1.15)
One can see that exp(ik . r) + 1('I?)exp (-ikr)/r,
1/1;
~
I/Ii
= (I/I~k)*
(2.1.13') (2.1.16)
.
The functions I/It and
1/1;
are the solutions of the integral equation (2.1.17)
where G±k(r,r') is the Green's function of the free electron, defined as the solution G ( r') = ±k r,
_-.!.. exp(±iklr 4n
Ir - r'1
r'I)
(2.1.18a)
of the equation (2.1.18b) At
r~r',
we find
1 exp(ikr - ik' • r'), k' = k!: ; Gk(r,r') = --4 nr
r
(2.1.19)
and since 'I? is the angle between k, r, which is the same as that between k, k', we obtain 1('19) = - 2:h2 !exp (-ik' • r) U(r)I/It(r)dr.
(2.1.20)
Equations (2.1.17, 20) are useful for obtaining a solution of the problem by the method of successive approximation due to Born. In the integral equation (2.1.17) one can replace the unknown I/Il on the right-hand side by some approximation, and obtain a better approximation on the left-hand side. For the first approximation one can use exp(ik • r) in place of I/Il on the right-hand side; this gives IB('I9) = -2;2!U(r)exp [i(k-k'). r]dr.
This is the first Born approximation for the scattering amplitude.
(2.1.21)
2.1 Fundamentals of Scattering Theory
13
Quasi-Classical Approximation
2.1.3
As noted above, to find precise scattering phases 1'//, a numerical solution of the radial equations (2.1.3) is necessary. However, the problem is considerably simplified in the quasi-classical approximation. In this approximation, the function R/ for a particle with angular momentum I in a centrally symmetric field U(r) has the form
I (IhJ
R/ c::::
IL
vk r
sin
r
Pr dr +
rl
n) ,
-
(2.1.22)
4
where (2.1.23) For a free particle, this becomes
[.!. j
R/ c:::: _1_ sin J2m$ - 1i2(l + 1/2)2r-2 dr VI r Ii ro
+
!:].
(2.1.24)
4
The turning points r" ro are the zeros of the expression under the radical. From (2.1.22-24) one can see that the presence of the scattering potential results in phase shift 1'/1 in the argument of the sine, where 00
= J J2mli- 2[& -
1'/1
U(r)] - (l
+ 1/2)2r- 2 dr
rl
-
(2.1.25)
00
JJ2mli- 2& - (l
+ 1/2)2y-2 dr
ro
This phase may be identified as the scattering phase. It can be shown that the quasi-classical approximation is applicable when a large number of partial waves 1/11 make a substantial contribution in elastic scattering cross section. In that case, the main contribution to the sum over I is made by the terms with large values of I. At large I the lower integration limits in (2.1.25) should also be large iiI
r, -
iii
J2m($ - U)
, ro - - - . J2m$
If IU(r)1 decreases with increasing r so quickly that in the whole range of r the following condition is fulfilled: U(r)~$
then r, '11
~
ro
~ I/k,
= - 'J~ Ilk
(2.l.26)
,
where k
i:::
U(r)
mv/Ii, and
Ii Jk 2 - (I + 1/2)2y-2
dr.
(2.1.27)
14
2 Theory of Atomic Collisions
In the quasi-classical approximation, the angular momentum of the particle is mvp, where p is impact parameter. Therefore hJl(l + 1) ~ Ii,[ ~ mvp, and
1= kp .
(2.1.28)
If we assume that the particle moves in a straight line with constant velocity, then from (2.1.27,28) we obtain 1
'71
= -:2 '7(p) ,
1
'7(p)
00
= h J U(r)dt, -00
(2.1.29)
In the case of elastic scattering by an atom in the state a one has to substitute the diagonal matrix element of the interaction UIIII(r) which is the first-order correction to the energy of the state a due to the interaction with the scattered particle. Consequently, 1
'7(p) =
00
h J L1Ea(t)dt.
(2.1.29')
-00
In other words, in the quasi-classical approximation, the value of -2'71 is equal to the phase shift due to the shift of the atomic level during the collision. It is easy to prove that for the field U(r) = hC/rn, (2.1.29) gives the same (esuIt as the more accurate (2.1.27): (2.1.30) If we replace in the formula (2.1.11) for the elastic cross section the sum with respect to I by the integral over p, according to ~)21 + I) ~ k 2 Jpdp, 1
we obtain 00
(J
= 4nf[1 - cos '7(p)] pdp .
o
(2.1.31 )
As has already been mentioned above, the quasi-classical approximation is valid when partial waves with large values of I give substantial contributions to the cross section. It means that collisions with the values of impact parameter p II,
p~-
mv
= l\
(2.1.32)
are most important. Here l\ is the de Broglie wavelength of the electron.
2.1 Fundamentals of Scattering Theory
2.1.4
15
Inelastic Scattering
In the general case, when both elastic and inelastic scattering occurs, the wave function must contain, besides the incoming plane wave, a large number of outgoing waves, corresponding to different types of scattering, or different scattering channels. For purely elastic scattering the intensities of incoming and outgoing partial waves (l waves) are the same. For inelastic scattering, the intensity of an outgoing wave corresponding to elastic scattering must be smaller than that of an incoming one. Taking this into account, the wave function t/! describing elastic scattering at large r can be written in the form
m ) 1/2
t/!:::::. ( fik
+
I
2ikr~?1(21+1)P/(Cos'l9){-exp[-i(kr-ln/2)]
+ 2i'1l) exp [i(kr -
exp (-2/31
(2.1.33)
In/2)] ,
where /31
~
0. Hence we obtain for the scattering amplitude
/('19)
=
2~k ~)21 + 1) P/(cos '19) [exp (-2/31 + 2i'1l) -
1] .
(2.1.34 )
This formula differs from (2.1.9) only by the replacement of the real phase '1 by the complex one '11 + i/3l. From (2.1.2) it follows that tTelastic
=;
y(21
+ 1) 11 -
exp (-2/31
+ 2i'1d1 2
•
(2.1.35)
Using the expression (2.1.33) we can also derive a formula for the cross section for inelastic collisions, which is defined by a difference of fluxes corresponding to incoming and outgoing waves: tTinelastic
=
n
k 2 y(21
+ 1)[1
- exp (-4/3d] .
(2.1.36)
The total cross section is tT
= tTelastic + tTinelastic
= For /31
2n k 2 y(21
+ 1)[1
(2.1.37) - exp (-2/31) cos 2'11)] .
= 0, tT = tTelastic; for /31 = 00, the term exp (-2/31) = 0, and so tTl. elastic = = n(21 + 1)/k2 . It is easy to see that n(21 + 1)/k2 is the number of
tTl. inelastic
particles with angular momentum I incident on the scattering center per second when the flux density is equal to unity.
16
2 Theory of Atomic Collisions
From (2.1.35-37), the following limits of variation of the cross sections can be obtained:
o :::; O'I.elastic :::;
4n
o :::; O'I.inelastic :::; o :::; 0'1 :::;
4n
+ 1) ,
k 2 (21
n k2 (21 + 1) ,
k 2 (21
(2.1.38)
+ 1) .
We note that inelastic scattering is always followed by some elastic scattering. If exp ( - 21lt) 1= I, then at any value of '11 including '11 = 0, 0'elastic 1= O. The cross sections of elastic and inelastic scattering can be related to the elements of a matrix, which is usually called the scattering matrix, or S matrix. Let us denote the initial state of the scattering system by a and write exp (-2Ilt - 2i'1l) = S~~ .
(2.1.39)
Then O'elastic
= ; ~'<21 + 1) 11 - S~~ 12 ,
O'inelastic
0'
=;
1)(1 - IS~~) 12) ,
2(21 +
= O'elastic + O'inelastic = !~ 2(21 + 1)Re {I - S~} .
(2.1.40) (2.1.41) (2.1.42)
Inelastic scattering is connected with transitions of the scattering system from the state a to all energetically accessible states b (i.e., to the states with energy which does not exceed the sum of the initial energy Ea of the atom and the kinetic energy of the incident particle 8). We denote by O'ab the cross section of the transition a - t b. In Sect. 2.2, it will be shown that the cross section O'ab can be related to a nondiagonal element of S matrix:
_ kn" L../21 + 1) I
O'ab -
(I) Sab
2
12 .
(2.1.43)
The conservation of the total particle flux implies the inequalities (2.1.38), and is equivalent to the requirement of S matrix unitarity,
2:IS~~12=l, 2:1~~12=1-IS~12.
(2.1.44)
b~a
b
According to these equations, the modulus of the matrix elements S~~ cannot exceed unity. The inequalities (2.1.38) arise immediately from this condition, and also the inequality
< O'inelastic (I) < ~(21 + 1) . - k2
(I) O'ab -
(2.1.45)
2.2 Theory of Electron-Atom Collisions
17
2.2 Theory of Electron-Atom Collisions In this section we consider the general problem of scattering of electrons on atoms and ions. In contrast to the previous discussion, we have to deal with a complex system composed of an N -electron atom and an incident electron. Their interaction depends, in particular, on the atomic state. Besides, it is necessary to consider exchange effects, so that the system has to be described by an antisymmetrical wave function. After collision, the atom may be in any of the excited states or in the initial state. Hence, general equations describing collision process are similar to multiconfigurational Hartree-Fock equations. We now make some simplifying assumptions. We shall deal mainly with inelastic collisions resulting in the excitation of an atom. Therefore, we shall not analyze any specific characteristics of the ionization process [2.4,5]. Moreover we shall restrict ourselves to such transitions when quantum numbers of only one electron are changed. We shall call this electron "optical" in what follows, and usually suppose it to be in the outer shell of the atom. The atomic core without the optical electron will be called the parent ion. We shall describe the atom by a wave function which is constructed from one-electron functions in accordance with the rules of angular-momenta coupling. When we say "atom" we cover both neutral atoms and positive ions. We denote the nuclear charge by ?E and the charge of the atomic core by z:
z=?E-N+l
(2.2.1 )
where N is total number of bound electrons. z can be called asymptotic charge; the optical and incident electrons move in fields which are asymptotically equal to -z/r and -(z - 1 )/r, respectively. z coincides with the spectroscopic symbol of an ion: HeI, LiII etc. [A] means the isoelectronic ion sequence of an atom A. We use atomic units with the Rydberg unit for energy: Ry = 1/2 a.u. = 13.60 eV In these units v 2.2.1
=k=
p
= ..;s.
Cross sections are in the units 1ta~.
General Formulas for Cross Sections
We shall denote by tpaoMokomo the completely anti symmetric wave function of the system. The upper indices describe the state of the system before the collision, namely the atom in the state aoMo, and the incident electron with wave vector ko and spin projection Mo denotes the magnetic quantum number of an atom (or z projection of the total angular momentum of an atom). We shall expand this function in terms of atomic eigenfunctions: ( It'+I-j tpaoMoko mo =A E tpaM(~l "'~N) l/IaMmS(o, A = E ~ P~~. (2.2.2)
mo'
aMmS
j
N+l
]
18
2 Theory of Atomic Collisions
is anti symmetrization operator, P~~j is the permutation operator being a set of space and spin variables. In accordance with the general definition, the differential cross section of transition aoMomo ---. aMm s equals the flux of electrons with the spin projection mS in the solid angle dO, provided that the atom occurs in the state aM, and the incident electron flux equals unity. The velocity of the scattered electron v = k is in that case given by the relation
where
A
~ ~ ~j, ~j
kJ + Eao = k 2 + Ea .
(2.2.3)
Using the anti symmetrical properties of the function 'P, we obtain da
= v(N + l)j IA'PaMt/!aMms
12d~r2dO (r ---. 00),
(2.2.4 )
where d~ denotes the integration over all variables besides r. The asymptotic form of the integrand in (2.2.4) depends on whether the state aM belongs to a discrete or to a continuous spectrum. If we restrict ourselves to the simpler case of a discrete spectrum (for the other case, see [2.4]), only the term with P~~ remains in (2.2.2) as r ---. 00, because 'PaM decays exponentially. Using the asymptotic expression for t/!aMms similar to (2.1.1), t/!aMms
~ ~[exp(ik . r)J(aMmS, aoMomo) + faMms(1),cp) exp(ikr)/rlxms
(2.2.5)
,
where Xms is the spin function, we obtain da(aoMomo, aMmS) = IlaMms(1),cp)1 2dO.
(2.2.6)
We shall now separate the radial and angular variables. This can be done by expanding the wave function of an outer electron in partial waves. To simplifY the formulas we take the z axis along the direction of the vector k o. Then (2.2.2) can be rewritten in the form 'PaoMokomij =AE fJlo 'PaM ( ~1 ... ~N )~FJO(r)Yhn( 1), cp) Xms , loy r s }' = aMAmm , }'O = aoMoAo OmO .
(2.2.7) (2.2.8)
Here A and m are, respectively, the angular momentum and its z projection of the outer electron (we reserve the letter I for an optical electron of an atom); Y'\m( 1), cp) are the spherical harmonics. The radial functions FJO(r) in the expansion (2.2.7) are the solutions of a scattering problem. They fulfil the conditions: FJO(O) FJO
= 0,
~ ~ {JyyO sin ( kor - A2n) + TyyO exp
[i (kr -
~) ] }.
(2.2.9)
The asymptotic form in (2.2.9) and below is written for simplicity for the case
2.2 Theory of Electron-Atom Collisions
19
of neutral atom. For scattering by positive ions it should be replaced by the expression (2.2.40) given below. Comparing (2.2.7-9) with (2.2.2 and 5), we obtain
Plo
-'lo J41t{2A.o
-
leo
1
+ 1)
'
(2.2.10)
'lo-A J41t{2A.o + 1) faM",,{fJ,({)) = ~1 k TmYbn{fJ,({)). loAm 0
(2.2.11)
Thus, if we know the radial functions F:O{r), and hence the matrix Tyyo' we can determine f aM"" {fJ, ({)), and then the scattering cross section according to formula (2.2.6). The representation y used up to now is in fact useful only for perturbationtheory calculations. To derive. general equations of the Hartree-Fock type it is necessary to use the total angular momentum representation. In the LS coupling scheme, the system is described by the set of quantum numbers
r
1 = aA. 2LTST, a = rxLS ,
(2.2.12)
where rxLS is the set of atomic quantum numbers, and LT,ST are the total orbital and spin momenta of the system consisting of the atom plus outer electron. The formulas that follow are independent of the particular coupling scheme, i.e., the definite form of r. We shall denote the symmetric transformation matrix y ~ r by (yin. Then the total wave function of the system is
ljIaoMoko ms ~r
=A~ plo{yln ~r ~ F~O{r) , lor
r
(2.2.13)
= ~(rly)ljIaM YbnX"" . y/r
Using the unitarity of the transformation matrix, we obtain
F~O{r) ~ ~ {b rro sin (/cor - ~1t) + Trro exp TyyO =
~
ro/Yo,Fly
[i(kr - A.21t)]}, (2.2.14)
(Yolro)(rly) Trro .
In this formula the summation is over those quantum numbers from the set r that do not occur in the y set. We shall denote them by r/y. In the LS coupling case, r/y = LTST. From (2.2.14), (2.2.6), and (2.2.11) we obtain the following expression for the differential cross section:
da{aoMomo, aMmS ) =
4~\ ~
ko ro/ao,Fla,m
ilo-AJ2A.o+1{yolro){rIY)TrroYbn{fJ,({))\2dO.
(2.2.15)
20
2 Theory of Atomic Collisions
Usually one has to deal with collisions of unpolarized electrons with randomly oriented atoms. The orientation of an excited atom, described by the quantum number M, may be important because it determines the polarization of subsequent radiation. In order to obtain the corresponding cross section it is necessary to average (2.2.15) over Momo' and sum over mS. It is convenient also to expand the product YAmY;'m' in (2.2.15) in spherical functions Y"I' of the same angles. It is easy to show that only J.l = 0 terms give nonzero contributions, i.e., the cross section is independent of cp, as would be expected. We shall write the final result in the form da(ao, aM)
=
1
(2.2.16)
-k2LB"P,,(cos'!9)dO. 2go 0 "
In the case of LS coupling, B
"
=
2ST + I ""A.o-..:,+).' -).-2m[ LA.' AA'][KL L']2 2( 2So + 1) L."l "'IJ 0 T T x
K\ (
( A A'
0 0 0)
A A' K\ (Lo Ao LT ) ( Lo -m m 0) Mo 0 -M Mo
LA LT \ (L x ( M m -Mo) M
L~ \ m -Mo)
A'
(2.2.17)
*
TrroTr'r~
the summation extending over LT,L~, Ao, A~, A, A', m,Mo. Here and below we use the following designations .. ... ] -- (2'JI [JIJ2
+ 1)1/2(2'J2 + 1)1/2 ....
b(ab ... ,a'b' ... )
(2.2.18)
= baa,bw ...
(The properties of Wigner's 3j symbols
(jl
\ml
h h)
m2
were described in
m3
[Ref. 2.6, Sect. 4.2]). We shall now consider the total cross section. Equation (2.2.16) after integration over angles gives a(ao, aM)
=
21t
(2.2.19)
--2Bo. goko
Summing with respect to M, i.e. over the final orientations of the atom, we obtain a(ao, a)
= La(aoAo, aA) , A.oA
a(aoAo, aA)
= 1ta~k~
gr ITrro 12 , o r o/aoA.o.rja). go
(2.2.20)
L
where go is the statistical weight of the state ao of the atom, and gr is the statistical weight of the state r of the system.
2.2 Theory of Electron-Atom Collisions
21
Equation (2.2.20) provides a simple relation between the cross section a and the matrix T for an arbitrary coupling scheme. The partial cross sections a( aoAo, a2) are introduced for convenience in the further discussion. In the case of LS coupling, (2.2.21 )
For transitions between J levels One should derive the formula using J} (or J2) coupling: r = aJ,2!(J)h. If the atom is described in LS coupling, and magnetic electron-atom interaction is neglected, the dependence on J is purely kinematic and can be expressed explicitly. For the matrix elements Trro we can return to LS coupling and obtain
a(aoJOAo, aJ2)
= na5 (2.2.22a)
s
where the 9} symbols
h { 12 k2
S} • Trro 12 '
S
Jo Jo
JT J J
}III }O} 10 kl
SO} {STLT
~o Lo
~ L
were defined in [Ref. 1.1, Sect. 4.2],
ko
summation and transformation formulas are given in Sect. 6.3, too. In particular, (6.3.5) provides a possibility to rearrange the columns (or rows) in the sums of 9} symbols. Using this relation we can change the summation over angular momenta }o}Jr to the sum over multipole indices kqv and write (2.2.22a) in a more convenient and simpler form: (2.2.22b)
We introduce now M-factors [2.12]: So S Mq v(SU) == Mql(v(SoLoJo, SLJ) = [JoJv] { Lo L Jo J I(
q} " .
(2.2.23)
v
Utilizing the relations for 9} symbols with One zero we can write (2.2.22b) in a
22
2 Theory of Atomic Collisions
compacter and symmetrical form:
cr(aoJoAo, aJA.)
2k ( =ltao 2
2
"L..J(q K)4Mq2 K v(SLJ)
o 2Jo + I )qKV
(2.2.22c) X
2.2.2
ILTST L [STLT]MqqO(SSST)MKKO(LALT)· Trrol2
S-matrix and Collision Strength
In scattering theory, one usually uses an S matrix linked with our T matrix by the simple relation
Srro
= brro - 2iTrro '
cr(aoAo,aA.)
= 1ta~~ L 2ko
gr ISrro - brro l go
(2.2.24)
2 •
The asymptotic form of FJO(r) is represented in this case by
FJO(r)
~ k- I/ 2 {b rro exp [-i(!cor - ~1t)]
- Srro exp [i(kr _~1t)]}. (2.2.25)
The S matrix is symmetric, and satisfies the unitarity condition
L r
(2.2.26)
ISrrol2 = I .
The definition of cross section directly in terms of the unitary matrix S (or T) often proves to be inconvenient because the approximate matrix may no longer be unitary. The most important example shows up the 1st-order perturbation theory when Srro rv (rlulr o) and not limited by any condition. Moreover, even the individual terms ISrro I can exceed unity. Therefore, the number of scattered particles can exceed the number of incident ones. To avoid this defect, the K matrix is often used [2.8]. It is connected with the S matrix by a nonlinear relation,
S=I+iK 1- iK'
(2.2.27)
where I is the unit matrix: Irro = brro ' This K-matrix representation is used in particular in the quantum defect method [2.9]. Discussion of various matrices of the collision theory can be found in [2.1 0]. The matrix K is symmetric and Hermitian, but nonunitary. The corresponding radial functions are real and have the asymptotic form
FJO(r)
~ k- I/ 2 [b rro sin (!cor - ~1t) + Krro cos (kr _ ~1t)]
.
2.2 Theory of Electron-Atom Collisions
23
These functions can be represented as linear combinations of functions (2.2.14). No matter what kind of approximation is used for the calculation of the K matrix, the S matrix derived from (2.2.27) is unitary, and the corresponding cross sections, being approximate, are however in accordance with the particle-number conservation condition. Sometimes instead of the transition cross section t1aoa ' the dimensionless quantity, collision strength, is used (2.2.28) The collision strength is symmetric with respect to direct and reverse processes, and is additive with respect to atomic level structure. In case of transitions with no spin change at large energies, t1 ex &-1, i.e., Q = const, or increases slowly (logarithmically). As mentioned above, see (2.1.38), the total partial cross sections of inelastic processes obey definite inequalities. Since the cross section of a specific transition cannot exceed the total inelastic cross section, these inequalities can be written in the form
E Q(aoAo, aA.) ::; 2..1.0 + 1 •
(2.2.29)
l
2.2.3
Radial Equations
The functions F~O(r) are the solutions of radial equations, which can be derived by means of a variational principle similarly to the derivation of the HartreeFock equation for discrete spectrum states. Although the analogy with the Hartree-Fock equation is rather close there are certain differences, which we shall briefly discuss below. First, in collision theory the total wave function '1' of the system must contain many different channels, i.e. it is multiconfigurational. Consequently the outer electron is described by a set of functions F~0 (r), satisfying a (generally infinite) set of integrodifferential equations. On the other hand, the self-consistent field of the free electron is zero. This makes it possible to determine the atomic wave functions independent of the outer electron. In other words we can consider the atomic wave functions as known. Normally, no orthogonality conditions with atomic functions are imposed on the functions of an outer electron. The equations are derived regarding possible nonorthogonality. This leads naturally to a wider class of trial functions, but the equations become more complicated. However if certain additional assumptions are made, the equations become substantially simpler, and resemble the usual multi configurational Hartree-Fock equations.
24
2 Theory of Atomic Collisions
Finally, we note that the energy of the system is also considered as known, in contrast to the discrete-spectrum case, where it has to be determined by solving an eigenvalue problem. We shall not describe here the rather cumbersome derivation of equations [2.7], and give only the final results. The set of integrodifferential equations to be solved can be written in the form
(!l'r
+ k 2 )Fr = 2:' r'iT
(2.2.30)
Urr,(r)Fr , .
The operator !l'r is the usual Hartree-Fock operator, d2 !l'r = -d2 r
-
A(A + 1) r
2
c
-
Ur(r), Ur(r) = Ur
+ Urr
,
(2.2.31 )
r
where U describes the interaction of the outer electron with the atomic core, and Urr, the interaction with the optical electron. The potentials Urr' (including the case r' = r) are integral operators which are expressed in terms of radial integrals: (2.2.32)
YU' = [1l'AA'] (~~~)
(~~~) 2? ~~I (1- cll,JKOr»
(2.2.33)
xPlh)Fr , (rddrl , Cll'
1 '2 1 2 = 2( -BI + k ) = 2( -BI' + k ) .
(2.2.34)
Here PI(r) and BI are the radial function and energy parameter of the optical electron. In (2.2.34) we neglect the difference between the energy parameter and the level energy. The factors IX and f3 depend only on the angular-momentum quantum numbers. If the atom is described in a fractional parentage scheme, a = Yp Lp Sp nlsLS, then IXK'
rr'
= J(S S') (-1 ~T+L+L' +Lp [LL'] { L L' ,)
K' }
A' A LT
{L L' K' } I' I Lp , (2.2.35)
{SSS}{LALT} " " f3~r,=(-I)I+I+I-s-s[SS'LL'] S's; LpI'L' T I A' K" where [jlh ... ] is defined by (2.2.18). Eqs. (2.2.32,35) can be written in more symmetrical form which is convenient for general derivations and for computer codes. We use the factors M defined
2.2 Theory of Electron-Atom Collisions
25
by (2.2.23). Then Urr,(r)Fr ,
= I:( -1/+ ActKq
[2b(q)y~Fr' - [q]2y~Pl'] ,
Kq
(2.2.32a)
ct Kq
= (-It+ q [%~~~]] MOqq(SpsS)MoKK(LpIL)Mqqo(SSST )MKKO(LALT) . (2.2.35a)
These formulas are symmetrical on orbital and spin variables. of the interaction is 1 and s = !, the "radial spin factors" are 2b(q,0), and Y~ = 2q + 1. The factor (-1 )1+)' is connected to (2.2.33) and (2.3.10-11) in place of (lIICKII/'). If there are m equivalent optical electrons in the state nlm , p in (2.2.35) must be replaced by
If the "spin part" Y~ = (! III q II!) = the 3j-symbols in the factors ct and (2.2.36)
Gf
s are fractional parentage coefficients. (See [Ref. 2.6, Sect. 5.1.5]. The where p p tables of fractional parentage coefficients for electronic configurations p3, p4 and p5 are given in Sect. 6.3). For transitions between terms of one nlm configuration, the ct, p are related to the coefficients ( II UK II ) and ( IIVK II ) [Ref. 2.6, Sect. 5.4.1]. The potential Uf can be expressed in terms of radial integrals in a similar way. Very often, however, simpler approximations are used for U since for inelastic collisions it is not very important. In the above formulas, the summation limits over K are defined by triangular and parity conditions, namely
r
K
= Kmin,
Kmin
+ 2,
...
Kmax ,
K~in
= max (II - l'I. Iit - it'I),
K~in
= max (1/- it'l, lit - 1'1), K::mx = min (l + it', it + 1') .
K~
= min (l + I', it + it') ,
(2.2.37)
The radial equations should be supplemented by boundary conditions. When r = 0, all F~O(O) = O. The asymptotic form of these functions depends on the sign of k 2 :
k2
~ 0, Fr r~oo k- I/ 2 {brro sin ( kr - ~1t) + Trro exp [i(kr -
it21t) ] } ; (2.2.38)
k 2 < 0, Fr ~
r--+oo
o.
(2.2.39)
26
2 Theory of Atomic Collisions
If the target particle is a positive ion Xiz > l), it is necessary to change the argument in the asymptotic form of according to
FJo
An) [kr (kr - 2" -t
1
An + z-k- ln 2kr + arg r 2"
( l)] A+ . 1-
z-
lk-
(2.2.40)
where r(x) is the gamma function. The value of k 2 in the above formulas is determined by energy conservation. There is no scattered wave for energetically inaccessible final levels (k 2 < 0). The inclusion of these states in a general system of equations corresponds to the inclusion of polarization terms in perturbation theory.
2.2.4 Integral Radial Equations To analyze the equations of collision theory, and in some cases for their numerical solution, it is useful to pass from differential equations to integral equations. They can be derived by means of the formal solution of (2.2.30) using the Green's function that satisfies the equation (!l'r
+ k 2 ) Gr(r,r') = b(r -
(2.2.41 )
r').
The Green's function can be expressed in terms of two linearly independent solutions of the corresponding homogeneous equation: (2.2.42)
(!l'r
+ k 2 )Fr = (!l'r + k 2 )Fr = 0,
Fr(O)
= 0,
Fr(r
-t
(2.2.43)
0) = ar-A
(2.2.44 )
q = ik
(2.2.45)
2.2 Theory of Electron-Atom Collisions
27
With the Green's function the integral equations for the functions Fr are written in the form I Fr(r)
= Drri'ro(r) + "" J Gr(r,r') 2:.' o
Urr,(r')Fr,(r') dr' .
(2.2.46)
r'",r
Substituting (2.2.42) and (2.2.44) in (2.2.46), and comparing with (2.2.38), we obtain
= Drro exp (i1f) sin 1] - "" J F r 2:.'
Trro
o
(2.2.47)
Urr,Fr' dr .
r'",r
The operator f£ in (2.2.43) as defined in (2.2.31) describes the motion of the particle in the field Ur. Therefore the solution Fr of (2.2.43) is usually called a distorted wave. Other representations are also possible. In particular it is possible to transmit the term with Ur from f£ r F r to the right-hand side of (2.2.30), i.e., take the free-motion operator as the basis. This representation is ca!led the Born representation. We shall give here the explicit formulas for F and F in the Born representation, which are needed below: Fr
=
Fr
= vqri;.(qr),
Vkr h(kr),
F=
iVkrh~I)(kr),
= 2 = -vqrk;.(qr),
F
(k 2 > 0) ,
(2.2.48) (k 2
=
_q2
< 0) .
11:
hl
Here hand l ) are spherical Bessel and Hankel functions, and i;., k;. are the same functions for an imaginary argument. 2
2.2.5 Polarization Potential As shown in the preceding sections, the problem of the calculation of cross sections amounts to solving an infinite set of integrodifferential or integral equations. Using the iterative procedure for the solution of integral equations, we obtain another formulation of the problem with a clearer physical interpretation. I
See [2.11], where the Green's function for homogeneous boundary conditions is given.
It can be shown that the same formulas hold for inhomogeneous conditions of the type (2.2.38) if r =I- roo For r = r o, two solutions of the homogeneous equation, one of which satisfies the condition at r = 0, and the other satisfies the condition (2.2.38) at r ....... 00, are linearly dependent. In this case the second solution should satisfy some other condition, for example, (2.2.35) without the sine term. This is the reason for the additional term with r = ro in the right-hand side of (2.2.46). 2 The spherical functions J;., h~l), i1, k1' n1 are linked with the usual Bessel, Hankel and Neumann functions lA, Hf), h K1 and N1 by the relation
Z1(X)
= !"fZ1+!(X),
28
2 Theory of Atomic Collisions
We shall proceed from the set of integral equations (2.2.46) and take the free term as zeroth approximation: (0)
-
Fr = ~rroFro .
(2.2.49)
Then for the first approximation we get ",,(1)
-
= Fro,
1';'0
00
J Gr(r,r') Urro(r')Fro(r') dr' , (r i:- ro).
F~I) =
(2.2.50)
o Extending the iterative procedure to increasingly higher approximations, one can obtain
- + J Gro(r,r' ) Vroro(r,)Fro(r - ,)dr, , = Fro 00
Fro
o
(2.2.51)
00
Fr =
J Gr(r,r') [Urro(r') + Vrro(r')]Fro(r') dr', (r i:- ro) ;
o and for the T matrix,
00
Troro = exp (i'1o) sin '10 -
J FroVroToFrodr o
(2.2.52)
00
Trro = -
J Fr(Urro + Vrro ) Fro dr, (r i:- ro) . o
The quantity Vrro is called the polarization potential. This is an integral operator of the type 00
V(r)
J V(r,r')
(2.2.53)
o and is represented by the series 00
Vrro =
E
11=2
(II)
Vrro '
Urrl···rn_lrO(r,r') =
Jdrl ... dr -2 Urr1(r) Grl(r,rl) Ur1 r2(rJ) ... ll
x Grn _ l (rll -2,r') Urn_lrO(r').
(2.2.54)
The last formulas are applicable both for r i:- r 0 and r = r o. In the sum over r I ••• rII-I it is necessary to omit all terms that include one or more diagonal factors Urkrk . Thus the solution of the collision theory equations is expressed in the closed from (2.2.51). The correction for the first-order matrix 7}~o is determined through the value Vrro. From the second formula (2.2.52) it is seen that Vrro is the correction for the Hartree-Fock potential Urro ' which is where the term "polarization potential" stems from.
2.3 First-Order Approximation
29
Strictly speaking, only a formal solution has been obtained, since a lengthy solution of an infinite set of equations has been replaced by a no less cumbersome calculation of an infinite series (2.2.54). Besides, the question of the convergence of the series is still not clear. However, if the series converges, the use of a polarization potential to get the approximate solutions has a number of obvious advantages. In particular, in some cases it is far easier to formulate an approximate expression for the potential than for the wave function.
2.3 First-Order Approximation 2.3.1 General Formulas In the previous section the formal solution of integral equations and the equation (2.2.52) for the T matrix were obtained. Here we consider in more detail the first-order approximation, and derive explicit expressions for the T matrix and cross sections in terms of radial integrals and some angular factors. The latter are expressed in terms of 3nj symbols. The equations derived here are used in Chap. 3 for a discussion of some approximate methods. The first-order approximation is reaqily obtained from a general solution (2.2.52), if one omits the terms with polarization potential:
= exp(i'1o) sin '10,
00
= - J FrUrroFro dr.
(2.3.1 ) o This expression corresponds to replacement of the full set of equations by pair of independent equations,
Tforo
Tfro
(2.3.2) From comparison of the boundary condition (2.2.38) for ro = r with (2.2.44) it is clear that Fro = Fro. Below we shall restrict ourselves to the discussion of inelastic collisions (i.e., r =F r0), and as usual, we shall not allow for the relativistic interaction of the outer electron with the atom. We begin with the case of LS coupling with the states of the type
a = YpSpLpnlSU , where YpI. pSp define the state of the atomic core. On substitution of eqs (2.3.1), (2.2.32a, 35a) in (2.2.22c) we obtain
u(aoAo,al) = nao2 ~(2J.2
0+
I
1) E MqICv(SLJ) E MqqO(SsST )MIC/CO(LA.LT )[qK]2 qICv Lr8-r
30
2 Theory of Atomic Collisions
and after summation over LTST: a(aoAo,aA.)
2
2 E IMqKv(SLJ)MOqq(SpsS)MoKK(LpAL) o 2J0 + 1) qKV
= 1Wo k 2(
x [LpSp].
[q~](_l)q+K+l+)' [2b(q)R~-[qfR~]12,
(2.3.3)
00
R~
=
J Fro Y~Pldr. o
r. However the case when they are independent of LTST is most interesting, and we restrict ourselves by this case. It is necessary to sum over LTST. Now we can separate the radial and angular factors, and we write a in the form
F rand RK depend, in general, on all quantum numbers
a(ao,a)
=E
[Q~(aoJo,aJ)a~(/o, I)
+ Q~(aoJo,aJ)a~ (/0, I)]
K
C"(q)
= ~[q]2 2
(2.3.4 ) ,
where C(p) are C' or C", a~ and a~ are defined by (2.3.9) below. The amplitude angular factor is (2.3.5) Here, b and Q', Q" depend only on the angular-momentum quantum numbers of the states ao, a. Q~ coincides with the angular factor QK for the probability of 2K-pole radiative transitions [Ref. 2.6, Sect. 9.3.6)]. We use both notations Q and Q'. The radial factors a~(/o, I), a~(/o, I) are equal to the cross sections of one-electron transition nolo - nl. a' includes the direct and mixed parts, and a" is the exchange part. The interval in which K can vary in both the terms of (2.3.4) is the same, 1/0 - II :::; K :::; 10 + I. However, the physical meaning of K for the two terms is different. In the first one it is the index of mUltipole interaction. Therefore, only those a~ do not vanish for which the value of K has the same parity as 1/0 - II. In the second term the quantity K is simply the summation index, see (2.2.32a), and a~ with any value of K may exist. The set of formulas for a, Q ... is given in Sect. 2.3.2. For transitions between the mixed states ao, a, where W(a)
= E(ala)w(a) ,
(2.3.6)
alii
the cross section is given by (2.3.4) with bqKV (ao, a) =
E
(ao lao) b qKV (ao, a)(a Ia) .
ao/iio.a/ii
(2.3.7)
2.3 First-Order Approximation
31
where bqKV(ao,a) has been defined in (2.3.5). For intermediate coupling a/ii = LS. Thus, only the angular part depends on the coupling scheme. The radial part can be calculated independently. We see from (2.3.5) that angular factors for direct and mixed terms are the same (that permits to include the mixed term into the radial part a~). The presence of J( q) provides J(So, S) both in direct and mixed terms; therefore, the contribution of the direct term to the probability of intercombination transitions is '" (v / c f. The case of configuration mixing is more complicated since the radial part (one electron cross section) also depends on the configuration. The total cross section cannot be written ·for this case in the form (2.3.4). The following approximations are most often used: (i) Born-Oppenheimer Approximation: The functions Fr in (2.3.3) are the freemotion radial functions, i.e., solutions of (2.2.43) at Ur = O. If exchange terms are neglected in Eqs. (2.3.3-5) we obtain the usual Born approximation. (ii) Coulomb-Born Approximation (with or without exchange): The Fr are the Coulomb radial functions for the potential [Ur = -(z - 1)]/r. For neutral atoms (z = 1), approximations (i) and (ii) coincide. (iii) Distorted Wave Approximation: Fr are the solutions of (2.2.43) taking Ur as the Hartree-Fock atomic potential. (In some cases Thomas-Fermi or other approximate expressions for Ur are used.) The approximations and also some modifications are discussed in Chap. 3. Approximations (i) and (ii) are the most important for applications.
2.3.2
List of Formulas for
(J
and Q-Factors
For arbitrary coupling scheme, aiioii
, + aiioii " = aiioii = ~ [Q~(iio,ii) a~(lo, I) + Q~(iio,ii) a~(lo, I)]
,
(2.3.8)
K
where a~(lo, I) and a~ (/0, I) are one-electron cross sections, depending on quan. tum numbers nolo, nl only:
(J~(l0,/) = na~ ko2 [:OK]2 -loA ~R~(R~ - R~)
a~(lo, I) = na~ k2[: ]2 ~(R~i o OK -loA R'
(2.3.9)
== Rd and R" are direct and exchange radial integrals:
R' = [I 0 120 2] (lOKI) (AoK2) 000 000 K
x 2
'Jo 'J Fro (r')p/o (r") r>:~l P/(r")Fr(r') dr" dr' 0
(2.3.10)
32
2 Theory of Atomic Collisions
R"K
= '" (-1 L..J
)K+K" [
Kif
"]2 { Klo I 1 } RCK"
KK" 1_ K "0
II.
R = [IlL A.] (/OKA.) (AoKl) 0 "0 000 000 C
Kif
211 o
Fro(r')p/o(r")
::1
(2.3.11 ) (1 - cr>I>(K",O))Fr(r")p/dr" dr'
r>
0
From the 3j and 6j symbols in (2.3.10, 11) it follows
Kmin = max (II - 10 1, K~in
= max (IA. -
10 1, II - Aoi),
In the sum of Q~u~ all K
= Kmin + 2m,
In the sum of Q~ u~
IA. - Aoi),
K
Kmax = min (I + 10, A. + Ao) , K~ax
have the parity of .dl
The angular factors equal to
= 1-/0: (2.3.13a)
can be of either parity, but all
K"=K~in+2m,
K=Kmin+m,
= min (A. + 10, 1+ Ao) .
m = 0, 1,2 . .. . K
Q~, Q~
(2.3.12)
K"
have the parity of I - A.o:
m=0,1,2 ....
(2.3.13b)
for the transition iio-ii in intermediate coupling are
2/0 + 1 '" b2 (- -)C(p)( ) Q(p)( K ao, a-) -_ (_) L..J qKV ao, a q,
gao
qv
(2.3.14 )
where ao, a are the states in the LS coupling, 9 (iio) is the statistical weight of the state iio, and the shorthand superscript (p) stands for prime and double primes, respectively, i.e., C' = 2;:( u q, 0) ,
C" -_ -21 [q]2 .
(2.3.15)
The (amplitude) angular factor b in the LS coupling for the transition
ao = YpLpSpno/osLoSoJo
-+
a = ypLpSp nlsLS.!
(s =
~)
2.3 First-Order Approximation
33
is equal to
(2.3.16) x {LO L K } (-1 )s+s+Sp+L+lo+Lp+K+q 1 10 Lp
.
We give now the formulas for the Q factors in the case of LS coupling for the same transition (2.3.16). Formulas for other types of transitions will be given in Sect. 6.2. For simplicity we show as arguments only the last quantum numbers for ao and a. From (2.3.14-16) we obtain
Q~(Jo, J) = c5(So,S) [loJLoLf {1 fo;} {~o t L: } 2
2
"1,,
QK(JO,J) =
2 Tv'[/oJSoSLoLqv]
2 {
SoSq
}~5~
}
2
2
(2.3.17)
{SOSq} {LoLK}2 S sSp 1 10Lp
For transitions between the terms Lo So-LS we should sum (2.3.17) with respect to J, and average it with respect to J o :
2Jo + 1 Q'(J. J) Q'(L S LS) - " K 00, -J;;( 2Lo+l)( 2So+1) K 0, and similarly for
Q~.
,
(2.3.18)
As a result we obtain considerably simpler equations: (2.3.19)
(2.3.20) Thus the cross section for transition between terms Lo So-LS can be written in the form
aaoa =
~ QK(Lo,L) [c5sosa~(lo, /) + 2(~~p++\) a~(lo, I)]
(2.3.21)
Summing over L we have
Q(Lo,LpSpl) =
I: QK(Lo,LpSpIL) = 1, L
Q(LpSp1o,LpSpl) = 1 .
(2.3.22)
34
2 Theory of Atomic Collisions
For a more general case 1'0 - 1~-1/, by summing over S, L p, Sp, we obtain
QK(/'O' 1~-1/)
= QK(/'OLoSo, 1~-1/)
= Q~(/'O,/~-l/) =
Q~(/'OLoSo,/~-ll) = m,
(2.3.23)
and therefore (1(/'0, 1~-1l) = m L [(1~(lo, I)
+ (1~(lo, I)]
.
(2.3.24 )
k
One can see from (2.3.24) that LK(1~(lO, I) and LK (1~(lo, l) correspond to cross sections of one-electron transitions. However, the interpretation of particular terms in the sum requires special consideration. According to (2.3.9,10),
L(1~ = L(1~ K
+L
(1~~1I .
(2.3.25)
KKK"
Here (1~ is the cross section for direct 2K-pole interaction; (1~~1I is a mixed term consisting of direct 2K-pole and exchange 2K" -pole interactions. In contrast, (1~ contains the sum of exchange terms of all multipole orders K". The sum LK (1~ can be rewritten in the form (2.3.26) where (1~1I is 2K"-pole exchange cross section, and R~II is defined by (2.3.l1). It should be noted that an explicit summation over K and the transformation to the form LKII (1~1I are possible only for the total cross section of a transition between configurations, when Q~ does not depend on K. For some problems the partial cross sections (1(ro,r) with definite values of LTST are necessary. For transitions between terms LS we can use (2.2.21) without the sum over LTST. The derivation similar to that used for the total cross section gives
or (2.3.27)
where R' and R" are defined by (2.3.10, 11). The factors A and B depend only
2.3 First-Order Approximation
35
on angular momenta. For the transition 1'O~I~-1 I we obtain
ao = I'OLoSo,
a = 1~-I[LpSp]ILS
A = (_l)LT+Lo+L+Lp[KL L] { K Lo L} { K Lo L } GLoSo 'm 0 Lp110 LTA.A.o Lpspym I(
B
sos
= (_l)I-S-SO[SS,] 0
In particular for Sp
{!
2
= 0,
Bs~s
So ST}
! SS
P
= (-1 fT+ I;
sI 1/2 Bsos = (-1) '2(2S + 1) bST 1/2.
while for So
= 0,
(2.3.28)
3
Approximate Methods for Calculating Cross Sections
Various approximate methods for calculating the cross sections of excitation and ionization by electron impact are considered. Firstly, the Born approximation and its modifications taking into account the Coulomb field, exchange interaction, and normalization of the cross sections are described. The range of applicability and accuracy of these methods are discussed. In Sects. 3.3 and 3.4 some other more complicated methods are briefly discussed, in particular, the second Born approximation, the method of polarization potential, and the close-coupling method. For more detailed discussions of these and some other approximate methods see [3.1-3]. Special consideration is given to the case of transitions between highly excited levels with n ~ 1. The Born approximation as well as the quasi-classical approximation are reduced to comparatively simple formulas. The results of numerical calculations are also given.
3.1
Born Approximation
3.1.1
Collisions of Fast Electrons with Atoms; Multipole Expansion
In those cases when the interaction responsible for scattering can be considered as a perturbation and the exchange can be neglected, it proves to be possible to obtain simple general formulas for the cross sections without using a partial wave expansion. We consider first the scattering of a charged particle of arbitrary mass on an atom. We denote the reduced mass of the system by J.l. In accordance with the well-known perturbation theory, the formula for the probability of an atomic transition between discrete states aoMo, aM, accompanied by a change in the perturbing particle wave vector ko - k is dWaoMoko,aMk
= 2"1t IUaoMoko,aMk l2 o(Eo - E)dk,
(3.1.1)
where
(3.1.2)
I. I. Sobel'man et al., Excitation of Atoms and Broadening of Spectral Lines © Springer-Verlag Berlin Heidelberg 1995
3.1 Born Approximation
37
The factor 2 in the expression for U is due to the use of the Rydberg unit of energy (Ry); '" ko and '" k are the free-motion wave functions of the perturbing particle. The final state function is normalized to 11 (k - k'), or = (2n)-3/2 exp (ik. r). We normalize the wave function of the initial state to unit flux density, '" ko = VOI/2 exp (iko . r). Then the differential cross section du coincides with the transition probability dW. Integrating (3.1.1) over k, we obtain the Born cross section
"'k
Jl2
k
d~oMo,aM = l6n 2 . ko II exp[-i(ko -k)· r]UaoMo, aM(r) drl 2 dO , k2/Jl=Eao-Ea+k~/Jl.
(3.1.3)
If we are not interested in the orientation of the atom after scattering, we can sum du over M and average over Mo. Then dUBaoa
. - k) • r] UaoMo , aM(r) dr 12 dO, = -Jl212' -kk . '"" L.J I J exp[-l(ko 6n
MoM
090
(3.1.4) where 90 is the statistical weight of the state ao. Equation (3.1.4) is called the Born formula. The case a = ao, k = k{J corresponds to elastic scattering; the case a i= ao, k i= ko, to inelastic scattering. The Born approximation is a good approximation for calculating electron-atom scattering, if the electron velocity is large compared with the velocities of the atomic electrons. In the following part of this section, we treat collisions with electrons only, and so we can suppose /.l = 1. After integration of (3.1.4) over dr by means of the relation
I
exp( -iq . r)
Ir-ri I
4n
.
dr= 2" exp(-lq. ri), q
(3.1.5)
we obtain . (3.1.6) FaOMO,aM(q) = (aMI
E exp( -iq . rj) laoMo) j
q
= ko - k , q2 = k~ + k 2 - 2kok cos fJ
(3.1.7)
We now separate the radial and angular variables. We expand exp (-iq . rj) in (3.1.7) in spherical harmonics, see (2.1.6), exp (-iq • r)
= 4n E i- K Y:I'( fJ q , KI'
qJq)
YKI'(fJ, qJ )jK(qr) .
(3.1.8)
38
3 Approximate Methods for Calculating Cross Sections
Substituting (3.1.7) and (3.1.8) in (3.1.6) and using the Wigner-Eckart theorem [Ref. 3.4, Sect. 4.3], (yJMITKIlIYoJoMo)
= (-I)J-M(yJIITKllyoJo) (
.!M :
jo) ,
(3.1.9)
and the summation rules for 3} symbols and YKII , we obtain B
dUaoa
8n
= -2k I (aIlTKllao) ogo
~t5aoa
2
I
dq 3""' q
(3.1.10)
where TKII is the operator TKII
=;=
(2K4:
1)
1/2
YKII(f)j,<{Jj)}K(qrj).
(3.1.11)
We shall begin with inelastic scattering ao =I- a. In that case the matrix element in (3.1.10) is nonzero only for one-electron transitions and (3.1.10) becomes simplified to 8n
B
dUaoa
= k~(2/0 + 1) ~QK(ao,a) [RK(q)]
2
dq q3·
(3.1.12)
The total cross section for transition ao - a is (3.1.13) Here R K ( q) is the radial integral RK(q)
= [Klo/]
(~/~ ~ )
1
P/(r)P/o(r)[ }K(qr) - bKo] dr,
(3.1.14)
which is similar to the corresponding integral in the multipole transition probability formula, but contains}K (qr) in place of rK. We note that J.K (qr) q --> __ O (2K
qK
+ I)!!
rK
.
(3 . 1.15)
The factor QK(aO,a) in (3.1.13) depends on the angular momenta of the states ao, a. The same factor is present in the expression for the line strength of electric 2K-pole radiation [Ref. 3.4, Sects. 9.3,6]. We note also that the QK in (3.1.13) and Q~ in (2.3.8) are the same. Generally speaking, the radial functions P/(r) of the optical electron of the atom depend on the whole set of quantum numbers a. However below we assume for simplicity that the radial functions depend only on quantum numbers n, I, and consequently we shall denote them as P/(r) or Pn/(r).
We shall write (3.1.13) in the form
U~oa
= L QK(aO, a) u~(lo, I), K
(3.1.16)
3.1 Born Approximation K
= Kmin,Kmin + 2, ... 10 + I; B
al«(1o,/)
8
2
Kmin
39
= 1/0 -II
ko+k
2
(3.1.17)
dq
= nao · kJ(2/0 + 1) koL [RI«q)] q3 .
Equation (3.1.16) is called the multipole expansion, and al«(1o, I) is the 2K-pole one-electron cross section for the transition nolo -nl. For ao = lWLoSoJo, a = 1~-I[LpSp] lLSJ,
QI«ao, a) = bsos[loJLoL]
2{KJOJ}2 { KLOL}2 ("'£oso)2 S L Lo Lp I 10 m, ULpSp
(3.1.18)
where Gio~o is the fractional parentage coefficient. A fuller list of formulas for p p QI( is given in Sect. 2.3.2 and 6.2. The possible values of K in (3.1.16) are determined by the 3j symbol in (3.1.14) and correspond to a 2K-pole electron-atom interaction (i.e., they do not pertain to any partial wave). All the K are of the same parity according to the change of atomic parity during the transition 10 -I. In many cases it is sufficient to consider only minimum multiplicity K = Kmin, since al( decreases rapidly with increasing K. We should note that the decreasing of a I( with increasing K is not connected with any small parameter. In this point, the electron-atom interaction radically differs from the interaction of the atom with an electromagnetic field. In the latter case, the higher multipoles contain the factor (ze 2 /hc )2r<:+1 = (z/137 il(+I , and each successive term is smaller by a factor of about 10-4 z2. In the case of electron-atom collisions such small parameter does not exist. Numerical calculations show that in the Born approximation the multipole cross section al(+2 is usually 5-10 times smaller than al(. From (3.1.14,18) it follows that the selection rules when K f. 0 are the same as for electric multipole transitions. For example, in LS coupling at K = 1 : A I
=±
Lo + L
1; AL ~
= 0, ±
1; Jo
+J
~
= 0, ± AS = 0 ;
1; AJ 1;
1;
= 0,±2; AL = O,± 1,±2; AJ = O,± 1,±2; 10 + I ~ 2; Lo + L ~ 2; Jo + J ~ 2 ; AS = 0 .
(3.1.19)
at K = 2: Al
(3.1.20)
K = 0, in contrast to radiative transitions, ao f. O. By means of (3.1.13,14,18), the relation between the cross sections of direct and reverse processes clm be obtained. Exchanging in these formulas the initial and final states of the atom, and also ko and k, we have
At
gokJaB(aoko, ak) = gk2a B(ak, aoko).
(3.1.21)
It is easy to see that this relation coincides with (1.2.8) which was obtained from the principle of detailed balance.
40
3 Approximate Methods for Calculating Cross Sections
For the elastic scattering on the atom in the state a containing closed shells and the open shell 1m , the differential cross section is equal
8n
B
dUa = k2(21
+ 1)
{
[00 sin qr {
0/ p(r)dr -
+ E QK(a)[RK(q)]2} K
where p(r)
]
2
diq
(3.1.22)
00
J p(r) dr = N
= ENlIj lj P~jl/r),
QK(a) =
fZ
o
~:~ I (zmsLllu KllzmSL)1 2 .
The formulas for the reduced matrix element of UK are given in Sect. 6.2. The sum over" is limited by the conditions" ::;;; 2/, " ::;;; 2L, " being even. If I ~ 1, L > 0, the term with " = 2 can be expressed through the atomic quadrupole moment. 3.1.2
Betbe Formula
By expanding jK(qr) in the radial integral (3.1.14) in a power series, and neglecting all terms beyond the first nonvanishing term, we obtain RK(q) ex q\
Ro(q) ex q2 .
(3.1.23)
It is clear that at " = 1 (i.e., Al = ± 1), the main contribution in the integral (3.1.13) is made just by the range of small q where this expansion is justified. Therefore we can get a simple approximation for the cross section. One should however substitute in the upper limit of the integral (3.1.13) some limited value qo, since at large q the function jiqr) oscillates and this range can be neglected. The formula obtained in such a way contains
00
Qt/max 1{PIoPI r dr
12
Jf.
ex Aa; ,
where faoa is the oscillator strength for the transition ao - at; AE = Ea - Eao , the transition energy. As a result, we obtain the Bethe formula (which can be called the "dipole approximation"),
uaoa ~
I.
2
7tQo •
8 qo Jc6AE . faoa In leo _ k .
About calculation of the oscillator strengths see [Ref. 3.4, Sects. 9.4,7].
(3.1.24)
3.1 Born Approximation
41
According to this formula, the cross section depends on qo only logarithmically. To estimate qo we should note that RK(q) is determined by the range of r ;:S ro with ro ~ IEaol-I/2. Therefore qo = min(ko
+ k, /lE:D
(3.1.25)
For large energies the logarithmic term in (3.1.24) is
In~ ~ In 2qko ko - k
(3.1.26)
LJE
The Bethe formula (3.1.24) is applicable to dipole transitions only (in other words, to optically allowed transitions). Due to its simplicity it is useful for estimating cross sections, although its accuracy in some cases is considerably less than that of Born formulas (3.1.13) or (3.1.16,17). One can see from (3.1.23) and (3.1.13) that at K #- 1, the approximation (3.1.23) is not adequate since the value of q- 3 R K (q) becomes large at large q. In other words, the approximate result is too sensitive to the value of qo. A detailed discussion of the Bethe approximation and related questions can be found in [3.5]. 3.1.3
Brief Description of Born Cross Sections
Excitation cross sections for neutral atoms calculated by the Born formulas (3.1.16,17) have a number of characteristic features. Some of them can be obtained by analysis of general formulas; others arise from the results of numerical calculations (Chap. 6) [3.6,7]. We stress that here and everywhere in this section we consider only transitions without change of spin. At high energies tff ~ LJE B Intff uKoc7
B UK OC
1
$
K=I,
K
#-
LJl=±I,
(3.1.27) (3.1.28)
1.
Below we often use the scaled energy U=
tffo - LJE
tff
DE
DE
(3.1.29)
For various atoms and transitions the Born cross sections reveal a similar behavior if the electron energy is expressed in threshold units DE
= LJE.
(3.1.30a)
These units are widely utilized in many calculations. However, they are certainly not appropriate for transitions between closely spaced levels when
42
3 Approximate Methods for Calculating Cross Sections
AE ~ IEol, Eo being energy of the initial state counted from the ionization limit. Here the choice DE=
IEol
(3.1.30b)
is more adequate. If the same energy scale is necessary for different transitions in the ion Xz the scale DE =z2Ry
(3.1.30c)
is more appropriate. As an illustration (Fig. 3.1 a-<:) excitation cross sections of some transitions in Hand Na with AE from 0.3 to 10 eV are depicted in the scales a, band c from (3.1.30). For convenience of comparison, all cross sections are normalized to the same maximum value. Usually cross sections reach a maximum value at U ~ 1. For optically forbidden transitions the maximum is moved to smaller u. One can see from the Fig. 3.1 that this similarity is better with the scale DE = lEo I. As a rule, for transitions between levels with An ~ 1, the maximum value IT~ = ITB(U m ) ex: AE- 2 • For transitions no - n with n~no, the cross section is proportional to n- 3 • For optically allowed transitions, both rules can be written in the form B ( lTaoa Urn)
~
2 faoa 1tao(AE)2
'
(3.1.31)
where f aoa is the oscillator strength. The descriptions given above have to be modified in the case of small AE ~ IEol, where Eo is the energy of the initial atomic state. For such transitions, threshold units are not useful, and one is most interested in energies & ~ IEol ~ AE. At these energies the cross section is almost independent of AE. Only for K = 1 is there the weak logarithmic dependence. It should be noted that all these features can be seen even in the Bethe formulas (3.1.24,26): B 2 lTaoa ~ 1taO·
faoa
(AE)2 .
InCu U
+1.
At large AE, this gives (3.1.31), and at small AE and &~AE,ITB ex: lng/C. It must be emphasized that the formulas above can be used only for preliminary estimates of cross sections. These properties also have to be taken into account when constructing semiempirical formulas. We have not mentioned above the problems of applicability of the Born approximation, and its agreement with experimental data. At large energies the Born cross section and the experimental one should agree. In fact, experimental results are often normalized to the calculated Born cross section at large energies (however, there is a question what energy value is sufficiently large). As an illustration we give here two examples: excitation of optically allowed ls-2 p and forbidden ls-2s transitions in H atom. (Figs. 3.2 and 3) The Born approximation
3.1 Born Approximation
43
1.2
5
f( 7'
0.8
b
:r-
0.2
o
I
1.2
1.0
rl
0.8
0.6 b
;/ II
~ 'r-3
o
i
·1-
r--._ .
---~
4
17"""::.
,I
0.4
0.2
~.:'
/I,! 2 / ,"-... Ii ,: !. /5
0.6
0.4
t>r---:--'- --'-. -----I'-.... --- "?- r-- -.• .i:..- ••
1.0
r-
~
~ 1:----
3
, ....
-~
a
I"~~
'"
-"- "- .. .. - --- -----"3,5
.................
~.
2
..............
"'- ~
--
6
4
1
............ b
1.2 r------,-----r---r---,--r----.--...,-----,
Fig. 3.1. Effective cross sections for transitions in atoms H (curves 1-5) and Na (curve 6): Transition Is-2s (1); Transition Is-2p (2); Transition 2s-5p (3); Transition 3s-4p (4); Transition 4s-5p (5); Transition 3s-3p in Na atom (6). (a) DE = LJE, (b) DE = Eo, (c) DE = Ry
44
3 Approximate Methods for Calculating Cross Sections 0.5
3,\
0.4
4 \
1\
15-25
\
it-' ..:a..",..... ",-
If
2 '.
~
1
0.1
..(\
.
,,
:
-----
~ 1'_ ~ ---.--- .. ----- ----- ------
o
4
5
u-
..
6
7
Fig. 3.2. Effective cross section for the transition Is-2s of the H atom: (1) Experiment [3.6]; (2) Born approximation; (3) Distorted wave method without exchange; (4) Approximation of close coupling between three levels Is-2s-2 p with exchange
1.6
(V!...
1.2 1/2/. ~~ ::::--
;1 1
14
0.8
III ,.- --U_,l ' l
15-2p
. ::::--
-~ ~ ' .. ------
------
--
._- ------- r----..
I
I
o
2
4
6
u-
Fig. 3.3. Effective cross section for the transition Is-2 p of the H atom: (1) Experiment [3.6]; (2) Born approximation; (3) Distorted wave method without exchange; (4) Approximation of close coupling between three levels Is-2s-2 p with exchange
usually overestimates the cross sections up to a factor of two in the vicinity of the maximum, and the maximum is located too close to the threshold. Such a feature of the Born and the experimental cross sections is rather typical. There are two main reasons: (i) The repulsion of optical and incident electrons is neglected in the Born approximation (atom polarization effect); (ii) The Born cross section is increasing infinitely with increasing interaction (aoIUla), this results in S-matrix unitarity violation (normalization effect),
3.1 Born Approximation
45
In the sections to follow this will be discussed in more detail. For a detailed comparison of calculated and experimental cross sections see [3.10]. Ionization and Three-Body Recombination
3.1.4
It is not difficult to generalize the Born formula to transitions for which the initial or final state of the atom belongs to the continuum. The transition of an atom from a discrete state to the continuum means ionization. The reverse process is called three-body recombination, since it implies the capture of an electron by an ion with simultaneous scattering of the second electron. The presence of the third particle is necessary to fulfill the conservation of energy and momentum. The equation for the ionization cross section can be derived from (3.1.16, 17), if we assume that the state a belongs to the continuum: a = aielLSJ, where ai is the state of the ion, and e is the energy of ejected electron. Usually we are not interested in the particular total angular momentum of the system: ion plus ejected electron, and the cross section should be summed over those quantum numbers. If the continuum radial function Psi is normalized to t5(e - e'), the differential ionization cross section is
(3.l.32) i
du,,(lo, el)
"
8
2
= 'TWo· k2(21 + 1) de o
0
ko+k
J [R,,(q)] ko-k
2
dq 3".
(3.l.33)
q
The radial integral R" can be calculated according to (3.1.14) with the function 1'0 according to (3.1.18) we have, cf. (2.3.22),
Pel in place of Pl(r). For ionization from a shell
(3.l.34) Therefore Qi does not depend on K. If the state ao is described by definite genealogical scheme ao = YpLpSp1oLoSoJo then Qi = 1 (to be more exact, t5LiLpt5SiSp ). For applications, the total ionization cross section is required:
where Ez is the ionization energy of the atom Xz • The cross section of the reverse process, namely, three-body recombination, is defined in a similar way, exchanging the initial and final states. The wave function of the electron in the continuum has to be normalized to unit flux instead of t5(e - e'). Besides, the result has to be averaged over the directions of wave vector k of this electron, and over the states of the ion Xz + 1. In this way
46
3 Approximate Methods for Calculating Cross Sections
we get the relation 2 2
2n k090
dui(ao, aiel) de
= ek
2
(3.1.36)
9j tT(ai el, ao) .
As mentioned in Chap. I, the dimensions of the differential ionization cross section duijde in the cas system are cm2 erg-I, while the total ionization cross section is measured in cm2 and for three-body recombination ur has dimensions cm4 s, so that N;vv' ur has the dimensions of S-I . The structure of (3.1.32,33) is similar to that of corresponding formulas for discrete spectra. The total ionization cross section (3.1.35) includes an additional summation over I, and integration over the energy of the ejected electron e. This entails considerably more lengthy calculations as compared to the case of excitation cross section. In fact, up to ten terms in the sum over I should be taken into account. Several values of /C correspond generally to every value of I. The first Born approximation is certainly applicable for large velocities··of the incident electrons. However, in the case of ionization this condition should be discussed in more details. If the energy of the ejected electron is e, the energy of the scattered one is $' = C - Ez - e; it may be small if the ejected electron takes most of the energy C - Ez . In other words, the range of small C' where the Born approximation does not work, can contribute to the integral (3.1.35) for any C. Analysis and numerical calculations show that for large C and e -+ C - Ez du B ( e) is small and the corresponding error is not considerable. If, however, an exchange is included, du i ( e) become symmetrical with respect to ejected and scattered
1.2 BK_ 1.0
0.8
l'
B1 1\ I'" '
\
liVsK
'6'0.6 Itl
~B2
I!(~ ~BO
B1
I
~, ~
B2······
~
6" 0.4 BO_._
~-.;;;:
~~
0.2
°
-5
°
5
m
~
m
~
-
~
35
X=g'/Ev Ez =13.61eV -
Fig. 3.4. Ionization cross section for Is level of the hydrogen atom given in various approximations (Sect. 3.1.4)
3.2 Some Refinements of the Born Approximation
47
electrons, i.e., da i(8)
= dai(C'),
C'
= C - Ez -
8
(3.1.37)
and the contribution of small C' may be considerable. On the other hand, from the (3.1.37) follows that the total cross section may be written [with an exact da i(8)] as a
i
1 Em da i(8) J --df.= 2 0 d8
= -
Em/ 2
J0
da i(8) --d8. df.
For the Born approximation without exchange the two expressions are not equal and the second one is preferable since it excludes the range of slow scattered electron. In what follows we shall always use for the total ionization cross section the following definition i
a
Em/ 2
= J o
da i( f.) -d-d8, f.
Em
= C-Ez.
(3.1.38)
A detailed and mathematically more accurate consideration of the symmetry of the ionization amplitude was done in [3.8,9]. In particular, it was shown that general equations include the interference term with a phase choice which is rather uncertain. Usually this interference term disappears from the final expression for the total cross section. In most cases (3.1.38) is in better agreement with the experimental data than (3.1.35). However, it should be noted that this agreement is partly occasional: one can see that (3.1.38) gives always smaller result than (3.1.35), but the Born approximation usually overestimates cross sections. Generally speaking, the energy dependence of the ionization cross section is similar to that of the excitation cross section. We note that for ionization the two scales (3.1.30a, b) coincide: DE = Ez • In the sum over I there are terms with K = 1 as well as K =I- 1. At large energies they are <X In (u )/u and l/u, respectively. It is difficult to predict at what energy the logarithmic term will become important. Near the threshold a i <X u3/2 in the Born approximation. A more accurate analysis which is beyond the scope of the Born approximation shows that, in fact, a i <X u [3.9-11]. In Fig. 3.4 the ionization cross sections of the H atom in the ground state Is are presented. The results (BI, B2) obtained using (3.1.35,38) are shown together with the cross section (BK) recommended in the compilation [3.12]. The curve BO was obtained with exchange included by Ochkur method (see below).
3.2
Some Refinements of the Born Approximation
The Born method for calculating inelastic collision cross sections differs from all other approximate methods in its simplicity: it does not require a partialwave
48
3 Approximate Methods for Calculating Cross Sections
expansion. The calculation of cross sections in the Born approximation amounts to the numerical calculation of a few integrals. At the same time, the Born method provides a sufficiently accurate qualitative description of cross sections, and often does not lead to large quantitative disagreements with experimental data. For many types of transitions from the ground state, an overestimate of the maximum cross section by a factor 1.5-2 is typical. For transitions between excited states, there is insufficiency of experimental data. However, for transitions between the excited levels of multiply charged ions the Born method should provide very reasonable accuracy of cross sections in the energy ranges that are of the most interest in practical applications. In some cases, however, the Born approximation is totally inadequate. For example, it gives the zero result for intercombination transitions in LS coupling. It is therefore of interest to consider the possibility of refining the Born approximation by taking some evident physical effects into consideration. It should be emphasized that we mean only the possibility of including new types of transitions with the same typical accuracy, i.e., a factor of the order of 2 near the maximum cross section. We do not consider here any attempts to improve this accuracy. The main physical effects mentioned above are the distortion of incident and scattered waves by the atomic field, the exchange, and normalization. All these refinements can be realized only in the partial wave representation (Sect. 2.2), so that the simpler q representation (Sect. 3.1) cannot be used. The following will be based on the first-order approximation for the solution of a general set of equations (Sect. 2.3). This approximation requires, however, some refinements and modifications to take into account properly the physical effects mentioned above. In the following sections we discuss these refinements.
3.2.1
Distortion of Incident and Scattered Waves; Excitation of Ions
The simplest refinement of the Born approximation is the distorted wave approximation which corresponds to the first-order approximation without exchange (Sect. 2.3; Jr! = 0). In this case the functions Fr are the solutions of the radial equations for an electron in the attractive field Ur of the atom. At this point, however, we should distinguish between the effects of attraction of the electron by the short-range field of the neutral atom and the attraction by the long-range Coulomb field of the ion. In fact, the polarization of the atom due to repulsion of the outer and optical electrons overcomes the first effect, so that the average distance between electrons increases as compared to the case of free movement of the outer electron. For this reason, the Born approximation overestimates the cross section. Inclusion of the attractive field without regard for polarization effects would result in larger'overestimation of the cross section at small energies. Allowance for the polarization effects (i.e., the repulsion of electrons) is possible only in second-order perturbation theory. From the above it is clear that the
3.2 Some Refinements of the Born Approximation
49
distorted-wave method is not appropriate for the calculation of excitation cross sections. This is confirmed by the results of numerical calculations. In contrast to the attraction of electrons to neutral atoms, the Coulomb attraction to positive ions leads to an increase of the electron flux density in the vicinity of the ion owing to electrons with large initial values of the impact parameter. The effect of Coulomb attraction of electrons to the ion provides the qualitative change of the excitation cross section at threshold, namely,when go = LlE,O" i=- 0, in contrast to the case of the excitation of neutral atoms. For this reason one should not neglect the Coulomb interaction in calculations of ion excitation, at least in the vicinity of threshold. The Coulomb-Born approximation refers to the method in which only the distortion by a Coulomb field with asymptotic value z - 1 of the charge is taken into account. The cross section is defined by the formulas of the first-order approximation (Sect. 2.3) without exchange terms. In the integral Rd in (2.3.10) we have to substitute the Coulomb radial functions. We obtain O"aoa
= L:Q,,(aO,
a)O",,(lo, I),
O",,(lo, I)
2 4 d 2 = lta0k2[l F L:(R,,) ,
"
Rd = "
0
[I IA A) 0
0
OK
~A
(3.2.1)
(K000 10 I) (K AO A) 000 (3.2.2)
where PI are the radial functions of the optical electron of the ion, and FA are the functions of the outer electron which· are defined by equation
_ (~ d r2
A(A + 1) r2
+ 2(z r-
. ( FA ~ k- 1/2 sm kr - -An r-+oo 2
1)
+ k2) FA
z- I + -k-
_ 0
-
,
In kr + '1 ) ,FA(O)
= o.
(3.2.3 )
The angular factors Q" are the same as in the Born approximation, and are defined by formulas of Sect. 2.3. The sum over An, A in (3.2.1) converges very slowly. However, the value of R~ tends to its Born limit at ..10 , A~ 1; thus the total cross section can be calculated by means of B 4n '" d 2 B 2 0",,(l0,/)=0",,(l0,1)+k FL.,[(R,,) -(R,,»). 2 [l
o
OK
(3.2.4 )
).0 A
Here R~ is defined according to (3.2.2,3) with z = 1, and O"~ is the Born cross section (3.1.17), which can be calculated without partial-wave expansion. The sum in (3.2.4) converges much better. In spite of apparent similarity, the Coulomb-Born approximation and the distorted-wave method are radically different. At z = 1, the Coulomb-Born
50
3 Approximate Methods for Calculating Cross Sections 2.0
I 1.5 ",=
~ ~
1.0
'"
UI
,<2 "-
/
~
1s-2p
-
'---
/-' 0.5 o
4
5
r- r-8
u-
Fig. 3.5. Effective cross section for the transition Is-2 p in the ion C VI (C5+): (I) Born approximation; (2) Coulomb-Born approximation; u = (8 - iJE)/iJE
approximation coincides with the Born approximation. By a simple substitution of the variables zr
-+
r,
klz
-+
k,
one can show that the CoulomlrBorn approximation is the first-order perturbation theory result with parameter liz. Therefore the error of this approximation should decrease with increasing z. In Fig. 3.5 the excitation cross sections are given for the hydrogenlike ion CVI calculated in the Born and CoulomlrBorn approximations. One can see that the CoulomlrBorn cross section, in contrast to the Born cross section, jumps at threshold to its maximum value. When the electron energy increases to u '" 1--':2, the difference between Born and CoulomlrBorn approximations vanishes. For a detailed discussion of electron impact excitation and ionization of positive ions see [3.13], and a recent review on experimental data [3.14]. 3.2.2
Allowance for Exchange
a. Intercombination transitions (LIS = 1). The transitions with change of spin in the LS coupling approximation take place due to the exchange interaction. The corresponding generalization of the Born (or CoulomlrBorn) approximation can be obtained from the first-order approximation formulas. We shall use the exchange term in (2.3.8), and substitute the free-electron (or Coulomb) wave functions into the radial integral R~IfK of (2.3.11). This method is called the Born-Oppenheimer approximation. Numerical calculations imply, however, that the accuracy of the Born-Oppenheimer approximation is much poorer than that of the Born approximation for transitions with LIS = O. This failure is mostly due to nonorthogonality of the wave functions of the initial and final states of the system. One can demonstrate this nonorthogonality
3.2 Some Refinements of the Born Approximation
51
in the case of a hydrogenlike ion. The functions cPo(rJ,r2)
= Plo(rJ)F;'o(r2),
cP(rJ,r2)
= PI(r2)F;.(rJ)
are nonorthogonal because P(r) is the eigenfunction for the field -z/r, and F(r) is that for the field -(z - 1)/r. The angular parts of the wave functions provide the orthogonality for the case Ao =1= I, A =1= 10 . The lack of orthogonality of the total wave functions in initial and final states implies that the Born-Oppenheimer approximation isn't the first-order approximation of a perturbation theory. To avoid this defect the method of orthogonalized functions was suggested [3.15]. In the first-order theory, the modification ~f the formulas of Sect. 2.3 consists simply in the substitution of the functions F;. instead of F;. in the exchange radial integrals: F 1.0 = FI.o - (F1.o IPI) . PI . {)11.o
'
(3.2.5) F;. = F;. - (F;.IPlo) . Plo . ()Io;' • Then using the formulas of Sect. 2.3 for transitions with LIS = 1, we obtain
= EQ~(ao,
U aoa
a)u~(lo, I),
(3.2.6)
K
"(/
UK
0,
I)
=
7t
a?;
0
t1
4 " (R'K,)2 kJ[lOK]2
R~ =L:(-lt+K"[KK"]2 {K
10 I} [/o/AoA] (/0 K" A) K"AOA 000
K" 00 00
2f
o
f Fro(r')Plo(r") 0
K
(Ao K"/) 000
(3.2.7)
:~1 [l-cr>{)(K",O)] Fr(r")PI(r')dr"dr' .
r>
The angular factors Q~ are the same as defined in the Sect. 2.3. Numerical calculations show that the accuracy of the orthogonalized function method for intercombination transitions is about the same as that of the Born approximation for allowed transitions. The method is applicable to neutral atoms as well as to ions. Below we shall use the designations B, CB and CBE (or BE for z = 1) for the Born, Coulomb-Born and orthogonalized functions approximations. With increasing z the role of the orthogonalization is decreasing (P and F functions are in almost the same field) and CBE method gives the same results as the CB-Oppenheimer approximation. For z = 1 the contributions from the two terms in (3.2.5) are much larger than their difference. In that case the simple subtraction procedure defined by (3.2.5) may be inadequate; a somewhat better one is to omit the contributions from Ao = I and A = 10 • Another modification of the Born-Oppenheimer approximation was proposed for neutral atoms by Ochkur [3.16]. The Ochkur approximation is often used in practical calculations due to its simplicity, although the range of its applicability
52
3 Approximate Methods for Calculating Cross Sections
is more limited. The basic assumption of this approximation is as follows: in the asymptotic expansion of the exchange-scattering amplitude in powers of 11k, only the first nonvanishing term has physical meaning at small or medium energies. If we neglect all the other terms, the exchange cross section can be calculated in the simpler q representation in a way similar to that for direct cross sections [cf. (3.1.16,17)]. The result for the transition between the atomic terms LoSo and LS with AS = 1 is (J'aoa
_
=L "
Q~(ao, a)u,,(lo, I),
q2
R,,(q) = k~ [Klo/]
(3.2.8)
(K000 10 I ) £ 00
P/o(r)P/(r)j,,(qr)dr.
(3.2.9)
In contrast to the orthogonalized functions and the Born-Oppenheimer approximations the Ochkur method does not require a partial wave representation - results can be given in a q-representation in similar way to the Born cross section. This much simplifies its applications. However until now, no generalization of this approach was proposed for ions. It is easy to see from (3.2.8) and (3.1.14) that for large energies ,c the cross section of the exchange transition decreases as ,c-3 as compared with ,c-' or ,c-'ln,c. Asymptotically (at large ,c), the Born-Oppenheimer approximation and its two modifications considered above coincide. Usually, however, this asymptotic agreement is achieved only for very large values of ,c, when the cross section is too small. h. Allowed Transitions with AS = O. The transitions with AS = 0 are connected mainly with direct interaction, and the correction due to exchange is usually comparatively small. In some cases (in particular, for ions) the exchange correction proves to be more important because of a considerable compensation of the direct and interference terms. For Al = ±l, this compensation can occur at threshold when AE ~ lEo I (Eo being the initial energy of the atom). The typical example (and important one) is the excitation of singlet states of [He] ions' from the ground state. For IAII =I- 1, the influence of exchange can be even more impor tant because the exchange term can exceed the direct term at threshold. To calculate the cross section taking exchange into account, we should use (2.3.8) with both the direct and exchange terms. According to the above discussion we shall use in the radial integral ~ the Coulomb wave functions defined by (3.2.3), and in the exchange radial integral ~II", we shall substitute the orthogonalized functions FA defined by (3.2.5). Of course we cannot consider this method as quite consistent, but it provides good results for medium values
I
Here and everywhere we denote an ion of the isoelectronic sequence of atom A by [A].
3.2 Some Refinements of the Born Approximation
of z (for large z, uaoa = u~a
F;.
53
coincides with F;.). The cross section is determined by
+ u~oa = E .
K
[Q~(ao, a) u~(lo, 1) + Q~(ao, a) u~(lo, 1)], (3.2.10)
u~( 10 , 1) = na~ ko2 [:OKF "0;' E R~(R~ - R~) (3.2.11)
u~(lo, I) = na~ k2[: F E(R~i o OK "0;'
where R~ and R~ are defined by (3.2.2,7), and formulas for Q~ and Q~ are given in Sect. 2.3.2. As mentioned above, the exchange is important mainly due to compensation of the direct and interference terms in u' . We shall consider as an example the transition between states LS (without consideration of the fine structure ). According to (2.3.19), the cross section (3.2.10) can be written in the form u aoa
2
= nao·
4 ( 2 kJ(2/0 + 1) . EK QK(Lo,L) 1
2S + 1 ..2) - Ig + 2(2Sp + l)Y
,
(3.2.12) Usually for Al = ±1, g ::5 I. The exchange becomes important if the exchange amplitude g is of the order of the direct amplitude I, and at the same time the spin factor in (3.2.12) is small. For example, for the transition Is2 IS -Is 2p Ip in a [He] ion at threshold g ~ 3/4/,(28 + 1)/2(2Sp + 1) = 1/4. Therefore, the expression in brackets in (3.2.12) is equal to 0.4/2, compared with the value 12 without exchange. For K > 1 (Le., Al =I- ±1), g can exceed 1 at threshold due to exchange interactions with K" = 0 and 1 in (3.2.11). For this reason the role of exchange for such transitions can be even more important than for AI = ± 1, and even for AE ~ lEo I exchange can be important. In any case for 8 ~ AE, the exchange can be neglected because of the decrease ex 8- 3 in the exchange cross section. In Fig. 3.6 the cross sections of excitation of 2 I P and 2 3P levels in 0 VII are given. At the threshold, the two cross sections are almost equal. This fact is confirmed by experimental observation of X-ray spectra of laser plasma and the solar corona. The calculation of u(2 I P) without exchange gives for the ratio u(2 IP)/u(2 3P) > 2, which contradicts the experimental data. It is worth noting that if we sum the cross sections over S the expression in brackets of (3.2.12) would take the form
12
-gl +rr
which is insensitive to exchange if only g ::5 1 (Fig. 3.6). For example for [H] ions (only one value of S), the exchange can be neglected.
54
3 Approximate Methods for Calculating Cross Sections
10 2.5 \.
"- "/
(
\3
o.5 \ o
\
-.........
~ ......
OW ~ k!
~ r:::::::: t:::-
-
4567
B
910
uFig. 3.6. Effective excitation cross-sections for heliumlike ion 0 VII: (1) Coulomb-Born approximation for the transition 1; 1S-ls2 pIp; (2) Coulomb-Born approximation with exchange for the transition 1; 1S-ls2 pIp; (3) Exchange excitation cross section for the transition 1; 1S - Is2 P 3P; u = (8 - JE)/JE
3.2.3 Normalization The partial excitation cross section must satisfy certain inequalities arising from the conservation of particle number similar to the inequalities (2.1.38). According to (2.2.24) and the unitarity condition of the S matrix (2.2.26), we have q(r r) < n(2ST + 1)(2LT + 1) == qlim(r r) 0, - 2(2So + 1) (2Lo + l)kJ 0" q( aoAo, aA.) :::;
kJn (2Ao + 1) .
(3.2.13)
The Born approximation in the general case does not ensure the fulfillment of conditions (3.2.13). For sufficiently strong interaction, the partial cross section q(ro, r) can exceed the limiting value qlim(ro, r). As a consequence the total Born cross section in some cases is too large. Below, this situation will be referred to as ''normalization failure." A Born cross section corrected with regard for the inequalities (3.2.13) by means of any procedure will be called a normalized cross section and denoted by ii. 1 We consider here the normalization method based on the use of the K matrix. According to the definition (2.2.27) of the K matrix, the matrix relation
S
= 1+ iK
I -iK
(3.2.14)
1 Particle number conservation (or probability conservation) requires the unitarity of scattering matrix which imposes stricter limitations than inequalities (3.2.13).
3.2 Some Refinements of the Born Approximation
55
ensures the unitarity of the S matrix, independent of the approximation used in calculation of the K matrix. In (3.2.14) I denotes the unit matrix. For the purposes of normalization it is sufficient to take into account those matrix elements which include the initial state 0, i.e., we assume
r
0
Kror.
KrOr2
(
~ ;~:~: ~
K
... ) (3.2.15)
~
..... ........ .... :::
The K matrix method has been applied by Seaton [3.17] to ensure the unitarity condition. However, in [3.17] the full K matrix has been used instead of (3.2.15) and in consequence some other effects were admixed (cf. discussion in Sect. 3.3.2). After substitution of definition (3.2.14) in (2.2.24) we obtain the following expressions for the normalized cross section:
_ u(ro, r) u(ro, r) = [1 + '" K2 ]2· L..J r'ro
(3.2.16)
a'l'
r
= rxLSA!LTST. In the case of transitions between levels LSJ, In (3.2.16), r = rxLSJ,A!U)JT and the summation in (3.2.16) should be over 20 AjOjJT. It is easy to show that in the first-order approximation,
K2
r'ro
=
~ u(ro, r') 4 ulim(ro, F') .
(3.2.17)
We note that in the denominator of the second of equations (3.2.16), we should not sum over LTST. That means independent normalization of each LTST channel. We cannot perform the summation over LTST in (3.2.16) explicitly due to the nonlinear relation of u(ro, r) with u(ro,r). For this reason, instead of the formulas of Sect. 2.3.2 we have to use a general expression (3.2.16) and (2.3.27, 28) for u(ro,r): (3.2.18) The calculations with (3.2.16-18) are much more complicated than those with the usual formulas of the first-order approximation (Sect. 2.3.2). Recalling the approximate nature of the K matrix normalization procedure we simplify (3:2.16) by substituting in the denominator the average value of K;"ro:
K2
_
l'la -
(2LT + 1)(2ST + 1) 2 L~T (2Lo + 1)(2So + 1)2(220 + 1) Kr'ro
-- L7sT '" 4n(22ok5 + 1) u(r 0, r') --
k5
( L ' A') 4n( 2Ao + 1) u aO""l), a
•
(3.2.19)
56
3 Approximate Methods for Calculating Cross Sections
With this simplification we can perform the explicit summation over LTST in (3.2.16). The values of O'(aoAo, aA) can be calculated by the formulas of Sect. 2.3.2:
O'(aoAo, a' A')
=
L
[Q~O'~(/oAo, ['A')
+ Q~O'~(loAo,
l' A')],
(3.2.20)
K
where O'~(/oAo, ['A') and O'~(loAo, l' A') are partial cross sections from the sums (2.3.9). From (2.3.22,23) one can see that the sum over a' does not depend on the total momenta Lo,L'. Therefore, we can finally write (3.2.16) in the form
a(ao,a)
= L O'(aoAo,aA)/D, "0"
D
~ ]2 = [1 + 4n(2Ao + 1) n1f,1I KO'K(/oAo,lA)
(3.2.21 )
We also note that for a calculation of the exchange part of LK it is better to use (2.3.26). The sum over).' in denominator of (3.2.21) contains a few terms - L1[ = 1/0 - II· The sum over atomic states n'l' is infinite. Usually however only one or two states n'l' are important. It has to be emphasized that in many cases this level does not coincide with the final state of the transition. For example, in the case of the 3s-4p transition in the Na atom, the normalization is determined by the 3p level, i.e., by the resonance transition 3s - 3p in the sum over n'I'. In other words, normalization can be important even in the case of fulfillment of the conditions (3.2.13) for a given transition. In fact it is necessary to fulfill the condition (3.2.13) for all the transitions from a given initial state ao. One can infer from (3.2.21) that normalization by means of the K matrix provides a normalized cross section a~ O'lim when 0' ~ O'lim. The most consistent method of obtaining normalized cross sections is the accurate solution of the set of equations (2.2.30) with regard to close coupling of the states which are important for normalization (Sect. 3.3). The unitarity of the S matrix in this case is ensured if only the interaction matrix U is Hermitian. It is necessary, however, for the diagonal potentials Uroro and Urr to be omitted in (2.2.30); these terms provide the distortion of the incident and scattered waves. The last effect is not related to the problem of normalization, and can be a source of inaccuracies in the cross sections (Sect. 3.2.2). The results of numerical calculations by this method are in good agreement with those of the K matrix method. We note that when 0' ~ O'lim, the close coupling method decreases the cross section a compared with O'lim even more than the K matrix method does. In Figs. 3.7,3.8, cross sections of the 3s - 3p and 3s-4p transitions in the Na atom are given.
3.2 Some Refinements of the Born Approximation
57
1001-----.0£+""""""-+---+----+----1
t 75 ~850~-74+----__+_~~~~~----~
.!:!b 25 , '
1/ I
o
2
3
5
4
fUFig. 3.7. Effective cross section for the" transition 3s-3p of the Na atom: (1) Born approximation; (2) Cross section normalized with the use of the K matrix; (3) Close-coupling approximation; (4) Experiment [3.18]; u = (8 - AE)/AE
4
1/\ 1/r-\
Nal 3s-4p
IY' ~
I 'S"" '/ 1/
.;~
1
~ t--
o
4
............
- -6
u-
8
~ :::10
Fig. 3.S. Effective cross section for the transition 3s-4 p of the Na atom: (1) Born approximation; (2) Cross section normalized with the use of K matrix; (3) Close-coupling method; u = (8 - AE)/AE
3.2.4 Concluding Remarks: Generalized Born Approximation The Born approximation with the refinements discussed in the above sections provides excitation cross sections with accuracy sufficient for most applications. Usually the Born approximation gives a result which overestimates the cross section in the vicinity of the maximum by a factor of 1.5-2, and becomes more accurate with increasing energy. A typical example has been given above in Figs. 3.2 and 3.3 for excitation of resonance levels of the hydrogen atom.
58
3 Approximate Methods for Calculating Cross Sections
According to recent measurements and also astrophysical data, similar accuracy is provided by the Coulomb-Born approximation in the case of excitation of ions. Moreover, the accuracy of Coulomb-Born approximation increases with increasing z.l To obtain sufficiently accurate results in some cases, the exchange has to be taken into account. The typical example is the excitation of [He] ions from the ground state. The transitions with change of spin are fully connected with the exchange interaction. The method of orthogonalized functions outlined in Sect. 3.2.3 provides for these transitions in ions accuracy comparable with the characteristic accuracy of the Born approximation for transitions without spin change. However for neutral atoms, the accuracy of the orthogonalized-function method can be poorer. At least for transitions between levels with small energy difference LJE, the normalization procedure is necessary to provide similar accuracy. The Born approximation taking into account the effects of the Coulomb field, exchange, and normalization will be called the generalized Born approximation (GBA). The range of applicability of the GBA is much broader than usual Born approximation. At large energies, 8 ~ LJE both methods give the same results. We note that the GBA does not include transitions through a virtual level (Sect. 3.3). The calculations in the framework of the GBA are lengthier than for the Born approximation. The computer program for these calculations isn't too complicated, however, and does not require much computer time. The results of such calculations will be presented in Chap. 6. In this section we have discussed the calculation of excitation cross sections. In the case of the ionization cross section, only Coulomb attraction is important. Moreover the influence of the Coulomb field does not result in any qualitative effect similar to that in the case of excitation. More accurate analysis shows that the behavior of the ionization cross section near threshold is the same for ions and neutral atoms: CTj <X (80 - LJE).
3.3 More Accurate Methods of Calculation of Excitation Cross Sections In two previous sections we discussed methods based on the first-order approximation. To obtain more accurate results one should take into consideration higherorder terms of the perturbation theory or find the exact (numerical) solution of the equation set (2.2.30) with a finite number of equations. Computations of this kind are very complicated and of little use for the systematic calculations of cross
I The important exception to this rule are the near-threshold resonances connected with the long-range Coulomb interaction (Sect. 3.4).
3.3 More Accurate Methods of Calculation of Excitation Cross Sections
59
sections which are necessary for applications. Analysis of the results of some individual calculations reveals poor convergence of both methods with respect to the number of states that were included. One of the reasons for such a poor convergence is based on the opposite signs of corrections due to different terms in the equation set or in the series. One possible example is the mutual compensation of the effects of electron attraction to a neutral atom and polarization of the atom in respect to inelastic scattering (Sect. 3.2.2). One can distinguish two types of refinement of the results. Firstly, there are quantitative refinements in which the characteristic inaccuracy of the generalized Born approximation (GBA) is decreased or totally removed. The second type applies to cases where the GBA is for some reason inadequate, and the inaccuracy is much greater than that characteristic of the method. In the latter case the need for more accurate methods is evident. However instead of simply increasing the number of terms or equations it is advisable to add only those terms which overcome the deficiency of the GBA. In the rest of this section we discuss some of the problems mentioned above. The treatment is rather illustrlltive in places, because a complete account of the problem is beyond the scope of this book. We do not discuss here such methods as the Glauber approximation, impulse approximation, free electron scattering model, and variational methods. For the first two of these methods we refer to [3.2, 3, 19]. The free electron scattering model is discussed in [3.20]. About variational methods see [3.21].
3.3.1
Transitions Via Virtual States
The Born approximation for excitation cross sections corresponds to the first term of a series in perturbation theory. The higher-order terms contain infinite sums over all possible virtual states. Generally we cannot select a few terms from such a sum because of its poor convergence (see above). There are however cases in which the first term of the series in perturbation theory is small or even vanishing for some reason. Then it is necessary to treat the first non-vanishing term. Two-electron excitation or ionization with a simultaneous excitation of the ion are examples of this type of transition. If the one-electron wave functions in the initial and final states are supposed to be orthogonal, the transition matrix element in the first Born approximation is zero. A non-vanishing cross section in the first order can be obtained only with slight nonorthogonality of the oneelectron atomic wave functions before and after the transition. In second order, such a transition occurs through virtual levels corresponding to the excitation of one electron. The number of such virtual levels is not more than two. The orthogonality of wave functions in this case is of no importance, and the cross section in second order can prove to be considerably larger than in the first Born approximation.
60
3 Approximate Methods for Calculating Cross Sections
A similar situation can arise for some one-electron transitions. We consider as an example quadrupole transitions (for example, s - d). In the Born approximation, the cross section of such transitions is much smaller than that of dipole transitions. In second order, the transition can be accomplished through the virtual level as a "sequence" of two dipole transitions. The matrix element of such a transition often exceeds the first-order matrix element of the quadrupole transition. Usually one should consider only one virtual level. For example, in the case of the ns - n'd transition, this level is np, i.e., in second-order, we have the transition ns - np - n'd. The choice of virtual level is based on the high probability (around unity) of the excitation ns - np. For calculation of cross sections in second order we can use (2.2.52-54):
00
- L: a\).\
f f F).(r)Urr\ (r)Gr\ (r, r')Ur\ro(r')F~(r')drdr' ,
(3.3.1 )
0
where the orthogonalized functions F;. (3.2.5) should be substituted in the exchange integrals. The Green's function Gr \ for a neutral atom in accordance with (2.2.42) and (2.2.48) is Gr\ (r, r') = -ik\"'h\ (k\r < )hl~)(k\r» ,
kf = 8 0
-
(3.3.2)
Ea\ao .
In the sum over a\ we can consider only a few terms. Usually one state a\ which is most strongly coupled with the initial state ao, and the final state a is sufficient. In Sect. 3.1 we expressed the Born cross section in the q representation without a partial-wave expansion. In second order we cannot derive an analogous expression. It is possible however to obtain the approximate formula in the q representation. We begin with the three-dimensional expression for the excitation cross section, cf. (3.l.4), CTaoa
1 ko+k =-8 k 2 f qdq
1tgo
0 ko-k
L: IL: f[<>a\a
MoM
a\
+ Waa\(r)]Ua\ao(r)exp(-iq.
(3.3.3 )
r)drI2,
where Mo, M are total angular momentum projections, q = ko - k, and U(r)
= L: j
W(r)
=
(_2_ -~) , Ir-rjl r
(3.3.4 )
fU(r - x)G\(x) exp(ik . x) dx.
Here G\ is the three-dimensional Green's function. Below we assume that G\ is
3.3 More Accurate Methods of Calculation of Excitation Cross Sections
61
the Green's function of a free electron (even for ions): GI(x)
= - 4~ exp(iklx) ,
kf + Ea1ao = k 2 + Eaao = kJ
(3.3.5)
In spite of this approximation, the calculation of Waa1 is very complicated. Only in the case of k ----+ 0 can we obtain a simpler expression for W. We assume that the level al is situated lower than the final level a, and consider at first the interelectron interaction
U=_2_=~
Ir- rIi -
P.
By substituting (3.3.5) in (3.3.4) and integrating over x we obtain for k = 0 W
=
-E 2 [1 - exp(iJEaal p)] , aalP
k
----+
0.
(3.3.6)
In the opposite case of large k one can show that W is imaginary and proportional to k- I . The simplest interpolation formula which satisfies both this condition and (3.3.6) is _
W(p) - 2
( I - cos(..p;;;;p) 2 kiP
kf = k 2 + Eaa1
,
P = Ir -
. sin(..p;;;;P
-I
»)
~'
klyEaalP
(3.3.6a)
rll .
For a many-electron atom, taking into account the interaction with the nucleus, we must replace W by (3.3.7)
2]W(Pj) - W(r)] . j
On substituting (3.3.6a, 7) in (3.3.3) we obtain an approximate expression for the
excitation cross section in the second Born approximation in the q representation. For numerical calculations it is necessary to separate the radial and angular variables by means of multipole expansion of the potentials (3.3.4) and (3.3.6a). In spite of the more complicated expression of W(p), as compared to U(p), its expansion is not very difficult. If we confine ourselves to excitation transitions without change of the spin, we obtain First order: Second order:
a~~~I = 1ta~.
nol'OLoS - nol~-I[LpSp] nl LS nol'OLoS - nol~-I[LpSp] nlllLIS - nol~-I[LpSp] nl LS
L K
AI = (lIIKKI110)
2
ko+k
0
ko-k
k2CK
f
qdq
f jK(qr)(A I +AII)r2dr 12 ,
100 0
,
K"o K) {K'10 0
(3.3.8)
62
3 Approximate Methods for Calculating Cross Sections
where
C
=
K
2L + 1 {Lo 2K + 1 I
L
K}2
10 Lp
(3.3.10a)
,
The radial operators KK and WK are defined by the following formulas: r~
I
2,
KK(r, r ) = 2----=t:J - -u KO , r~
I
WK(r, r )
=
r
1 I J Eaal I 2i" k2KK(r, r ) + 2 - 2 -w K - -k w K ,
kl
I
w~(r, r') = (2K
w~(r, r')
x
=
+ l)jK(x< )nK(x»
= (2K +
JEaa1r,
x'
(3.3.11)
I
- C>KOnO(x) ,
l)jK(x)jK(x' ) - C>KojO(X) ,
=
JEaa1r' .
Here jK and nK are the spherical Bessel and Neumann functions (see footnote at page 27). We note that the sum over K' ,K" in (3.3.9) includes only a few terms in accordance with the triangle conditions
II - III ::::;
K' ::::;
I
+ II,
III - 101 ::::;
K" ::::;
11
+ 10 ,
(3.3.12)
and parity conservation.
3.3.2 Use of the K matrix Equations (3.3.8-12) for cross sections of transitions via virtual levels are approximate especially at large energies. Moreover they are not applicable for transitions with change of spin. For this reason we consider another approximate method based on the K matrix (2.2.27). We shall use the K matrix elements, calculated in first order, 00
Kr"r' = -TJ"r, =
J F;,,,Ur"r,F;.' dr,
(3.3.13 )
o
as well as the cross section calculated in accordance with (2.2.24), and the matrix relation (2.2.27). If we include in the K matrix the elements coupling the states aoAQ, alAI, aA, the resulting S matrix will describe the direct transition ao-a, the transition via a virtual level aO-aI-a, and also the normalization effects (Sect. 3.2.4). The latter property is an important advantage ofthe K matrix approximation.
3.3 More Accurate Methods of Calculation of Excitation Cross Sections
63
With the three types of transitions mentioned, we obtain from (2.2.27)
Srro =
~[Krro + i L:Krrl Krlro +o(K3)]
(3.3.14)
).1
where O(K3) includes the terms of the fourth and higher order with respect to Kr'r" and D is the determinant of the matrix 1- iK:
D
= III - iKll = 1 + K;ro +
L:K;lro + L:K;'r +O(K2) ).1
(3.3.15)
"I
If we neglect the terms o(K2) and O(K3) in (3.3.14, 15) we can obtain the following expression for the cross section:
(1aoa
=ED-1[1(aOAo, aA.) (1
+
4n:
T
T
+l)(2S +l)1 12] k6 L~T (2L (2Lo + 1)(2So + 1) fKrrlKrlro
.
(3.3.16) We note that in contrast to (3.3.8) the mixing term in (3.3.16) is absent because we used here the high velocity limit' for scattering amplitude. 3.3.3
Polarization Potential
The polarization potential Vrro (2.2.54) is used mostly in elastic scattering problems since no adequate approximation for off-diagonal potentials Vrro has been found up to now. The cross section for elastic scattering is determined by the diagonal potential Vroro' For simplicity, the zero indices will be omitted in this section. Instead of the equation (2.2.52) for the T matrix we introduce the potential Vrr in the left-hand side of the basic radial equation (2.2.41,43) and confine ourselves to the second-order term in Vrr . Inclusion of Vrr in the radial equation corresponds to partial allowance for the higher-order terms. We obtain the following equations for elastic scattering:
(!l'r - Vr + k 2)Fr = 0 , Fr r~oo k- I / 2 exp(i'1) sin
Trr = exp(i'1) sin '1,
(kr - ~n: + '1) ,
(3.3.17)
00
VrFr = -
L:
Urrl
rIfT
J Grl(r,
r') Urlr(r')dr'.
(3.3.18)
0
We shall consider now the so-called adiabatic approximation, in which we neglect the exchange term in (3.3.18) and approximate the Green's function by a () function:
Grl
1 ~
,
= - LJEu(r - r ) , LJE = Eal - Ea ,
(3.3.19)
64
3 Approximate Methods for Calculating Cross Sections
where Ea and Ea\ are atomic energies in initial and virtual states (in Ry units). In this approximation, the potential Vr is local. We average it over LT as in Sect. 3.2.3. Then we obtain the simple expression
Vr
'" sK(a, ad K 2 [lJ,]2AE [YII\(r)] ,
= Va(r) = - fa";
(3.3.20)
where QK is the angular factor that was determined in Sect. 2.3.2. From (3.3.20) one can derive the two limits: r -+ 0, and r -+ 00. In the case of r -+ 0, only the term with K = 0 is nonzero, and therefore It = I, LI = L, Q(a, ad = l/ga, and
Va(O)
4 AE n\ gaLJ
=E
[00J Pn\r(r)Pnr(r)..!. d]2 0 r
The main term in the asymptotic region (r II = I ± 1, and we have
b Vu(r)=-y4'
(3.3.21 ) -+
'" 4faa\
b=~(AEf(r-+oo),
00) is that with
K
=
1, i.e.,
(3.3.22)
where b is the polarizability of the atom in the state a, and f aa\ is the oscillator strength. In calculations a simple approximate expression for the polarization potential is often used: b (3.3.23 ) Va(r) = - (r2 + r5)2 ' where ro is the atomic radius. This approximation asymptotically coincides with (3.3.22), and is finite at r -+ O. A better estimate of ro can be obtained by application of (3.3.21). The adiabatic approximation is applicable at small energies of the outer electron: k 2 ~ AE. It is necessary also that .JAEro ~ 1.
3.3.4
Close-Coupling Method
Usually by the close-coupling approximation is meant the exact solution of the set of equations
(.5t'r
+ k 2)Fr = E Urr,Fr' , r = r'
.5t'r
d2
= -d 2 r
-
A.(A. + 1) . 2 - U[.(r) , r
aUrST
,
(3.3.24)
3.3 More Accurate Methods of Calculation of Excitation Cross Sections
65
where the number of the states a (or "channels") is limited by some condition. Below we shall use the Born representation when the term with diagonal potential Urr is included in the sum in the right-hand side of (3.3.24). The simplest version of the close-coupling method is the two-level approximation, (.!l'ro
+ kJ)Fro
=
E UrorFr, ).
(.!l'r
+ k 2 )Fr = E UrroFro .
(3.3.25)
.1.0
The first-order approximation can be obtained from (3.3.25) if we neglect the right-hand side in the equation for Fro. In other words; we neglect the influence of the final channel on the initial one. The consideration of this influence is the main feature of the close-coupling method. The equation set (3.3.24) or (3.3.25) is Hermitian and therefore its solution provides a unitary S matrix in the framework of included channels. That means we obtain a normalized cross section automatically. The set r can include the energetically accessible states a (or open channels with ,1E < 80, k 2 > 0) and also some energetically inaccessible states a (or closed channels with ,1E > 8 0 ,k2 < 0). In the system of equations (3.3.24), the open channels a' i:- a describe the excitation through virtual levels a'. The inclusion of closed channels corresponds to allowance for the effects of atom polarization by the outer electron. Of course this separation of the role of open and closed channels is approximate but it proves to be useful for' general discussion. As mentioned in the beginning of Sect. 3.3, the convergence of the method with increasing nuniber of channels is rather slow. Now we can explain this in the following way. The diagonal potentials Urr in the set (3.3.24) describe the attraction of the electron to the atom by the average field. This attraction determines the elastic scattering of the electron, and at the same time provides a decreasing of the distance between the atomic and outer electrons. The latter effect, however, is considerably reduced by the interelectron repulsion, i.e., by polarization of the atom. To allow for this polarization, we have to include in the equation set many other states mainly corresponding to closed channels. It should be noted that the diagonal polarization potential Vrr also describes the attraction of the electron to the center of the atom. The increasing of interelectron distance is described by the off-diagonal terms Vrr,. The inclusion of energetically accessible states in the set of equations describes, as mentioned above, mainly the transitions through virtual states. It is clear that this effect is important only when we deal with the influence of the strong channel on the weak one. In particular, this effect is unimportant in the case of resonance-level excitation. As an illustration of the above qualitative statements we consider the excitation of the 2s and 2p levels of atomic hydrogen. The results of some calculations by various approximate methods together with experimental data are shown in
66
3 Approximate Methods for Calculating Cross Sections
Figs. 3.2 and 3.3. As mentioned above the Born cross sections exceed the experimental data in the vicinity of the maximum cross section by a factor of 1.5-2. The inclusion of the electron-atom attraction (the distorted-wave approximation) provides a further increase of the cross section, and an increasing discrepancy with experiment. This effect is especially great in the case of the Is - 2s transition. We note that the effect of attraction is considerably compensated by exchange (not shown in the figures). The close coupling three-state approximation Is - 2s - 2p (with exchange) provides slightly better results than the Born approximation does in the case of the Is - 2p transition. However this improvement is insignificant compared with the total inaccuracy. In the case of the Is - 2s transition, the close-coupling method provides worse results than the Born approximation. The reason is the inclusion in the equations of the diagonal potentials without adequate regard for polarization effects. It is interesting that the results of the close-coupling approximation are near to those of the distorted-wave approximation with exchange. The six-state close-coupling approximation (Is - 2s - 2p - 3s - 3p - 3d) was used only in the energy range between the n = 2 and n = 3 thresholds. Taking into account n = 3 states in that case, one can partially take into account polarization of the atom, which results in a considerable decrease of the cross section of the Is - 2s transition. The above-mentioned possibilities of the close-coupling approximation do not concern the near-threshold region. The influence of close coupling in this region can be very important, particularly in the case of degenerate I levels. Due to degeneracy, the cross section appears to be finite at the threshold and oscillating in its vicinity. The close-coupling approximation adequately describes these features. In this book, however, we do not consider such effects. One can see from the above that the use of the close-coupling method requires an accurate choice of the set of levels and even potentials which have to be included in the equation set in accordance with a particular problem. For example, to obtain a normalized cross section it is sufficient to use the two-state approximation, and moreover, we should neglect the diagonal potentials apart from the Coulomb field. It is useful to omit the non-Coulomb diagonal potentials in all cases when the polarization effects are not taken into account. The consideration of polarization requires the solution of a large equation set. For this reason in [3.22] the so-called pseudostate method was proposed. In this book we cannot describe this method in detail, and refer to the reviews [3.23,24].
3.4 Excitation of Highly Charged Atoms In this section we consider some special properties of the inelastic scattering of electrons on highly charged atoms. One of such features, namely the finite value of the cross section at the threshold, was mentioned in Sect. 3.2.1. Here
3.4 Excitation of Highly Charged Atoms
67
we consider in more detail the pecularities connected, in particular, with thresholds of other channels. These pecularities are closely connected with dielectronic recombination which will be considered in the Sect. 5.2 on the basis of a different approach which is more convenient for applications. Here we are interested mostly in the general theory of inelastic scattering on highly charged atoms. The outline of this section is based on the works of Presnyakov and Umov [3.25,26] (see also [3.27]). When we deal with highly charged atoms (z ~ 1) it is convenient to use the Coulomb system of units. In this system the unit of length is aolz, and that of energy is z 2 Ry. Equations (2.2.30) in the Coulomb system are written in the form (.!l'r
+ k 2 )Fr = -1 L z
.!l'
=~_ dr 2
Urr,Fr' ,
(3.4.1)
r'
A( A+ 1) r2
+ 20c
r '
oc
=
1 _ 1I z ,
r
where Urr , are defined by equations (2.2.32) and (3.3.35), but the terms U + 20clr are included in Urr . At z~ 1, the potentials Urr , are almost independent of z. The boundary conditions for the functions Fr, in accordance with (2.2.14) and (2.2.40), are Fr(O) d
=-
k2
= 0,
Fr ~ k-I/2{b rro sin(kor + do) r-+oo
~ + ~ In (2kr) + arg r (A + 1 - i~)
= 0'0
-
,
+ Trro
exp[i(kr + d)]},
(3.4.2)
Eaao .
In place of (3.4.1,2), a set of integral equations of the type (2.2.46) can be introduced. We shall write these equations separately for open channels, r = y (ki > 0), and closed channels r = c(k'/: < 0):
(3.4.3 )
where FAij is the regular solution of the homogeneous equation [see (3.2.3)]. The integral operator G is defined by the relation 00
Gq>(r) =
J G(r, r') q>(r') dr' ,
(3.4.4 ) o where G(r, r') is the radial Coulomb Green's function of (3.4.1). In Sect. 3.4.2 the regularity of Gy will be proved. This means that coupling of open charmels at z ~ 1 is weak and perturbation theory is thus applicable for these charmels. In contrast to the case of neutral atoms, now we have the parameter liz, and for z~ 1, first-order perturbation theory (i.e., the Coulomb-
68
3 Approximate Methods for Calculating Cross Sections
Born approximation) should be a good approximation in the absence of closed channels. In contrast to Gy , the closed channel Green's function Ge contains the poles, and perturbation theory isn't applicable to these channels. This question will be considered in Sect. 3.4.2.
Coulomb Green's Function
3.4.1
The Green's function is determined by (2.2.42-45). We substitute C-II/> in place of F, and write Gr in the form
,1
Gr(r, r)
=
=
-Cl/>(jl, k,r<)F(jl, k, r»,
I/>(jl, k, r) = r Jl + 1/ 2
= A. + 1/2 , where C = C(jl, k)
when r
->
0,
(3.4.5)
jl
C(jl, k)
does not depend on r, and is defined by the equation
dF
dl/> = dr F.
= I/> dr -
(3.4.6)
Now we introduce instead of the two linearly independent functions I/>(jl, k, r) and F(jl, k, r) a new pair of functions I/>± = I/>(±jl, k, r). Using (3.4.6) and an asymptotic expression (2.2.44) for F we obtain an expression for Gr in terms of I/>±:
(3.4.7)
In the case of the Coulomb field Ur = -2a./r, from (3.4.7) we have ,
Gr(r, r ) (p)
-
-
= cot(1tv) FVJl(r) FvJl(r
,_
1
,
)
+ G(p) r (r,
-
,
r ),
--
Gr (r, r ) - -.-(-)FvJl(r < )[cos(21tjl)FvJl(r» - Fv -Jl(r»] , sm 1tjl . jl=A.+l/2,
v=ia./k,
(3.4.8)
Im{k}~O.
The radial functions F VJl are related to the Coulomb functions FA from (3.2.3) for a complex value of k = ia./v: FVJl(r)
=
av = [icot(1tv)
avF).(r) ,
In the particular case when k is real,
_
FVJl
=
(
1ta. coth T
) -1/2
+1
FA'
+ 1]-1/2.
(3.4.9)
3.4 Excitation of Highly Charged Atoms For imaginary k, when v = n is a positive integer and E
FVJl=(;::Y/2pn.l.,
v=n,
69
= _r:x2jn 2, we have
Jl=.A.+1j2.
(3.4.9a)
The radial Coulomb Green's function in (3.4.8) includes two terms. The first term in the case of closed channel (k 2 < 0) is singular (over energy) because of the factor cotnv. The poles at v = n correspond to a series of resonances which converges to the new channel threshold (k 2 -+ -0). The second term GJ!') does not contain any singularities as a function of energy. At k -+ 0, GJ!') is independent of k and is a regular function of r, r'. It is important for applications that the singular part of Gr is factorized over its arguments rand r'. 3.4.2
Potential and Resonance Scattering
We rewrite the integral equation set (3.4.3) to show explicitly the singular part of the closed channel Green's functions: Fy
1
•
= (jyrOFAo + - E GyUyr,Fr" z r'
y = akAtLTST, (3.4.10)
Here Ae does not depend on r and is defined by equation 00
zAe
= cot(nv). E f FeUerlFrldr, r'
(3.4.11)
0
with the function Fe defined by (3.4.9). For v =I- n an iterative method can be applied to get the solution. For y =I- ro we obtain, cf. (2.2.51), (3.4.12) and the set of algebraical equations for A e ,
E [z tan(nv) [)ee l -
Reel ]Ae l
= Rero '
(3.4.13 )
el
where Reel
7o
= Fe(Ueel + Vee/ ) Fel dr,
(3.4.14)
and Rero is defined by (3.4.14) with substitution of FAo in place of Fel. Polarization potentials Vrr' are defined by (2.2.53,54) with Gr = Gy for open channels and Gr = G~p) for closed channels. In contrast to ordinary perturbation theory
70
3 Approximate Methods for Calculating Cross Sections
Vrr' does not contain any singularities. Equations (3.4.12-14) are applicable also for v = n, the singularities being seen explicitly. From (3.4.12) we obtain
Trro
res pot + Trro = Trro '
(3.4.15)
(3.4.16)
The matrix Th!o is similar to that determined by (2.2.52), and corresponds to usual "potential" scattering. The matrix TPro describes the additional "resonance" scattering, which is related to the closed channels. Every closed channel c (a e, k; = tff0 - Eeao) is connected with a set of resonances in the vicinity of v = irxl ke = n (i.e., at values of tffo near Eeao - rx 2 In 2 ). Below we assume that all the resonances are independent, and hence we neglect the off-diagonal integrals Reel, in (3.4.13). Then we obtain Rero z tan(nv) - Ree '
A _ e -
res -
_~
rro -
L
(3.4.17)
RreRero
(3.4.18)
z2 e tan(nv) - Reel z
The scattering amplitude Trr0 reveals the resonances, their positions tffo( c, n) and widths 1> being given by tan(nve)
I
= - Re {Ree} z
(3.4.19) 1> ~
4rx 2 --31m {R ee }. nn z
Each closed channel c (i.e., energetically inaccessible state a e ) corresponds to an infinite set of resonances in the small energy range from threshold tff0 = Eaao up to tffo = Eeao. Hence n 2 rx/~, and usually n ~ 1. For large n, the radial functions P"" ex n- 3/ 2 and in accordance with (3.4.9a) Fe does not depend on v. We see that all the energy dependence of Trro is concentrated in a factor tan(nv). The excitation cross section for the transition ao - a in accordance with (2.2.20) is _
(Jaoa -
na~ k2 2
-2 .
z
'" L.J
0 "oALTSt
gr 1 Tpot rro go
-
res + Trro
12
'
(3.4.20)
and also contains the resonances at energies tff0 = tffo( c, n). One can prove that in the case of nonoverlapping (independent) resonances when (3.4.17,18) are
3.4 Excitation of Highly Charged Atoms
71
applicable, the averaged cross section can be expressed in the form 1
uaoa
=
2JC
BO+OB
f
o Bo-M
O'aoa(CO) dCo
(3.4.21 )
L
[O'Pot(ro, 0+ LUres(ror;c)],
J.oALTST
e
ures(ror.c) = ,
na~ . ~.
IRreRerol2
z4
z 1m {Ree}
kJ
[1-
B(C; -Eeao )] ,
(3.4.22)
where function B(x) = ±1 for x ~ o. In the averaging of O'aoiCo) in (3.4.21) we supposed that in the range 2JC all the matrix elements Rer and Ree are constant, and only the factor tan( nv) is energy dependent. We note that in this case all the interference terms are vanishing. This is relevant both to potential and resonance scattering and to different closed channels. We shall consider now the first-order approximation for Trro and O'aoa. In this approximation we can neglect potentials Vrro in (3.4.16), (3.4.18) everywhere besides the resonance denominator in (3.4.18), in which we have to keep the first nonvanishing term in the imaginary part of Ree. From (3.4.14) we have Ree
= oof-( Fe Uee + -1 L o
Z
r1
Uer, Gr , Ur,e A
+ ...
Fe dr .
) -
In accordance with (3.4.9a) the functions Fe are real. To get the imaginary part of Or(k 2 > 0) it is convenient to use the spectral representation of Or: ()F (') Gr ( r, r ')- 2kpfFk,;.(r)Fk';.(r')dk'_iF n k 2 _ k'2 kA r kA r ,
(3423) . .
where Fk}. = F;. are real functions and P denotes the principal value of the integral. If we determine 1m {Ree} from (3.4.23) we can get the first-order approximation for Tf7 0 • Thus we obtain pot
1, -;Rrro '
Trro
=
Tres rro
= __1 L
(3.4.24)
R're ·R'ero
z2 e tan(nv) - R~e/z + i L IR~eI2 /z2 ' y
where
R~'r" = 7F;"Ur'r"F;." dr,
°
(3.4.25)
whence for closed channels r = c the functions Fe = FV/1 should be substituted in place of F;.. On substituting (3.4.24) in (3.4.22) and (3.4.20) we obtain the final expressions for potential and resonance parts of the cross section in the first order
72
3 Approximate Methods for Calculating Cross Sections
approximation:
(Jpot(ro,r)
=
na5 . Z4
~ • gr IR:'r 12
kJ
go
(3.4.26)
0
-res(r r. ) = na~ . 2 gr (J 0" C 4 k2 • Z 0 go
IR:'c 12
L:y IRJc l2 (3.4.27)
Equation (3.4.26) coincides with the usual expression for the first-order partial cross section which was obtained in Sect. 2.3. It corresponds to the CoulombBorn approximation since we used Coulomb wave functions FA. In accordance with (3.4.21), the total cross section is increased due to the resonance part connected with all closed channels. In the vicinity of the threshold of the channel c when the closed channel becomes open (Yc), the value of R~ro is continuously transferred to R~cro. That means
ares,
=reS(r r. ) _ pot(r ) 0 , c - (J 0, Yc •
o
IR:'c 12
L: IRJc
12
'
(3.4.28)
y
near to the threshold of the channel c, and hence
L: areS(ror; c) =
(Jpot(ro,Yc)
r
80
(3.4.29)
= Ecao -
0
80
= Ecao + 0
When energy reaches the threshold, the terms ares(ror;c) related to this channel disappear in (3.4.21). At the same time a new channel ao - ac is opened. In accordance with (3.4.29) the sum over a of the resonance parts of the total cross section is equal to the threshold value of the cross section of the new channel.
3.4.3 Discussion and Examples In the previous section it was shown that the excitation cross section for the transition ao - a includes besides the usual part (J~~ an additional part a~sa. This additional part is connected with the possibility of electron attachment into a quasi-stationary state acnl of the atom Xz-I with subsequent decay of this state into Xz(a) + e. From (3.4.19), (3.4.18), and (3.4.24) it follows that the width of the resonance in first order is
4a:2 "wlRycl I 2 . nn z y
() = ~
(3.4.30)
3.4 Excitation of Highly Charged Atoms
73
Since () is equal to the autoionization probabilityl Wa (to the open channels y), the factor in (3.4.27,28) is
IRtcl 2 L IR:cI 2
WO
y
(3.4.31 )
One can see that this factor is simply a branching ratio when more than one decay channel is possible. The sum WO
r
r'
(3.4.32) For a given value of n, the most probable are the decays with minimum Eca' and the optically allowed transition '~c - Ar' = ± 1. However at very small Eca" in accordance with (3.4.32) only ve:ry large n are possible and since Wa ex n- 3 , the value of Wa can be very small. Besides the autoionization C -- r a radiative decay c - c' is possible into a stationary state of the atom Xz - 1• Usually in this case an attached electron does not change its quantum numbers: acnA-ac' nA. If the value of n isn't too small we can use the approximation (3.4.28). If we add the radiative transition probability A and use (3.4.31) we obtain for the resonance part of the cross section ~sa
L
=
ares(ror;c) ,
lQUTSrc
ares(r
r· c) =
o ,
upot(r 0,
) Wa(c,r) Yc W.l(c)+A(c) '
(3.4.33)
where upot( r 0, yc) is the threshold value of the ao - a c partial cross section. Since Wa ex z-2n-3 and the radiative transition probability A ex z2(137)-3 (in Coulomb units) is independent of n, we have
A/Wa
~
1O-6z 4 n3.
Usually radiative transitions can compete with autoionization at very large n only, i.e., in a narrow energy interval. Besides this small band (which widens with increasing z), the ratio ares/u does not depend on z. Although the energy range Co = Eaao -;- Ecao where resonance excitation can take place isn't large, in some Gases its part in the total excitation rate proves to be significant. This is especially true for optically forbidden transitions ao - a when there are higher levels ac for which uaoac is large. An illustrative example is shown in Fig. 3.9 for the transition 2s - 3s in the [Li] ion, 0 VI. At small energies the role of closed channels np(n ~ 3) is much larger than the direct 1 We recall that (j = Wa is in Coulomb units z2 Ry; in the Rydberg units, the values of (j and Wa are practically independent of z.
74
3 Approximate Methods for Calculating Cross Sections
60 ___~----,-~----,------. 3p 3d 45 n=oo II
I
I
t 30r-----~~-----+------~
'\§'
..!:!
,}:>
~ 15r-------4--------f=-__~~
o
0.2
0.1
0.3
logu-
Fig. 3.9. Effective cross section for the transition 1$-3s of the lithiumlike ion 0 VI: (1) Coulomb-Born approximation; (2) Cross section with resonances taken into account; u = (8 - AE)jE
excitation. We note however that the branching onto the 38 level decreases with increasing n. It should be emphasized that resonance excitation is important for the total excitation rate only in those cases when the potential excitation cross section O"pot is small for any reason. We note in conclusion that resonance scattering is closely related to dielectronic recombination, which will be considered in detail in Sect. 5.2. In fact these two processes are alternative final channels after the attachment of an electron in a quasi-stationary state: Xz(a') + e Xz(ao) + e --+ XZ-I(acnA)( (3.4.34) Xz-I(a'nl) + liw Among the resonance scattering channels, elastic scattering (a' = ao) and inelastic scattering in different states a' f=. ao can be distinguished.
3.5 Transitions Between Highly Excited Levels 3.5.1 Bom Approximation For transitions between the highly excited levels no, n ~ 1, the cross sections summed over quantum numbers 1m and averaged over lomo are of the most interest. The cross section of the transition no --+ n can be written in the form: 0"11011
=
f(q) =
1ta~
8 ko+k
-4 •
2k2
z
L lomolm
no
dq
J f(q)3' 0 ko-k q
I(no/omolexp(iq·
r)lnlmW ,
(3.5.1 ) (3.5.2)
3.5 Transitions Between Highly Excited Levels
75
where k and q are expressed in lmits z/ao. When no, n are not large, numerical summation in (3.5.2) is used. For highly excited levels no, n ~ 1, such summation is too cumbersome. In the case of the hydrogen atom, however, this summation can be carried out in an explicilt form [3.28]. Moreover, when no, n~ 1 and no, n ~ In-nol, further simplificatilon of the expression for the Born cross sections is possible. Formulas obtained for hydrogen may be applied to the transitions between highly excited levels of any atom, since for large n the system of levels is close to that of hydrogen. We shall rewrite (3.5.2) in the following form: f(q)
=
L
lim (Eo - Eno)(E - En) Eo~En
a'a"
E~Eno
(a'lexp( -iq • r)lal)(a"lexp(iq • r)la') (Eo - En' )(E - En") (3.5.3 )
where a' = n'/'m', a" = nil/limN. It is not difficult to see that the terms with n' i= no, nil i= n added in (3.5.3) vanish when Eo -+ E no ' E -+ En. By using the well-known spectral representation of the Green's function G ( E
') _ '" t/Ja*(r)w,(r')
r, r - ~
E _ Ea
(3.5.4 )
'
we obtain f(q) =
(3.5.5)
lim (Eo - Eno)(E - En) EO---'EnO E---+En
x
JJdrdr'GEo(r, r') exp[iq . (r -
r')]GE(r,r') .
The Green's function for the Coulomb potential is [3.29] G(r,r')
=
T(1 - v) • ( ) . v· L[W I (x/v)M I (y/v)] , 2n x - y V·1 vi"
x
= r + r' + Ir -
•
a - ox
r'l, y
a oy'
L----
= r + r' -Ir -
r'l, v =
y'z2Ry/( -E), (3.5.6)
where Wand M are the Whittakt:r functions of the first and second kind respectively. By means of (3.5.6) the calculation of f(q) can be reduced to the integral f(q) =
~ q
j A(q') dq' ,
(3.5.7)
0
where the function A( q) is expressed in terms of hypergeometric functions
76
3 Approximate Methods for Calculating Cross Sections
F(rx,rl, l;P) and their derivatives [3.28]:
1 { I;.(-no+ , A(q) = (non)2Re 1, -n+ 1)/;.'. (-no, -n)
-Il( -no + 1, -n)/~·( -no, -n + 1) 1 d2
-'6 dq2
[h( -no + 1, -n + 1)/;( -no, -n)
-h(-no + 1, -n)/;(-no, -n + I)]} ,
(3.5.8)
where h(rx, rx') = lrx + rx,-l(l - PO)-IX (l - P )-l F(rx, rx', 1;
l
= ~(po + P + iq), Po = I/no, p = lin,
P_
PoP
,
P) , (3.5.9)
d
- (l - Po)(l - p)' IA = d/;' .
Formulas (3.5.7) and (3.5.8) are exact. To obtain these expressions no simplifying assumptions have been made. Numerical calculations using (3.5.7,8) have been made in [3.7]. We shall now consider the transitions between highly excited levels. By using the known asymptotic expression of the hypergeometric functions in terms of the Bessel functions J, formula (3.5.9) can be considerably simplified [3.28]. When no~ 1, n~ 1, LIn = In - nol ~no,n, (3.5.10)
(3.5.11 )
(3.5.12)
e=
[1 +1 (~:/r/2
(3.5.13)
A correction factor
exp[Lln2 /2(no
+ n)][l + (Llni 14nonr2
is introduced in (3.5.10). This factor ensures that in the limit q - 0, the quantity f(q) from (3.5.7) tends towards the known classical expression for the oscillator
3.5 Transitions Between Highly Excited Levels
77
strength [3.30]: lim fnon(q)
q->O
= nijfnon =
32 ( non)3 I -3 LI ( ) LlnJ.1n(Lln )J.1n(Lln).
n no +n
(3.5.14)
As is known, formula (3.5.14) gives a good approximation even at small values of no, n. The correction factor in (3.5.10) is substantial just for small values of Lin = n - no, no, n. When Linin --> 0 it tends towards unity. One can expect similar results for the cross sections also. As an illustration the results of accurate calculations based on the initial formulas of the Born approximation and the results obtained with the aid of approximate formulas (3.5.10-13) are shown in Fig. 3.10. It is evident from this figure that (3.5.1013) provide a quite satisfactory approximation. The results of numerical calculations using the approximate formula (3.5.10) are given in Table 3.1. For convenience of interpolation the principal dependence
G / '\
I
nO=2 n=3
K
'\
'~ 2
p~
4
.10 4 N",=
~ l:t
~
~ r-==--InO=5 n=6
~ 2/
2
.......
II 0
~ r--
"
4 .10 3
r'~\
- r-
r--
nO=4 n=7
~1 ~
2.A~
o
o
2
I"--
4 X=
---
8
10
r(8-M)/M -
Fig. 3.10. Born effective cross sections for the transitions between highly excited levels: (I) Numerical calculations by means of exact formulas of the Born approximation; (2) Calculations with the approximate formula (3.5.10)
78
3 Approximate Methods for Calculating Cross Sections
of the cross sections on no, n, An is given in explicit fonn
z Ry . To . ffno(An, 2
8 0)
(3.5.15)
.
The values of ffno are given in Table 3.1. The function ffno can be approximately expressed as follows:
ffn o
~
8(noni (no + n)4An
+ 8n~ (no + n)3
(1 _0.25) In (1 + 8 (1 _0.6) (~3 + +
0 )
An
Eno
(no
An
(3.5.16)
n)An) tfo/Eno. n2 1 + tfo/Eno
Under the conditions 1 ~An~no, n, (3.5.15,16) give the well-known classical expression for the cross section obtained by Stabler [3.31]. The rate coefficient (vcr) averaged over the Maxwellian distribution can be written in the fonn similar to that of (3.5.15):
nony (Z2Ry)1/2 (AE) 3 I ( A;). T exp -T 4>no(An, T)[cm s- ]. (3.5.17) Table 3.1. Born effective cross sections for transitions no - n between highly excited levels. The function ~.o (.dn, If0) is given in tabular form. The cross sections are expressed in terms of ~.o by means of the formula lI:a~ I (non)3 z 2 Ry 00'0' = -;4 n~ (Lln)3 To~·0(Lln,80) no ../80/E.o Lin 0.20 0.28 0.40 0.57 0.18 0.80 0.40 1.13 0.64 1.60 0.90 2.26 1.16 3.20 1.42 4.53 1.68 9.05 2.21 1.81 x 101 2.74 3.62 x 101 3.27 7.24 x 10 1 3.80 1.45 x 102 4.33 2.90 x102 4.86 5.79 x 102 5.38 1.16 x 103 5.87
10 2
0.05 0.36 0.64 0.86 1.05 1.21 1.37 1.66 1.96 2.25 2.53 2.83 3.11 3.40 3.66
100
50 4
0.19 0.50 0.70 0.84 0.94 1.03 1.18 1.33 1.48 1.63 1.78 1.92 2.07 2.20
2 0.03 0.10 0.24 0.43 0.66 0.90 1.16 1.42 1.69 2.22 2.75 3.28 3.81 4.34 4.87 5.40 5.89
0.01 0.Q7 0.22 0.46 0.71 0.92 1.11 1.28 1.44 1.74 2.04 2.33 2.63 2.92 3.21 3.50 3.77
4
0.Q3 0.16 0.40 0.69 0.91 1.06 1.17 1.27 1.44 1.59 1.75 1.90 2.06 2.21 2.37 2.52
0.01 0.04 0.11 0.24 0.43 0.66 0.91 1.16 1.42 1.69 2.22 2.75 3.28 3.81 4.34 4.88 5.40 5.89
2
4
0.03 0.09 0.24 0.47 0.71 0.93 1.12 1.29 1.45 1.75 2.05 2.34 2.63 2.93 3.22 3.51 3.78
0.01 0.07 0.20 0.44 0.73 0.95 1.10 1.21 1.48 1.56 1.64 1.79 1.95 2.10 2.26 2.42 2.56
3.5 Transitions Between Highly Excited Levels
79
The values of tPno are given in Table 3.2. Using (3.5.16) it is possible to obtain the approximate formula for the function tPno '
tPn (LIn, T) o
~ 2.18 {
8(non)2 (no+n)4L1n
(1 _
0.25) q>(x) LIn (3.5.18)
+ (no
8n~ + n)3
(1 _LIn
0.6)
(~ + (no + n)Lln) n2
3
[1 _Xq>(X)]}
where
q>(x)
x
~ In (1 +
1 + 1.4yx ) ,
yx(l
+ l.4x)
= Eno/T, Y = exp(0.5772) =
(3.5.19) 1.78 .
It should be remembered that in the region of low energies $, the Born approximation as a rule does not satisfy the normalization condition. The normalized cross sections can be calculated in the quasi-classical approximation (Sects. 3.5.2, 3).
Table 3.2. Rate coefficients (VO"non) for transitions between highly excited levels in the Born approximation. The function cPno(Lln, T), which is given in tabular form, can be used to calculate the rate coefficients according to the formula 10
1
(VO"non) =
7 -8 n5
100
no
LIn EnolT 0.01 0.02 0.04 0.08 0.16 0.32 0.64 1.28 2.56 5.12 1.02.10 1 2.05.10 1 4.10.10 1 8.19.10 1 1.64.102 3.28.102 6.55.10 2
non (Lin)
3 (2 z Ry
T
LIE ) y/2 exp (-r cPno(Lln, T) [cm s
3 -1
10 8.34 7.76 7.18 6.61 6.03 5.46 4.88 4.31 3.75 3.19 2.65 2.13 1.65 1.22 0.86 0.57 0.36
100
50
2
4
5.55 5.24 4.92 4.61 4.29 3.97 3.65 3.33 3.00 2.67 2.32 1.97 1.61 1.25 0.92 0.63 0.41
3.57 3.41 3.25 3.08 2.92 2.76 2.59 2.42 2.23 2.04 1.83 1.60 1.34 1.07 0.80 0.56 0.37
8.36 7.78 7.20 6.63 6.05 5.47 4.89 4.32 3.75 3.19 2.64 2.11 1.61 1.16 0.78 0.48 0.36
]
2
4
5.75 5.43 5.11 4.79 4.47 4.14 3.82 3.49 3.15 2.79 2.43 2.04 1.64 1.23 0.84 0.52 0.29
4.17 4.00 3.83 3.66 3.49 3.31 3.13 2.94 2.73 2.51 2.25 1.95 1.60 1.22 0.84 0.52 0.30
8.17 7.78 7.20 6.62 6.05 5.47 4.89 4.32 3.75 3.18 2.63 2.10 1.60 1.15 0.77 0.46 0.25
2
4
5.77 5.45 5.13 4.81 4.49 4.16 3.84 3.50 3.16 2.81 2.44 2.05 1.64 1.22 0.83 0.50 0.26
4.26 4.09 3.92 3.75 3.58 3.40 3.22 3.03 2.82 2.59 2.32 2.01 1.64 1.24 0.84 0.50 0.27
80
3 Approximate Methods for Calculating Cross Sections
3.5.2 Transitions Between Highly Excited Levels in the Quasi-Classical Approximation When the principal quantum number n is large, the motion of an atomic electron can be treated as quasi-classical motion. We shall consider the problem of the calculation of the probability for the transition no - n in a quasi-classical limit Ii. ---+ 0. 1 The quasi-classical theory may be developed in different ways. One may pro~eed from the wave packets which in the limit of Ii. ---+ 0 give the classical trajectories. We shall use below a somewhat different approach which enables one to treat the distortion of motion of the highly excited electron during the collision in the simplest way. We proceed from the following representation of the atomic wave function:
'l'a ex:exp (kSa) ,
(3.5.20)
where Sa is the classical action function. The probability of transition ao - a is then written in the fonn
Waoa = lim 1('l'~O)(t)I'l'ao(t»12 1-+00
ex:
(3.5.21)
I~~ I(exp (kS!O») lexp (kSao) >12
where the superscript 0 corresponds to an unperturbed atom. To detennine the action function in the quasi-classical limit Ii. ---+ 0, one may use the classical Hamilton-Jacobi equation. The remainder of this section is based on [3.34], where this approach has been developed. 2 We shall write the action function Sao(t) in the fonn Sao(t) = S~)(t) + LlS(t) where LlS(t) is the increment of the action function due to the collision. When t ---+ -00, LIS ---+ O. It is convenient to use as dynamical variables the phase variables Uj and their conjugated momenta I j . The phase variables vary between o and 211:. The unperturbed action function is defined by [3.36] S!O)
=L
Ijuj -
(3.5.22)
Eat.
j
From the Bohr quantization conditions it follows that II = nli.,
lz
= Iii.,
h
= mli. ,
(3.5.23)
where n, I, and m are the principal, orbital, and magnetic quantum numbers;
The purely classical impulse approximation is developed in [3.31-33]. The correspondence principle method has been developed by Percival and Richards [3.35]. In this article one can also find a survey of classical, semiclassical and quantaI methods for collisions between charged particles and highly excited atoms. 1
2
3.5 Transitions Between Highly Excited Levels
81
a = nlm. Using (3.5.22,23) we obtain
Waoa
= t~ I (2~ )3
J! J
dUl dU2du3 exp [-
t(S~O) - S~~») + t LIS]
t~~ I(2~)3 Jdu exp (-ik . u + tLlS) 12 ,
=
2 1
(3.5.24)
where the vector k has the components LIn = n - no, Lli = 1-/0, LIm = m - mo. lt is not difficult to show that the transition probability (3.5.24) satisfies the unitarity condition independently of the approximation used in calculating LIS. Since the summation over the final states a is equivalent to summation over k, we have
~ Waoa = (2~)3 Jdufdu' c5(u -
u') exp [tLlS(u) - tLlS(U')]
=I.
The Hamilton-Jacobi equation for the action function S is as at + H (0) ( Uj,
as ) OUj
+ V ( Uj,
as )_ ou/ t - 0 ,
(3.5.25)
where H(O) is the unperturbed Hamiltonian function of an atom and V(Uj, as/OUj, t) is the perturbation induced by the incident particle. When LIS ~S(O) in first-order classical perturbation theory, the following approximate equation for LIS can be obtained:
a
a
~LlS - wo~LlS
UUl
~
=
-v
(OS~~) Uj, -a-' ~
t) .
(3.5.26)
We take into account that for the particular case of the Coulomb field Eao = E no ' and the unperturbed Hamiltonian function H(O) depends on phase variable Ul only. The quantity Wo = aH(O) / all = 2z2Ry /ling is the classical frequency for an electron with binding energy Eno' The term V(Uj, oS(O) / oUj. t) in (3.5.26) includes the derivatives of unperturbed action function oS(O) / au). The right-hand side of (3.5.26) can be expanded in a Fourier series, V=
E Vq(t) exp (iq
• u)
q
=
(3.5.27)
E q], Q2'
Q3
VQIQ2q3(t)exp[i(QlUl+q2U2+q3U3)],
where the quantities qJ, q2, q3 are integers. With the aid of expansion (3.5.27), the solution of (3.5.26) can be written in the following form: LlS(t) =
E Cq(t)
exp (iq . u - iqlWOt)
q t
Cq(t) =
J Vq(t') exp (-iqlwOt')dt' . -00
(3.5.28)
82
3 Approximate Methods for Calculating Cross Sections
Thus
_I (2n)3 1 2Ind . i 7C '" e u) 12 , u exp (-lk· u+ h
Waoa -
q
0
iq'
(3.5.29)
where 00
Cq=Cq(oo)=
I
Vq(t)exp(-iwot)dt.
(3.5.30)
-00
Fonnulas (3.5.29, 30) enable the probability of the transition ao - a to be calculated in the quasi-classical limit within the framework of the classical perturbation theory AS ~S(o). The validity condition AS ~S(o) for (3.5.29) differs substantially from the validity condition for quantum perturbation theory AS ~ h. In fact, when n is large it follows from (3.5.22,23) that S(O) '" nh~h. Therefore the classical perturbation theory is valid in the wider range AS ~ nh. The first order of quantum perturbation theory is obtained from (3.5.29) by putting exp(iAS/h) ~ 1 + iAS/h. Then (3.5.31 ) The calculation by means of (3.5.29) requires the use of a Fourier expansion of the classical interaction potential V(Uj,fJS(O)/fJUj,t). Such calculations are extremely cumbersome. It is known, however, that in the quasi-classical limit the quantum matrix element of the time-dependent interaction V(t) coincides with the Fourier component Vk(t)(k j = n - no, k2 = 1- 10 , k3 = m - mo) : (no/omolV(t)lnlm) -+ Vk(t) .
(3.5.32)
Hence (3.5.31) is equivalent to the first order of quantum perturbation theory for the probability of the transition no/omo - nlm caused by a time-dependent potential V(t). Thus the relation (3.5.32) enables one to calculate the increment of the action function AS and the transition probability Waoa using the quantum matrix elements. The summation over q = (q], Q2, Q3) in (3.5.29) means that the transitions via virtual levels a' == n' I'm' are taken into account. To obtain the probability for the transition no - n one has to sum with respect to 1m and to average over lomo : (3.5.33 ) For the quasi-classical probability (3.5.29) this is equivalent to summation with respect to k2 = I - 10 , k3 = m - mo, and averaging over 10 , mo. Calculation of the probability Wnon can be simplified if one assumes that AS does not depend on U2 and U3, and extends the summation with respect to k2 and k3 from -00 to 00. Then, using the average quantities Cq that do not depend on
3.5 Transitions Between Highly Excited Levels
the angular momenta q2 W,,'
83
= 10 - I' and q3 = mo - m', one can write
~ I;. {dU exp [-i(n - ",ju + k~ C
q";"]
I' ,
(3.5.34)
where the notations u = u\, q = qI are introduced. It is convenient to define the average value Cq by means of the following relation: 21
"L..J
no lomol'm'
ICnolomo n'l'm' 12 ,
q- n' - no , (3.5.35)
00
Cnolomon'l'm'
= J (no/omolV(t)ln'I'm')exp(-iqroot)dt. -00
This definition ensures an accurate result for the probability W~on in first-order quantum perturbation theory. The effective cross section for the transition no - n is 00
O'non
= 2n J p dp Wnon(P) o
(3.5.36)
.
When formula (3.5.34) for the probability Wnon is used we obtain the normalized cross section. 3.5.3
Transitions Between Adjacent Levels Lin
=11
Now we shall consider the special case when only matrix elements Vq with q = Lin = ±1 exist. We shall assume that C+ 1 = C- 1 = C. In this case the analytical expression for the transition probability can be obtained [3.39]: (3.5.37) where hn is the Bessel function, Lin = In - no I . We shall use the dipole approximation for the interaction potential V(t)
= ed . R/R3
,
(3.5.38)
where d is the electric dipole moment of the atom. In order to eliminate the pole in the potential it is convenient to define R in the following way:
R=r+~(Jp2+pij_p) , 1 The classical path first-order approximation with the cutoff procedure to ensure conservation of probability has been used for transition between adjacent levels in [3.37,38]. The results obtained by this method are close to those given below.
84
3 Approximate Methods for Calculating Cross Sections
where r is the radius vector of the outer electron, p is the vector of the impact parameter p which lies in a collision plane and is perpendicular to the velocity vector v. The parameter Po rv n2ao / z is introduced to avoid the pole in W at P = O. The magnitude of Po has to be taken so that at high velocities of the outer electron the quasi-classical cross section coincides with the quantum Born cross sections. When the energy of the outer electron Iff ~ lEn I both in the case of neutral atom and in the case of an ion, the rectilinear trajectory may be used: r(t)
= p + vt
(3.5.39)
.
Defining roo in (3.5.35) by means of the symmetrical relation no +nz2Ry
roo
= (non)2 T '
liroo(n - no)
= En -
Eno '
(3.5.40)
we obtain C2 _ q -
4 ( Ii ) 2 lX~on ):(13) mv q4(P5 + p2) .. ,
(3.5.41 )
2 no21nonq3 lXnon = (no + n)non z2' q = LIn, ~(f3)
= f32[~(f3) + Kr(f3)]
(3.5.42)
,
(3.5.43 )
2 2 13 - no + n z Ry . / 2 -q(non)2hvYPo+P ,
where Ko(f3) and KJ (13) are the modified Bessel functions, and Inon is the oscillator strength for the transition no ~ n. In the Kramers approximation for 1non we have 2 lx
non
32 3nv'3
= -- .
(non)2 fXnon (nO + n)4z2'
~
1.40
(no
non + n )2z
(3.5.44)
The more accurate calculation using (3.5.14) gives for the case n = no + I a numerical factor in (3.5.44) of 1.3l. The function ~(f3) can be approximately fitted to the simple formula ~(f3) ~
(1
+ nf3)
exp (-213) •
(3.5.45)
The error does not exceed 10 percent. Formula (3.5.37) and the dipole approximation are applicable for transitions with LIn = 1 only. When An > 1 the expression (3.5.37) takes into account only transitions via the virtual levels no ~ n' ~ no + 1 ~ no + 2 . .. but it ignores the direct transitions no ~ n. Therefore the asymptotic dependence of the cross section on the electron energy C will not be correct. Moreover, in the region of low energy of the outer electron C ~z2Ry, the higher multipole interactions
3.5 Transitions Between Highly Excited Levels
85
12r-------,--------,------~,_----__.
Fig. 3.11. Cross-sections for the transitions
n = no
+ 1 between highly excited levels:
(1) Born approximation; (2) Quasi-classical cross sections for the transitions 10-11 and 100-101 of neutral hydrogen; (3) Quasi-classical cross sections for ions with z = 4; (4) Quasi-classical cross section for ion with z = 8
Table 3.3. Quasi-classical (normalized) cross sections for transitions no -+no±1 in neutral hydrogen. Function ff nO( tf0). Gno,no±l
= 1ra~no(no ±
1)\Ryltfo )ffno(tfo)
tfo/Ry no: 10
20
30
40
50
100
150
200
250
0.01 0.02 0.04 0.08 0.16 0.32 0.64 1.28 2.56 5.12 10.24
0.049 0.144 0.325 0.664 1.13 1.68 2.21 2.67 3.06 3.39 3.69
0.090 0.233 0.500 0.921 1.44 2.00 2.54 3.00 3.37 3.70 4.00
0.139 0.324 0.655 1.13 1.67 2.24 2.77 3.22 3.60 3.92 4.22
0.186 0.413 0.791 1.30 1.85 2.42 2.95 3.40 3.77 4.10 4.40
0.414 0.790 1.29 1.85 2.42 2.98 3.50 3.94 4.31 4.63 4.93
0.617 1.07 1.61 2.19 2.75 3.30 3.82 4.25 4.62 4.94 5.24
0.791 1.29 1.85 2.42 2.98 3.53 4.04 4.48 4.84 5.17 5.42
0.942 1.47 2.03 2.60 3.16 3.70 4.21 4.65 5.02 5.34 5.63
0.016 0.052 0.138 0.338 0.670 1.14 1.66 2.12 2.51 2.85 3.15
must be taken into account [3.40]. In the case An = 1 the dipole approximation provides good results. The results of numerical calculations by means of formulas (3.5.36,37,41) and the quantum Born approximation for the transitions 10--11 and 100--101 are compared in Fig. 3.11. In the region tf ~z2Ry, the Born approximation gives an overestimate of the cross section. This is because of the fact that when p is small the probability WI calculated by first-order perturbation theory is far greater than unity. When formula (3.5.37) is used, the maximum value of W(p) is approximately equal to 0.3. At high energies, the quasi-classical approximation and the Born approximation coincide.
86
3 Approximate Methods for Calculating Cross Sections
Table 3.4. Quasi-classical cross sections for transitions no
-+
no ± 1 in hydrogenlike ions.
Function Fno(z,Go).
O"no.no±1 =
na5
- 4 no(no± Z
3
2
1) (z Ry/Go)Fno(z,Go)
100 Z
o.ot 0.02 0.04 0.08 0.16 0.32 0.64 1.28 2.56 5.12 10.24
2
4
00
2
4
00
2
4
8
00
0.06 0.15 0.33 0.67 1.11 1.56 1.95 2.29 2.60 2.89 3.18
0.14 0.33 0.64 1.01 1.38 1.72 2.04 2.34 2.63 2.91 3.18
0.41 0.65 0.92 1.21 1.50 1.79 2.07 2.36 2.64 2.91 4.42
0.41 0.79 1.29 1.85 2.39 2.85 3.23 3.56 3.86 4.14 4.42
0.79 1.29 1.82 2.28 2.67 3.01 3.31 3.60 3.88 4.15 4.42
1.65 1.94 2.23 2.52 2.80 3.07 3.34 3.62 3.89 4.16 4.95
0.79 1.29 1.85 2.42 2.95 3.39 3.77 4.09 4.39 4.68 4.96
1.29 1.85 2.38 2.84 3.22 3.55 3.85 4.14 4.41 4.69 4.96
1.81 2.28 2.67 3.01 3.31 3.60 3.88 4.15 4.42 4.69 4.96
2.22 2.52 2.79 3.07 3.34 3.61 3.88 4.15 4.42 4.69 4.96
Table 3.5. Quasi-classical rate coefficients (vO"no,no±l) for neutral hydrogen. Function IPno(T). (VO"no,nO±I) = 1O-8no(no ± 1)3(Ry/T) 1/2 exp( -AE/T)lPno(T) [cm3s- l ] T/Ry no
10
20
30
40
50
100
150
200
250
0.01 0.02 0.04 0.08 0.16 0.32 0.64 1.28
0.052 0.12 0.29 0.62 1.15 1.87 2.72 3.62
0.130 0.29 0.61 1.14 1.87 2.77 3.75 4.71
0.21 0.46 0.89 1.54 2.38 3.36 4.38 5.37
0.30 0.62 1.13 1.87 2.78 3.80 4.85 5.84
0.37 0.76 1.35 2.14 3.10 4.15 5.21 6.20
0.78 1.35 2.15 3.11 4.17 5.28 6.35 7.34
1.09 1.75 2.69 3.72 4.93 5.94 7.02 8.00
1.34 2.14 3.10 4.17 5.30 6.42 7.49 8.46
1.56 2.42 3.43 4.53 5.67 6.79 7.85 8.83
Table 3.6. Quasi-classical rate coefficients (vO"no,no±l) for hydrogenlike ions. Function IPno(z, T). (VO"no.no±1 )
-8
10 = -3-no(no ± 1)3(z 2 Ry/T) 1/2 exp( -AE/T)lPno(Z, T) Z
T/Z2Ry no Z
0.01 0.02 0.04 0.08 0.16 0.32 0.64 1.28
10 2
4
00
2
50 4
00
0.14 0.31 0.62 1.13 1.80 2.57 3.36 4.13
0.30 0.60 1.06 1.64 2.31 3.00 3.69 4.35
0.69 1.08 1.56 2.09 2.67 3.26 3.85 4.44
0.77 1.36 2.14 3.08 4.08 5.06 5.95 6.75
1.34 2.11 3.01 3.92 4.80 5.60 6.32 6.98
2.37 3.22 3.99 4.70 5.35 5.93 6.50 7.07
3
I
[cm s- ]
2
100 4
8
00
1.34 2.14 3.10 4.15 5.20 6.19 7.08 7.87
2.03 3.01 4.04 5.03 5.94 6.74 7.45 8.10
2.68 3.72 4.68 5.55 6.31 6.97 7.58 8.17
3.13 4.17 5.05 5.81 6.49 7.06 7.63 8.19
3.5 Transitions Between Highly Excited Levels
87
The results of numerical calculations by means of formulas (3.5.36,37,41) for transitions L1n = 1 in hydrogen and hydrogenlike ions are given in Tables 3.3 and 3.4. The rate coefficients averaged over the Maxwellian distribution are given in Tables 3.5 and 3.6. Similar to Tables 3.1 and 3.2 for the Born cross sections, Tables 3.3-6 give the values of the functions ff' no and
4 Collisions Between Heavy Particles
Collisions between heavy particles are treated here in the impact-parameter approximation. In the two-state approximation, a simple formula for the transition probability is obtained which is correct in both limiting cases of high and low velocities, and provides reasonable interpolation in the intermediate case. The simple formulas for the case of the multipole potentials and the numerical results for the most interesting cases of Coulomb and dipole-dipole interactions are given. Charge exchange cross sections are also estimated. A more detailed account of the physics of collisions between heavy particles can be found in [4.1-7].
4.1
Impact-Parameter Method
4.1.1
General Formulas
The collisions of atoms with heavy particles (e.g., atoms, ions) in a wide range of velocities can be described quasi-classically by considering the distance between the centers of the colliding particles as an explicit function of time R(t). If the colliding particles are neutral the trajectory R(t) is usually assumed to be rectilinear: R(t) = p + vt, where p and v are the impact parameter and relative velocity. With such an approach the effective cross section for the transition of a system from one state to another is determined by the formula 00
(J
= 21t
J W(p, o
v)pdp,
(4.1.1)
where W(p, v) is the probability of the transition in a collision with impact parameter p and relative velocity v. The problem of calculating the transition probability W(p, v) reduces to a solution of a system of equations for the timedependent amplitudes of the state, which we write in the form ',J,.dak" . = L..J Vkm(t) exp (lWkm t) am, t m
In d-
(4.1.2)
where hWkm = Ek - Em is the energy difference between the unperturbed levels, and Vkm are the matrix elements of the interaction, depending on the parameters p and v. In order to calculate the probability of the transition 0 -+ n it is necessary to find the solution of the system (4.1.2) satisfying the initial conditions ak( -00) = ()Ok.
I. I. Sobel'man et al., Excitation of Atoms and Broadening of Spectral Lines © Springer-Verlag Berlin Heidelberg 1995
(4.1.3)
4.1 Impact-Parameter Method
89
The required probability is given by WOn =
lan (00)1 2 •
(4.1.4)
The matrix Vkm is Hermitian. Therefore the amplitudes of the states an and also the transition probabilities WOn satisfy the normalization conditions
L: lan(x)1 2 = I, L: WOn = n
(4.1.5)
I .
n
By integrating the system (4.1.2) in first-order perturbation theory, i.e., assuming in the right-hand side of (4.1.3) am(x) = bmo , it is not difficult to obtain the. quasi-classical formula of the Born approximation,
wt" = 11,21 1-L VOn(t) exp (i Wno t) dt 12 00
,
(4.1.6)
In many cases the approximation (4.1.6) proves to be completely unsuitable. This approximation does not satisfy the normalization conditions (4.1.5), as a result of which W B can exceed unity, which contradicts the physical meaning of this quantity. The approximation (4.1.6) often gives incorrect results at low velocities even when W B ~ 1. All these deficiencies are inherent also in the Born approximation for the collisions between electrons and atoms. However in the case of collisions between heavy particles the thermal velocities are considerably smaller than the thermal velocities of electrons and the errors of the Born approximation prove to be far greater than the errors in the case of electronic collisions. Therefore it is necessary to solve the system (4.1.2) without recourse to the series expansion. A general survey of the problem is given in [4.3-5]. We shall consider below only the cases when the main contribution to the transition probability is given by a multipole interaction at comparatively large distances, larger than atomic dimensions. In these cases the maximum values of the cross sections are of the order of atomic dimension squared or greater. To investigate the properties of the solutions of the system (4.1.2) we shall restrict ourselves to the consideration of a system of two equations, which is analogous to the two-state close coupling approximation in the general theory of inelastic collisions. The exact analytical solution of the system of the two equations can be obtained only for some special potentials Vkm. One of the well known example of such solution is the so-called Rozen-Zener model. At present many such models are being investigated [4.3-5]. These models however do not describe several potentials met in practice. For example, the exact solutions do not exist for the multipole potentials V oc R- n . It is of interest therefore to use another approach based on an approximate solution of the system of two equations (4.1.2) not connected with some special form of the potentials. It is possible to construct an approximate solution correctly describing both limiting cases of high and low velocities: v - t 00 and v - t O. Examination of special examples, for which there exists an accurate solution of
90
4 Collisions Between Heavy Particles
the two equations, shows that this approximation also describes sufficiently well the intermediate range.
4.1.2 Two-State Approximation We shall consider the transition 0 - t 1 and retain in the system (4.1.2) only the two equations corresponding to the levels 0, 1. We shall introduce the notation Vo
= Voo/h,
VI
= Vu/h,
Veil!'
= Vodh = vto/h,
w = (EI -Eo)/h, where V is a real quantity. The substitution
x
= vt,
ao =
o [-~ (q> + ~x) ]
(4.1.7)
b exp
al = b l exp
[~ (q> + ~ x ) ]
leads to the system of two equations
I .db = -1Vb o + (1- + -w) dx v v 2v
.dbo = dx
1-
(1v
w)
- Vo - -
2v
l 1-
bo + - Vb l
v
VI
,
(4.1.8) bl
,
with the initial conditions
bo = exp
(i~x),
bl(-oo)
= o.
(4.1.9)
The probability of the transition 0 - t 1 is obviously given by W = Ib l (00 W. If the states 0,1 are the unperturbed states of electrons in the system of two colliding particles, the transition is described by nondiagonal matrix element V of the interaction, and the diagonal matrix elements Vo = VI = 0, then
.dbo 1 = -Vb l dx v
1-
W
-
-bo 2v'
.db l 1 W 1 - = -Vbo - -b l dx v 2v
(4.1.10)
.
The exact solution of this very simplified system can be obtained only in few special cases.
4.1 Impact-Parameter Method (i) The case of zero-energy defect w with the initial conditions (4.1.9) is
(!v-ooJ V dX) ,
bo = cos
bl
=
=
o.
-i sin
91
The solution of the system (4.1.10)
(!v-ooJ VdX)
(4.1.11)
and
(!v-oo7
W = sin2
V
dX)
(4.1.12)
(ii) Square well V(X) = Vc at Ixi < Po and V(x) =0 at solution of the system (4.1.1 0) yields
=
W
~V~ 2 +w
4Vc
(iii) V(x) obtains W
=
sin 2 (po. v
J4V~ + w 2 )
V
•
Ixl >
Po. The exact
(4.1.13)
Vcosh-I(yx), y being a constant. For the transition probability one
(nw) sm. (nvc) -- .
= cosh-2 -
2
2yv
yv
(4.1.14)
Let us assume now that the states 0, 1 are the states of the electron of a system of two particles at the fixed internuclear distance R with energies Eo(R),EI (R) (quasimolecular complex). Ifthe principal contribution to the transition probability 0 --t I is given by the "point of intersection" of the terms Eo(R) = EI(R) the system (4.1.8) leads to the Landau-Zener formula [4.8]. W
<5
= 2 exp (-<5)[1
=
- exp (-<5)]
2nV2(x)
v2
14L _4fJl1 dx
(4.1.15) (4.1.16)
dx x =Xo
The point Xo is given by (4.1.17) For more general assumptions about the form of the functions Vo(x), VI (x), V(x) and the magnitude of initial energy defect w, the system of coupled equations (4.1.8) can be solved only approximately. Various approximate methods have been discussed in [4.6]. An approach to an approximate solution of the system (4.1.8) with a wide region of validity has been proposed in [4.9]. Introducing the new function K(x) by the relation K(x) = bl(x)Jbo(x)
(4.1.18)
we can transform the system (4.1.8) into a nonlinear Riccatti equation for K(x). Solution of this equation permits to determine K(x). The probabilities are given
92
4 Collisions Between Heavy Particles
by b (X)2 _
2
1
- 1 + IK(x)l2'
o
bl(x)
=
IK(x)i2 1 + IK(x)12 .
(4.1.19)
According to (4.1.19) the normalization (unitarity) conditions (4.1.5) are satisfied independently of the approximation used in the calculation of K(x). The Born approximation for the transition probability can be deduced for small values of
Vivo An approximate solution of the equation for K(x) leads to the following transition probability W
1 J = _.
00
V
+ VI WI - Vo I~ w,
cx(x) = (w
When
dx V exp
w= I~v
{
x iJ dXI 0
-00
Vo)/v.
it can be assumed that
1 dxVexp {~JdXI[W2+4V2(Xd]1/2}12
-00
(4.1.20)
(4.1.21)
V 0
The interpolation formula (4.1.20) agrees with the accurate values of the transition probability in both the limiting cases v -+ 0 and v -+ 00. Examination of various specific potentials reveals that (4.1.20) gives good results also in the intermediate range. For example, (4.1.20) yields exact results in the aboveconsidered cases of square well (i) and zero-energy defect w = 0 (ii). In the case (iii) the expression for W, obtained by means of (4.1.20), coincides with (4.1.14) for nw/2yv < 1. For nw/2yv~ 1, when W is exponentially small, (4.1.20) gives the correct order of magnitude for the preexponential factor. By means of (4.1.20,21) it is possible to obtain the Bates results [4.10]. Instead of the Landau-Zener formula (4.1.15) the evaluation of the integral in ( 4 .1.20) yields when <5 ~ 1 const. exp( -(5) when <5 ~ I .
W _ {2<5
-
For small <5 this formula coincides with the Landau-Zener formula, and for large <5 differs from it only by the constant pre-exponential factor of order unity. It can be shown that in the intermediate region 0.2 ~ <5 ~ 5 the method considered above leads to the results which differ from the Landau-Zener fromula by no more than 20 percent. The general formula (4.1.20) has been compared with the results of numerical solution of the system of two equations for different potentials. In all cases it gives good interpolation between two limiting cases v -+ 0 and v -+ 00. It has also been shown that the cross section for the excitation of atomic hydrogen into
4.2 Transitions Caused by a Multipole Interaction
93
the stationary states 2s and 2 p in the collision between the two hydrogen atoms calculated by means of formula (4.1.20) differs from the cross section obtained by means of an accurate numerical solution by no more than several percent [4.3,11,12]. The difference of the results for the excitation by charged particles does not exceed 30 percent [4.13].
Transitions Caused by a Multipole Interaction
4.2 4.2.1
Two-State Approximation
We shall assume that one of the two conditions, w~ IVI
-
Vol,
IVI ~ IVI -
(4.2.1 )
Vol,
is fulfilled and take expression (4.1.21) for the transition probability. The second of the inequalities (4.2.1) can be fulfilled, for example, in those cases when the matrix element V decreases with increasing R more slowly than Vo, VI, and the principal contribution to the transition probability is given by the interaction at large distances, which considerably exceed the dimensions of an atom. The approximation (4.2.1) under the conditions (4.1.21) is of interest for many applications such as the transfer of excitation energy in the collisions of atoms with a small resonance defect, the excitation in a collision with an ion, and so on. The matrix element V can be calculated accurately only in the case of collisions between two atoms of hydrogen or collisions of a hydrogen atom with a structureless charged particle. It is not difficult to show that in a collision of two atoms of hydrogen, as a result of which the states of both atoms change, the matrix element V has the form V
1
n
= -;; - exp (-bIR) 2:: R
k=-n+1
C --f - exp (-b R) R 2
n
2::
~
R~'
(4.2.2)
k=-n+1
where n is determined by the multipole order of the transition under consideration: if one of the atoms changes from the state al to the state a~ and the other changes from the state a2 to the state a~, electric multipole transitions al -+ a~,a2 -+ a~, of the orders "I and "2 being allowed, then n = "I + "2 + 1. The constants b l and b2 are expressed in terms of the ionization potentials I of the states aJ, a~ and a2, a~ : b l = .j2fj + ..j2l[, b2 = /2l2 + (the quantities I are given in atomic energy units 2Ry.) The constants q and Cf are expressed in terms of the quantum numbers of the levels under consideration, and besides q and Cf, and 1 are linked in such a way that when R -+ 0, VCR) -+ const. In the case of collisions between arbitrary atoms the matrix element V must have the same basic properties as (4.2.2). We shall therefore assume that
V2iJ.
VCR)
= l/Rn - exp (-bR)f(R)
,
(4.2.3)
94
4 Collisions Between Heavy Particles
where the function f(R) is a polynomial of the same sort as in (4.2.2) and satisfies the condition V(R) -+ const when R -+ 0, and A is the constant with dimensions s-I cmn. The trajectories of the colliding particles will be considered to be rectilinear: R2 = p2 + v2(2 = p2 + X2 . We shall substitute (4.2.3) into (4.1.21), replace the quantity vw 2 + 4V2 by w + 2 V, which retains the basic analytical properties and limiting cases and which differs from the primary quantity by no more than the factor of ,j2, and integrate with respect to the complex variable z:
W=Re{~v f
V(p2+z2)exp
-00
[i~JV(P2+zI2)dzl+WZ]dZ}. v0
(4.2.4)
We shall assume further that the principal contribution to the transition probability is given by the distances R > Ro = l/b, for which V ~ A/Rn. To clarify the further approximation we shall assume at the beginning that n = 2 and in integrating use a contour, closed in the upper half-plane of z, with a cut along the imaginary axis from i 00 to ip. When calculating the integral we take the function exp (iwzlv), monotonic along the imaginary axis, outside the integrand sign at the point Zl, at which the derivative of the index of the exponent vanishes: Zl
= iJ~ +p2.
(4.2.5)
(The point ZI should be found before the replacement of vw2 + 4V2 by w+2V.) In the case n =I 2 the calculations can be carried out in a similar way. The difference is only that the lines of the cut do not lie along the imaginary axis but make an angle n(1/2 - lin) with it. Then
Im{zd
A )2/n 22/n ( _ sin2~ + p2 . w 2n
=
(4.2.6)
As a result, for the transition probability we have
W = exp {_2[2 2/nPn sin2(nI2n) + l]I/2}
[~V-oo f V(p,x) dX] ,
x sin2
(4.2.7)
where dimensionless constant Pn and parameter X are
Pn
=
A2/nw2(n-I)/n 2
v
pw
,x = - v .
(4.2.8)
Formula (4.2.7) is obviously valid if the point ZI lies outside the circle of radius Ro:
(
2A)2In
~
sin 2: + p2 >
R~ .
(4.2.9)
4.2 Transitions Caused by a Multipole Interaction
95
Thus, for all impact parameters satisfying this condition, the transition probability W is limited by the relationship W < exp (_2(n+I)/nylp;. sin 2: ) .
(4.2.10)
For sufficiently large 2 and small w, when (22/w)l/nsin(n/2n) > Ro ,
(4.2.11)
formulas (4.2.7,9) are valid for any p. It is clear from these formulas that with decreasing velocity the transition probability decreases exponentially. When W = 0 (zero energy defect), formula (4.2.7) coincides with the formula (4.1.12) obtained above for this case. We shall now go on to calculate the preexponential factor in (4.2.7). Substituting in the integral with respect to x the potential V(p, x) = 2/(p2 +x2)n/2, we obtain -1 00 J V(p, x)dx = r:t.n _2 p-(n-I), v -00 v (4.2.12)
When
_( 2)
P
I/(n-I)
(4.2.13 )
r:t.n-
V
the argument of sin2[Ajv J V dx] in (4.2.7) becomes larger than unity, and sin2[Ajv J V dx] begins to oscillate rapidly about the mean value equal to 112. If
(4.2.14)
Po>Ro,
the replacement of the potential (4.2.3) by the potential 2/R n does not significantly affect the magnitude of the cross section, because this replacement only leads to a change of the character of the oscillations of sin2[Ajv J Vdx] in the region where the argument of the sin[2/v J Vdx] is large. Therefore, for velocities v satisfying the relation (4.2.14) it is possible in calculating (J to use the approximation W
= sin2
(
;n'pn/2) ::I
r:t.
n exp [ -2(22/n Pn sin2 2n +) X2 1/2]
.
(4.2.15)
It is interesting to compare this expression with the Born approximation for
W:
wB =
(
r:t.
pn/2
;n'::l
2 )
exp (-2X) .
(4.2.16)
96
4 Collisions Between Heavy Particles
When p" ~ 1, (4.2.15) in practice coincides with (4.2.16) for all P for which WB < 1/2, and for smaller p, oscillates about a mean value close to 112. Therefore when p" ~ 1, it is possible to restrict oneself to the Born approximation, supplementing it with some method of normalization, for example, assuming W - {WB 1/2
for for
p > Po p < Po
(4
.2.17
)
where WB(pO) = 1/2. When p,,~I, (4.2.15) differs considerably from (4.2.16) even in the region of p where WB is small. The maximum value of W is restricted by the condition (4.2.10). Therefore when p" ~ 1, it is impossible to use the Born approximation formula (4.2.16) even for rough estimates. By substituting of (4.2.15) in (4.1.1) the following expression can be obtained for the cross section: A)2/("-I) (1 = 2n ( exp ( _2(2n+I)/"J7j;, sin 2: ) In(P,,), (4.2.18)
v
In(P,,)
x exp { -2J7j;, [( 221n sin2 When
p"
~
When
2: +
Jo sin
2
(a,,/y(n-I»)
P!/("-I)l) 112 - 2 1/n sin 2:]} ydy. (4.2.19)
0,
h(P2) ~ ~ In(I/P2), In>3(Pn)
=
~T
h(P3) ~ n/2 ,
2(n-2) I (n-l)a 2/(n-l)r (:
=~)
sin
=
(~: ~)
(4.2.20)
p,,~I,
In(Pn)
~ ~ (2y'2ii;, sin;: + 1) P-" I (n-I) .
(4.2.21)
The values of In(P,,) for n = 2 and 3 are given in Table 4.1. At low velocities when Pn is large, the cross section decreases very rapidly (exponentially) with decreasing v. Such behavior of the cross section in the region of low velocities is typical for the inelastic collisions of heavy particles. An exception is the case of small values of ill, when values Pn ~ 1 are possible also at low velocities. We shall consider the dependence of (1 on ill at a fixed velocity. When ill = 0 (zero energy defect), Pn = 0 and (1
= 2n (
vA)2/
(4.2.22)
4.2 Transitions Caused by a Multipole Interaction
97
Table 4.1. Factors hand h; 8.8 (-3) denotes 8.8 xlO- 3
P
0.02
h 21.6
h
1.42
0.04
0.08 0.16 0.32 0.64 1.28
15.9
10.7
2.56
5.12
10.24
6.25 2.94 1.01 0.268 8.3(-2) 2.7(-2) 8.8(-3)
1.16 0.95 0.70 0.44 0.224 9.8(-2) 4.2(-2) 1.9(-2)
1.32
When w :5 (VA-1/nt/(n-I), the cross section remains close to (4.2.22), and when W > (VA- 1/ n )n/(n-l), it decreases exponentially with increasing w. At high velocities when Pn ~ 1, formula (4.2.18) gives n i= 2
(J
rv
(A/V i/(n-I),
(4.2.23)
n=2
(J
rv
(A/viln (const x v) .
(4.2.24)
This dependence\ is obviously valid only in the case when A is so large and w so small that Pn can be small at velocities satisfying the condition (4.2.14). At higher velocities when the condition (4.2.14) is violated, the approximation (4.2.15) based on the polar potential, which tends to infinity at p --+ 0, becomes illegitimate. It can be shown that the potentials V(R) = m
n - I /(R~
+ R2)n-I/2
(4.2.25)
,
or (4.2.26) which do not have a pole when R in the Born region
n>2 n=2
(J
(J
rv (A/vR~-2)2 rv
--+
0, lead to the following dependence on v
,
(A/v)2In(const VROI).
(4.2.27) (4.2.28)
It must be noted that at small A when (4.2.14) can be infringed even at small
v, the presence of the pole in the potential V(R) leads to a considerable shift of the cross section in the region of low velocities. Thus the range of applicability of formula (4.2.18) for the cross section is limited by the conditions (4.2.9, 14). The range in which (4.2.17) is valid is determined by the second of these conditions, and the first one does not depend on velocity and is satisfied all the better the larger A is and the smaller wis. The case of small values of w corresponds to collisions which are accompanied by a quasi-resonant transfer of excitation energy. Assume, as a result of the collision, the first atom passes from the level EI to the level E;, and the second atom from the level E2 to the level E~, where EI > E; and E2 < E~. In this case, (4.2.29)
98
4 Collisions Between Heavy Particles
In the case of collisions of identical atoms when El = E~, E; = E2, W = 0 (exact resonance). In collisions between different atoms, cases are possible when the resonance defect liw is small. 4.2.2
Two-Levels and Rotating-Axis Approximations
We shall now discuss the applicability of the two-level approximation. It is usually applicable for the transitions between two nondegenerate levels. When one of the levels is degenerate the problem must involve many levels. To reduce it to the two-level problems, some additional assumptions must be adopted. The simplest and most physically clear approximation consists in the use of the body fixed coordinate system, in which the quantization axis (the z axis) is directed towards the perturbing particle. In the course of a collision the direction of the quantization axis is changed. In such coordinates the direction of the electric field does not change and therefore the electric field does not mix the states with different magnetic quantum numbers m. Then for the multipole transitions of the type ns ---- n'l', we obtain the two-level system of equations describing the transition ns ---- n'l'm = O. Such a description is not complete. The rotation of the internuclear axis leads to the transitions nlm ---- n'l'm' with L1m -I- 0 in a system of coordinates fixed in space. In the rotating coordinate system these transitions can be treated by introducing the rotation operator (4.2.30) where cp is the angular velocity of rotation of the internuclear axis, and Lx is the operator of the x component of the orbital momentum where the x axis is perpendicular to the collision plane. It is not difficult to see that T", ex v. Therefore when v ---- 0, the rotation of the axis can be neglected, the problem being reduced to the two-level system with L1m = O. When the velocity increases, the expression (4.2.30) increases and hence the neglect of L1m -I- 0 transitions is no longer possible. For example, for excitation of the optically allowed transition by the charged particle, the rotating axis approximation gives in the Born region a result n2 /4 times lower than the exact asymptotic value. To estimate the cross sections for the transitions between two degenerate levels aJ - a' J', the simple two-level approximation is however often used. In this case one has to substitute in the equations the potential averaged over M, M': VaJ, a'JI
1
= (- L
IVaJM, al JIM/12
)
1/2
,
(4.2.31)
gMM '
where 9 is the statistical weight of the initial level. The matrix elements in (4.2.31) have to be written in the coordinate system fixed in space. The cross
4.2 Transitions Caused by a Multipole Interaction
99
section obtained in such a way has to be considered as the averaged one: II I (fa.!, a'JI = -I " L..J (f(aJM, a J M ) .
(4.2.32)
gMM'
t
Since the operator qJ (4.2.30) is proportional to v then at v - 0 the results obtained with the averaged potential (4.2.31) are close to the results of the solution of the strong coupling equations in the system of coordinates fixed in space. We noted above, see (4.4.22-28), that the presence of the pole in the potential leads in the Born region to the difference with the accurate values of the cross section. Therefore the parameter Ro has to be chosen so as to ensure the coincidence of the cross section with an accurate Born asymptotic value. The latter can be obtained in the framework of the usual perturbation theory. In several cases it is of interest to obtain formulas for the averaged multipole potentials. For the excitation of an optically allowed transition in collision with a structureless charged particle with charge Ze, V = A/R2 1 A
= Ze
(~)1/2
Ii,
(4.2.33)
3g
where S is the transition line strength [Ref. 4.14, Sect. 9.2.2] and g is the statistical weight. Consider the case of a collision in which one of the colliding atoms passes from the level J 1 to the level J{ and the second atom from the level J2 to the We assume that electric multipole transitions of order Kl and K2 are level allowed between the levels JI, J{ and h, J~. The interaction constant is defined by the relationship.
Jr
V=A/R", n=Kl+K2+1,
A=
.!. ( Ii,
glg2(2Kl
S,,)S"2 ) + 1 )(2K2 + 1)
1/2
(4.2.34)
,
where S,,) and S"2 are the line strengths of the electric multipole tranSItIons JI - J{, J2 - J~ and g), g2 are the statistical weights of the levels J), h The line strength is defined by the formula
~S" = Q,,(J, JI)(21' + 1) (~ ~ ~r
If
Pl(r)P11(r)r"drr e2 .
(4.2.35)
To conclude this section, we give an estimate of the cross sections for the transfer of excitation in the case of small energy defect using the interaction potential (4.2.34). The condition for applicability of small energy defect approximation can be written in the form 11: A1/"W("-I)/,, 11: 2y'2 2/"P" sin- = i"+I)/,, sin- ~ 1 . (4.2.36) 2n v 2n
100
4 Collisions Between Heavy Particles
In this case exp
(-i"+I)/"Jp: sin 2: ) ~
1, I,,(P,,)
~ 1,,(0),
and formulas (4.2.22, 34) give the following expression for the cross section: 2 )2/(,,-1) [
U
~ 2n ( !!....-
-4
e glg2(2/(1 + 1)(2/(2 K\
liv
4.2.3
S S
K2
] 1/(,,-1)
+ 1)
1,,(0) .
(4.2.37)
Treatment of the Coulomb Repulsion of Nuclei
The previous results have been obtained using the assumption of rectilinear trajectories of the perturbing particles. In the case of collisions between the two positive ions one has to take into consideration the Coulomb repulsion, i.e., to use the hyperbolic trajectories. For low collision velocities the cross section for excitation by a structureless particle with charge Zpe (/(2 = 0) can be evaluated using the semiclassical first-order perturbation theory described in detail by Alder et al. [4.15]. In this approximation the cross section can be written in the form l 3(2n - 1) A.~
U= - - - -
JE,,-I(O
4n v2 a2,,-4 ZiZp/Mv2 ,
(4.2.38)
'
= e= ZiZpw/Mv3 •
a
(4.2.39) (4.2.40)
Here Zi and Z p are the target and projectile ion charges, M is the reduced mass of a colliding pair. The functions JE;.(O are tabulated in [4.15] (A. = n - 1). At low velocities, i.e., for large values of JE;.( 0 <X exp (-2ne), and is exponentially small. In case of dipole transitions, n = 2, A. = 1, the asymptotic value is
e,
Ji.EI
~
32n3 -21t~
9y'3e
,
;:
.. ~ 1 .
(4.2.41
)
e
When > 1 the cross sections are very small. They become comparable in magnitude with the electronic cross sections only for e < 1. In plasmas usually v < Z;/MI/2. Therefore, the excitation by positive ions is substantial for small energy splittings w~Z;;ZpMI/2
.
e
When rI -+ 00 the Coulomb repulsion may be neglected, -+ O. Moreover, at very high energies the Born approximation is valid provided the correct interaction potential is used. In this limiting case the Born approximation and the first-order impact parameter method (used with the same potential) coincide \ We recall that in this section the atomic units with the energy unit me4 /h 2 = 2 Ry are used.
4.3 Charge Exchange
101
asymptotically. Hence, at C --; 00 the order of magnitude of the cross section can be evaluated using the simple analytic formulas obtained by the impactparameter method with rectilinear paths and with the model potential Vn ex Rn-I/(R~ + R2)n-I/2 (Sect. 5.1.4). For dipole transitions (n=2) (J
8nZ; 2 = -2-A.2
(4.2.42)
(J
4n Z2 A.2 = 27 v: R~
(4.2.43)
v and for quadrupole transitions (n=3),
Xo
= Rowlv.
The functions
4.3 Charge Exchange 4.3.1
Special Features of Charge Exchange Processes
Charge exchange in atomic collisions, i.e., the process A
+ B+ --; A + + B
(4.3.1 )
in which an electron goes over from the atom A to the ion B, is an example of a process with redistribution of particles. The electron wave functions of initial state 'P(rA) and final state
102
4 Collisions Between Heavy Particles
In the limiting case of high velocities, perturbation theory can be used. In the framework of perturbation theory, the velocity dependence of the charge exchange cross section is given by the Brinkman-Kramers formula [4.l9]. a(v) ex v- 12 ,
(v~vo).
(4.3.2)
4.3.2 Resonance Charge Exchange We shall consider the collision of the atom A in the state y with the ion of the same atom A+ (4.3.3 ) We shall assume that the state y is the state ns and that the ion A+ contains only completely filled electronic shells. At low relative velocities, the system A( ns) + A+ can be considered as molecular ion At. As R ~ 00, the ground term of the system is doubly degenerate because the electron can be located near either of the two ions A +. We shall denote the corresponding wave functions by 'l'1 and 'l'2. When R decreases, the ground term splits into two terms, an even term Ve 1:g ) = Vg , and an odd term Ve 1:u ) = VU. In the adiabatic approximation the wave functions of these terms are expressed in terms of wave functions 'l'1 and 'l'2 in the following way
(4.3.4 )
The wave function satisfying the initial condition 'l'(t form 1 'l'(t) = J2['l'g(t) + 'l'u(t)] . By substituting (4.3.4) into (4.3.5) we have in the limit
~
-00)
=
'l'1 has the
( 4.3.5) t ~
00
(4.3.6)
(4.3.7) The probability of the transition I W = sin2 '1 .
~
2 is (4.3.8)
The corresponding cross section can be obtained by integrating W over the impact
4.3 Charge Exchange
103
parameter, (J
= 2n Jpdp sin2'1(p) .
(4.3.9)
o
If '1 ~ 1, the function sin2'1 can be replaced by its mean value 112. Therefore it is enough to know the function at comparatively large p when '1 < 1. In the case of the molecular ion Hi, the exchange splitting at large distances has the form [4.8, 20]
1
2 [Vu(R) -
Vg(R)]
= 2R exp (-1
(4.3.10)
- R) .
Here atomic units are used. In the rectilinear-trajectory approximation, R
=
J p2 + v2t2,
'1
= 2~ vOx3/2exp(_I_x), x = plao.
(4.3.11)
(J
x 2 ....Q. = na02'
(4.3.12)
v Using (4.3.9) we have 2
where Xo is determined using the equation sin '1(xo) 0.28(C = 0.5772 is Euler's constant):
3/2 Xo exp(-xo)
~
'1(xo)
=
exp (-C)/2
=
0.15v (4.3.13 ) --. Vo A detailed discussion of the resonance and quasi-resonance charge exchange is given in [4.6, 20, 21]. The expression (4.3.12) for the charge exchange cross section is valid if v < Vo = e2 /;". In the limiting case vivo ~ 1, see [4.6,21],
(J
4.3.3
=
~
8 na~ -2 (VO)2 15 v
[1-4 (V)2 21518 (VO)12 + 1]-5 ---. na~. Vo v
(4.3.14)
Contribution of Inner Shells
If the atom A in (4.3.1) is a multielectron atom there exists a range of velocities v for which the condition v > vov'i for the valence electrons and the condition v < Vo v'i for the electrons of the inner shell are valid. Here, I is the ionization potential expressed in atomic units, i.e., in units of 2 Ry. In this range of velocities, inner electronic shells give the main contribution to the total charge exchange cross section. Now we shall consider the cross section of the charge exchange process ( 4.3.15)
104
4 Collisions Between Heavy Particles
in which an electron from the shell na/~ is captured by a proton, and as a result the hydrogen atom in the state with principal quantum number n is formed. If the relative velocity of the colliding particles is not too low, the cross section can be described by a simple generalization of the Brinkman-Kramers formula [4.22,23]
( IN _ ) _ 2 28 " N[2I(na l a)]5/2 (VO)2 n3 f(v) v' u na a n - 1tao 5
(4.3.16)
where (4.3.17)
The ionization potential I of the shell na I~ is expressed in atomic units. In the original Brinkman-Kramers formula the factor" is equal to unity. The accurate first-order perturbation theory [4.24] gives in the limit of high velocity, " ~ 1/3. In the estimates given below, we shall assume" = 1/3. At low velocities, the cross section decreases more rapidly than follows from (4.3.16); in fact exponential decrease occurs: 2 n (nLJI Vo ) . u(nalN -n)=nao-exp --a 8y2 2y V
(4.3.18)
This result can be obtained by the method described in Sect. 4.1.2. We shall denote the velocity for which the curves u(v) defined by (4.3.16) and (4.3.18) intersect by Vc. When V > vc , the cross section can be estimated by means of (4.3.16), and when v < Vc. one has to use (4.3.18). The cross section for capture from the inner shells is usually given by (4.3.16). In this case, I ~ LJI ~ 1/2n2, and the maximum value of the cross section of capture from the shell nal~ is achieved at the velocity Vm = voy'4I/3: 25N n
u(vrn) ~ na~-3-(2l)-7/2 .
(4.3.19)
When v > Vrn , the cross section decreases rapidly (ex: V- 12 ). In the range of velocities v:n < v < v~, where v:n corresponds to the outer shell and v~ corresponds to the inner shell nala, the dependence of the total cross section on energy tf (summed over all shells nala) has the form (4.3.20) The limiting value of p = 2.5 corresponds to the heaviest atoms. The charge-exchange cross sections for the Ne and Ar atoms are shown in Figs. 4.1,2. At energies tf ~ 100keV, the outer shell gives the main contribution. At higher energies, the capture of electrons from inner shells becomes significant.
4.3 Charge Exchange
105
In the case of alkali elements, inner shells give the main contribution to the cross section of charge exchange beginning from energies tff ;<: 20 keY [4.27]. Experimental data on the electron capture cross sections in collisions of protons with neutral targets were given in [4.28, 29]. 10- 15
cm l 10- 17
t 10-
19
b
10- /1 10-23 10
c-
Fig. 4.1. Effective cross section of the charge transfer H+ +Ne-+H+Ne+. Solid curves show the capture from different shells. Dotted line is the total theoretical cross section. Points correspond to experiment [4.25] .. Crosses correspond to experiment [4.26] I
I
H+ +Ar(1s / 2s 1 2p6 3s 1 3p 6) -
H+ Ar+
4 0
o~
6
~
8
b
Ly/
0
\,
/~,,~) \
/
2
\.
.-1/
4
K / /
6
'/
/
~~.~
~ \~
10
Fig. 4.2. Electron capture cross section in collision H+ + Ar: broken curves show the contribution from K - and L- shells, the solid curve shows the total capture cross section calculated in a modified Brinkman-Kramers approximation. Circles and crosses are various experimental data (for details see [4.23]).
106
4 Collisions Between Heavy Particles
4.3.4 Charge Exchange in the Case of Multicharged Ions
The Brinkman-Kramers formula can be easily generalized to the case of charge transfer from an arbitrary ion to a neutral atom [4.23): A + Bz+1
-->
A + + Bz , (4.3.21)
The function I( v) is given by (4.3.17) when AI = I - In, In = z2/2n 2. Here the levels n of an ion Bz, are assumed to be hydrogenlike. The cross section of quasi-resonance charge exchange to the level of an ion Bz with the principal quantum number
no = z../ii;.
(4.3.22)
has evidently the maximum magnitude. However, applicability of (4.3.21) for the resonance charge exchange is limited to the range of high velocities v ~ vm . The Coulomb field induces a strong perturbation of the terms in the final channel. Therefore, the exponential decrease of the cross section with decrease of velocity occurs at velocities considerably larger than Vc defined by (4.3 .16, 18). The Coulomb perturbation of terms is responsible for another mechanism of charge exchange in multicharged ions. If the ionization potential In of the ion Bz is larger than the ionization potential of the atom A, then electronic terms of the system A + + Bz ( n) intersect the ground term of the system A + Bz+ I at the points Xn determined by the condition z2
2n 2
-
h -
z - I
Xn
=0.
(4.3.23)
In the vicinity of the point of intersection of the terms, nonadiabatic LandauZener transitions can take place. At small velocities such transitions give the principal contribution to the transition probability. At higher velocities, transitions at other values of R also must be taken into consideration. The calculations [4.30, 31] show that the most effective transitions at high velocities are those in the states of ion Bz with principal quantum number no for which the quasi-resonance condition holds at high X [4.5,25]. When v decreases, capture to other levels with n < no becomes efficient. For n < no the cross section can have two maxima corresponding to the two above-mentioned mechanisms. The total cross section of electron transfer to all excited levels of an ion Bz has relatively weak dependence on velocity up to those velocities at which an ion Bz in the state no is mainly formed. The magnitude of the total cross section O"tot increases with z. Although the different models give somewhat different dependences on z, the order of magnitude of O"tot can be estimated by means of
4.3 Charge Exchange
107
formula
A more detailed discussion of charge exchange in the case of multiply charged ions is given in [4.5,32-35]. The available experimental data on electron capture by multicharged ions from simple H- and He- targets are given in [4.7,36,37]. An extensive bibliography on electron transfer processes was recently published by Tawara [4.38].
5 Some Problems of Excitation Kinetics
This chapter may be considered as an introduction to some problems of plasma spectroscopy. In the beginning we give a summary of the analytic formulas which can approximate the dependence of the rate coefficients (va) on temperature and atomic characteristics. These formulas contain two fitting parameters which should be determined from the results of numerical calculations. Tables of these parameters will be described in Chap. 6. Some useful semiempirical formulas are also given below. Special attention is paid to the process of dielectronic recombination and formation of the dielectronic satellites. These processes are very important for the spectroscopy of high-temperature laboratory and astrophysical plasmas. The last section of the chapter is devoted to the simplest approaches to the kinetics of level populations in a plasma.
5.1
Rate Coefficients for Elementary Processes in a Plasma. Approximation of Cross Sections and Rate Coefficients by Analytic Formulas
5.1.1 Excitation of Atoms and Ions In this section we summarize the formulas expressing cross sections a and rate coefficients (va) in terms of radial integrals and angular factors Q. It is convenient for applications to plasma kinetics problems to use the approximate analytic formulas. In this section, simple fitting formulas are proposed which describe the results of numerical calculations by means of two or three adjustable parameters and provide the correct asymptotic behavior of the quantities a and (va). Some semiempirical formulas, which are often used, are also presented. When constructing the approximate formulas we are mainly concerned with the energy region 8 ;S Ez (Ez is the ionization energy of the ion Xz ) which is of. the most importance for plasma diagonostics. In particular, the asymptotic behavior of the cross sections for optically allowed transition is taken in the form 8- 1, instead of the form 8- 1 In 8 (Sect. 3.1.3). Therefore one has to be cautious when applying the formulas given here to the problems of excitation and ionization in beam experiments. In these cases, the factor In 8 can be substantial. In this section the initial state is denoted by index 0, and the final state by index 1. The final results are given in cas units.
I. I. Sobel'man et al., Excitation of Atoms and Broadening of Spectral Lines © Springer-Verlag Berlin Heidelberg 1995
5.1 Rate Coefficients for Elementary Processes in a Plasma
109
We shall assume everywhere that the electron energy distribution function JF(8) is the Maxwellian, see (1.2.1). For excitation 0 -+ 1 by electron impact the rate coefficient (VO"OI) averaged over the electron distribution function is ex>
(VO"OI)
=
J vO"oIJF(G)dG ,
(5.1.1 )
tiE
where G is the energy of the incident electron, and AE is the threshold excitation energy. On substituting the Maxwellian distribution function (1.2.1) we obtain VO"
_Kex> ~exp(-G/T)8d8 na~ (Ry)I/2T3/2 '
L
( 01) -
(5.1.2)
217 x 10- 8cm3-1 - . K -- 2.Jili.ao s . m It is convenient to express the energy and temperature (Sect. 3.1.3). On setting u
= (8 -
In
P= DE/T.
AE)/DE,
the scaled units
(5.1.3)
Eq. (5.1.2) can be written as DE) 1/2 ex> ( ) (VO"OI) = K ( -R p3/2e - pp J 0" u2 (u y 0 nao
+ p)e -
pudu
(5.1.4)
with p = AE/DE. The rate of the inverse process (deexcitation) can be expressed through the excitation rate by (1.2.7). As was shown in Sects. 2.3 and 3.1,2 the cross section for the transition ao - al can be written, in the general case, in the form O"aOal
= E [Q~(ao,adO"~(lo, ld + Q~(ao,adO"~(lo, IdJ ,
(5.1.5)
I(
where the quantities O"~ and O"~ depend only on the quantum numbers nolo and nlll of the optical electron. The dependence on the total angular momenta of an atom (J,S,L, ... ) is described by the factors Q~ and Q~. For the cross section summed with respect to J,S,L, ... ) in the case of configurations no/~-nol~-Inl/h we have
O"(no/~,no/~-Inl/t>
= m E[O"~(lo, Id + O"~(lo, II)] .
(5.1.6)
I(
Thus the quantities O"~ and O"~ correspond to the single-electron transition cross sections. The quantity O"~ includes the direct and interference terms ,.1
VI(
=,.
VI(
+ ,.int
VI('
Q'(ao,al ) ex 0SoSI ~ .' I(
(5.1.7)
110
5. Some Problems of Excitation Kinetics
the quantity a~ representing purely the exchange term. The expressions of a~ and a~ in terms of radial integrals are given in Sect. 2.3. These quantities, evidently, can be obtained only by means of numerical calculations. The index K varies in the interval of Kmin to K max , where Kmin
= 1/0 -
Id,
Kmax
= 10
+ II
(5.1.8)
.
In accordance with (2.3.9, 10), a~ -=1= 0 only for K with the same parity as Kmin. We shall use the analytical fitting formulas to represent the results of the numerical calculations. In computer codes one can explore formulas with many adjusted parameters providing very accurate fitting to numerically calculated or measured cross sections. However, good accuracy is based on mutual compensations of essential contributions from nearby terms of opposite signs. Therefore, a small change of cross section results in a much larger change of parameters. In particular, the extrapolation of parameters along an isoelectronic sequence becomes very difficult if possible at all. We use comparatively simple formulas with true asymptotic and 2 or 3 adjusted parameters. The accuracy of these formulas is usually a few percents, but an interpolation and extrapolation of parameters for similar transitions, in particular in isoelectronic sequence, is very simple. Generally we use (5.1.5) and the fitting formulas for a~, a~. For cross sections, summed over J, the factors Q' and Q" differ only in the spin parts: Q~ = QK(Lo,LI)Ao, Ao
= b(So, SI ),
Q~
A2
= QK(Lo,Ld A 2 ,
=
(2S1 + l)j2(2Sp
(5.1.9)
+ 1).
In this case the fitting formula may be applied to the total one-electron cross section (5.1.10) This provides often the better accuracy of fitting since for a direct transition a~ is energy function smoother than a~, which may be negative at small and medium energies. It should be noted, however, that for transitions between fine-structure components the J o - JI orbital parts of Q' and Q" are different and the form of (5.1.10) is not valid. Taking into account properties described in Sects. 3.1-2 the one-electron excitation cross sections are written in the form 2 a~(lo, II) = ~
2/0
+I
(R) --L DE
2 (
EI ) Eo
3/2
. C(]I, (u) u + q> u=---
a"(1 1)= K
0, I
1ta~ 2/0
+1
(Ry)2 (EI)3/2. DE Eo
DE
(5.1.11)
C(]I"(u)
u + q>
where Eo,E I are atomic level energies (from the ionization limit). For a~ the function (]II = (]I' is used. C, q> are the fitting parameters, DE is a scaling factor.
5.1 Rate Coefficients for Elementary Processes in a Plasma
111
The functions
depend on the type of transition, and generally can include a third fitting parameter D. If one prefers to use a two-parameter formula D = 0 should be assumed. For the excitation cross sections, we have '(u)
= [1 -
D/(u + Ii] '11(U)
"(u)
= [u +
0.4 +Dr2 '11(U)
(5.1.12)
where '11(U)
= {(U+ p)I/2, Z= 1
(neutrals) ,z>l (ions)
1
p = ,1E/DE
(5.1.13)
The excitation rate coefficient can be written in a similar way:
"
,
(5.1.14)
10- (RY 10- 8 (RY 8
EI)3/2 AG'(f3) . - - e - f3p [cm 3 S-I] , f3 + X
(vu (10 Id) = - - _. 2/0 + 1 DE Eo '" _ (vu"(1 0 I») I - --2/0 + 1 '" f3
EI )3/2 AG"(f3) n [ 3 -I] (5.1.15) e - I'P cm s DE Eo f3 + X '
--. - .
= DE/T.
Here A and X are adjusted parameters, the functions G(f3) can include the third adjusted parameter
= f31/2(f3 + 1 + D)'11 (p-I) , G"(f3) = f31/2(f3 +D)'1I(P-I). G'(f3)
(5.1.16)
For the total one-electron rate coefficient (vu~) =Ao(vu~) +A2(VU~)
(5.1.17)
the function Gt = G' is used. Eqs. (5.1.11-16) can be employed in any of the scales DE given by (3.1.30a, b, c). But in the case of closely spaced levels only DE = lEo I or z2 Ry are appropriate. The functions and G are symmetric with respect to the initial and final states. Therefore, in the case of deexcitation collisions 1 ~ 0, we have
(vu(aJ, ao») =
(vu'(1 I») " I, 0
L [Q~(al' ao)(vu~(ll' 10») + Q~(al' ao)(vu~(lJ, 10»)]
" = ~ (RY . EI)3/2. AG'(f3) 2/1 + 1 DE Eo P+ X
_ (vu""(1 I, I») 0 -
10- 8
--2/0 1
+
(RY
[ 3 -I] cm s ,
EI) 3/2 A G"(P) [cm3 s -I] . DE Eo f3 + X
--. - .
, (5.1.18)
(5.1.19)
112
5. Some Problems of Excitation Kinetics
5.1.2 Ionization Cross sections and rate coefficient of ionization can be described in the way similar to that outlined in Sect. 5.1.1. In this book we do not consider exchange effects in the case of ionization. The ionization cross section summed with respect to the quantum numbers J),L),SI is usually of interest. In this case the angular factor Qj does not depend on K. For the transition (5.1.20) We have (5.1.21) Thus we can write fitting formula for the total one-electron ionization cross section summed over K and II : CTj(lO)=
1ta~ (Ry)2CtP(U) 210 + 1 DE U + cp
10- (RD~ ) 8
(VCTj(lo») = 210 + 1
3/2
.
8-Ez DE
(5.1.22)
U=--
A G(P)
P+ X e - Pp [cm3 S-I]
,
(5.1.23)
P=DE
T'
where Ez is the ionization energy of the level ao, the scale DE is Ez or zZRy. The functions
=
U
1
u+ +
D"I(U) ,
(5.1.24)
(5.1.25) It should be noted that in the case of neutral atoms (z = 1), the formulas for
(
2 11,2)3/2 1t T exp (P p )(VCTj) .
m
(5.1.26)
5.1 Rate Coefficients for Elementary Processes in a Plasma 5.1.3
113
Recombination
In high-density plasmas the principal recombination process is three-body recombination. The number of these recombination events per second is Nz+IN;ICr, and the rate coefficient of recombination is related to the ionization rate coefficient by (5.1.26). In plasmas with moderate and low densities, two-body recombination prevails. The two-body processes are the radiative recombination and dielectronic recombination, see (1.1.4,5). The number of two-body recombination events per second is Nz+INe", where" = "v + "d. In two-body recombination a photon is involved, and therefore it is a weaker process than three-body recombination. When the density is not high, the probability of triple collisions is substantially smaller than the probability of binary collisions. This compensates the weakness of the interaction. Dielectronic recombination will be considered in detail in Sect. 5.2. For the rate coefficient of dielectronic recombination
Xz+I(CXo) + e
--t
Xz(cxlnl)
--t
Xz(cxonl)
+ liw,
(5.1.27)
the fitting formula has the form (Sect. 5.2.5)
"d = 10-13 QdAdP3/ 2 exp (-PXd) [cm3
P=
S-I],
(5.1.28)
(z + liRy/T ,
where Ad and Xd are the adjusted parameters. The parameters Ad, Xd for several types of transitions txo - cx\, are given in Sect. 6.1.7. The factor Qd depends on the type of the transition txo - CXI. For transitions CXo = 1'0 --t CXI = 1'0-111,
Qd = m/(2/0 + I), m Ik and for transitions 1o I
(5.1.29a) --t
/m-I/k+ 0 I I,
(5.1.29b) In most cases, recombination occurs onto the highly excited levels nl. We shall consider now the radiative recombination process,
Xz+I(aj)
+ e --t Xz(a) + liw
(5.1.30)
[Ref. 1.1, Sect. 9.5]. Taking into account the known properties of the radiative recombination cross section [1.1], we adopt the following fitting formula for the rate coefficient of recombination to the level a:
P=
Ea/T
(5.1.31)
where A,X and D are the adjusted parameters [5.1.], and Ea is the ionization energy of the level a, which corresponds to the term LjSj of an ion Xz+I. (We
114
5. Some Problems of Excitation Kinetics
note that the numerical factor adopted here is different from the factor used in [Ref. 5.1, Sect. 9.7.4]. The factor Qv depends on the angular momenta of the level a. When a = ajnlLS, aj = no/~-ILjSj,
(2S + 1)(2L + I) Qv = 2(21 + 1) (2Sj + I) (2Lj
(5.1.32)
+ 1)
For the cross section summed with respect to L, S,
= Qv(no/~-Inl) = and aj = no/~-ILjSj,
Qv(no/;;'"""" I [LjSj]nl) When a
= no/~LS
(2S + 1)(2L + 1) Qv = 2(21 + 1)(2Sj + 1)(2Lj
+ l)m
I .
(LS G LiSi
(5.1.33)
)2
(5.1.34)
For the cross section summed with respect to LjSj and LS m-I
Qv(no/~) = I - 2( 2/0 + I)
(5.1.35)
For the total rate coefficient of radiative recombination Xz+1 a formula similar to that of (5.1.31):
"v = ~ "v(a) = 10- 13 (:~) 1/2
A/Jlli:: D)
[cm3
-+ Xz
one can adopt
S-I] ,
(5.1.36) where Ez is the ionization potential of an ion Xz • The factor Qv should be taken into account in the summation with respect to a. It can be shown (see below) that radiative recombinations occurs mainly to those levels a for which lEal> T. Here and anywhere in this book the energy of a level Ea < 0 is measured from the ionization limit. For these levels "v(a) decreases slowly with increasing n, being proportional to n- I . The higher levels with lEa I < T produce only small contributions to "v, since for these levels "v(a) ex n- 3 • In the case of high temperature T> IEzl, radiative recombination to the states with minimal value of n provides the major contribution to the total recombination rate. We shall now give for reference the formulas which allow the calculation of the cross section and the rate coefficient of radiative recombination (for details see [5.1]). The rate coefficient of radiative recombination is given by expression
"v(a)
E 11/2 00 () p3 /2 J an ~ u exp (-pu) du, y 0 7tao
= K I Ra
u
= &/IEal ,
(5.1.37)
5.1 Rate Coefficients for Elementary Processes in a Plasma where
P= IEal/T, _
Urv -
li,w
and
2
2
1ta03 (137)3
= lEal + $,
Urv
Qv(a)
1m
115
is the cross section of recombination to the level a:
(lEal +$)3 $
E
2
ImP (kA.,nl),
).=1±1
(5.1.38)
= max (/, A.) .
The radial integral p(kA., nl) is equal to 00
p(kA.,nl) =
J Pnl(r)Pk).(r)rdr,
(5.1.39)
°
where Pnl and Pk). are the radial wave functions of the optical electron in the discrete and continuous spectra of an atom X z ' The function Pnl is normalized, as usually, to unity, and the function Pk). is normalized in accordance with (3.2.2):
. ( kr - -A.n - 1 sm Vk 2
~
Pk).
r-+oo
z + -lnkr + '1 )
k
.
(5.1.40)
(5.1.3~0) atomic units with the Ry unit for the energy are used. Recombination to highly excited levels n ~ 1 is well described by the quasiclassical formula [5.2]
In
2 16n:z2 LlnRy ~ urv(nl) = nao3(137)3 . ----;;&V 1 + 117 e (LIn, Ill) ,
e(Lln, Ill)
d
= ( dx JAn (X)
LI - Ii,wn 2 n - 2z2Ry'
_
III -
)2
-
(Llnf _x2 2 X2 [JAn(X)] , X = IlILln,
(5.1.42)
/1 _ (/ + 1/2)2
V
(5.1.41)
n2
On summing (5.1.41) with respect to I we get the known Kramers formula for the radiative recombination to the hydrogenic levels: uKr'(n) = na~ rv
16z2 Ry 3V3(137)3 LIn $ .
(5.1.43)
On substituting (5.1.43) into (5.1.37) and using (5.1.2) we find "v(n) Pn
=
64y'n aoli,
3/2
.
V3 Z Pn [-exp (Pn) El (-Pn)] , 33m 1373
= z2Ry/n2T
(5.1.44) ,
where Ei(-P) is the exponential integral. With the use of (5.1.44) it is not difficult to show that (5.1.45)
116
5. Some Problems of Excitation Kinetics
Using (5.1.44) for the levels with n ~ nl and the more accurate method for n < nl, one can write the radiative recombination rate coefficient summed over all levels in the form lev
E
=
lev(a) + ~'(n ~ nl) ,
(5.1.46)
a(n
Kr.(
lev
X
5.1.4
~ nl
n
)
=
32J1t aoh r::; z 3v3 • m • 137 3
nl
[In 1.78PI - exp (Pd Ei( -Pd
pI/2 I
(I + !: )l
PI = z 2Ry/niT .
(5.1.47)
Semiempirical Formulas for the Rates of Excitation, Ionization and Dielectronic Recombination
a) Excitation
In the range of high energies of the electron, the excitation cross section for optically allowed transition (L11 = ± I, L1S = 0) is expressed in terms of the oscillator strength by the formula (3.1.24). There are a number of semiempirical formulas for estimating cross sections which are based on the Bethe formula. Here we shall give the Van Regemorter formula [5.3] which is currently the most frequently used: 2
O'aOa(
= nao
8n y'3faoa(
(Ry)2 L1E u+
y(u) 1 '
(5.1.48)
where f aoa( is the oscillator strength for the transition ao -+ a I. The factor y( u) is determined from the experimental data and the results of numerical calculations of excitation cross sections. Its values for neutral atoms and ions are given in Table 5.1. When u -+ 00 , y(u)~
y'3
2nIn(l+u),
and (5.1.48) becomes the Bethe formula.
Table 5.1. Factor y( u) for atoms (z = 1) and ions (z > 1) y, y,
y'u z=1 z > 1
0.0 0.000 0.200
0.2 0.Q15 0.200
0.4 0.034 0.200
0.6 0.057 0.200
0.8 0.084 0.200
y, y,
y'u z=1 z > 1
2.0 0.328 0.328
3.0 0.561 0.561
4.0 0.775 0.775
5.0 0.922 0.922
6.0 1.040 1.040
1.0 0.124 0.200
5.1 Rate Coefficients for Elementary Processes in a Plasma
117
On using (5.1.48) for the cross section the excitation rate coefficient can be written in the fonn
(VO"aoa,) = 10- 8 x 32jaoa,
When
(~~r/2 pl/2exp(-p). p(PHcm3 s-I].(5.1.49)
P~l,
p(P)
~ - ~ Ei(-P)·
The values of the factor p(P) are given in Table 5.2. In various applications also the fonnu1as by Drawin [5.4], Mewe [5.5], and Gryzinsky [5.6, 7] are often used. In fact, all these fonnulas practically do not differ. The analytic fonnulas for the excitation cross sections can be obtained in the Born approximation using the model interaction potential VK(R) ()( RK / (R~+R2)K+l/2 [5.8]. For transitions between the levels with small energy spacing (with the same principal quantum number) such a potential is often fairly close to the real potential. In case of optically allowed transitions (AI = 1, K = 1) (5.1.50) where Zp is the projectile charge, M is the reduced mass of the colliding pair, iaoa, is the oscillator strength for transition ao -+ al (5.1.51) Kn(x) are the modified Bessel functions, Xmin = max
Ro ao
fM( V"RY Is
Y-;;
=f
~) VRY
,
(5.1.52)
(5.1.53)
Table 5.2. Factor p(fJ) for atoms (z fJ
z=1
p, p,
z > 1
p, p,
z=1 z > 1
= 1)
and ions (z > 1)
O.oI 1.160 1.160
0.02 0.956 0.977
0.04 0.758 0.788
0.1 0.493 0.554
0.2 0.331 0.403
0.100 0.214
2 0.063 0.201
4 0.040 0.200
10 0.023 0.200
>10 0.066p-'/2 0.200
fJ
0.4 0.209 0.290
118
5. Some Problems of Excitation Kinetics
In the case of quadrupole transitions 4
Uaoal = 135
(I(;
= 2)
22M Ry , -;cQ2(ao,a l )
7ta oZ p -;;;
x (21
I) (10 2/1)2 (l0Ir21/1)2 1+ 000 R~a~ x [4>2(Xmin) -4>2(Xmax )] ,
(5.1.54) (5.1.55)
00
(l0Ir21/1)
= J Pno/o(r)Pnl/l(r)r2 dr
(5.1.56)
o
iff~AE
When both Xmin
~~
Ro 2 ao
and Xmax > I, 4>1(Xmax ) and 4>2(Xmax ) can be neglected, and
(M) m
1/2 AE Ry
(RY) 1/2 iff
(5.1.57)
This approximation corresponds to the first-order impact parameter approximation with rectilinear trajectories. In this case the functions 4>1 (Xmin) and 4>2 (Xmax ) can be approximated by 4>1(X)
~
exp (-2x) . In (2.25 + 0.681/x) ,
4>2(X) ~ exp (-2x) . (2 + xJ3n/2)2 .
(5.1.58) (5.1.59)
The rate coefficients, averaged over the Maxwellian distribution, can be written in the form 16n l / 2 e 2 2 Q~(aoad (VU,,) = 21(; + 1 h ao [(21(; - 1)!!]2 x(21 I
+
I) (/ 0 I(; 11)2 (/olr"I/I)2 000 R2,,-2a2
o 0 xexp (-AE/T) . (Ry/T)1/2I,,(AE/T, Yo) ,
(5.1.60)
00
I,,(x, y) = exp (x/2)
J dt t2"-IKr(t) exp
(5.1.61)
o
Yo
= Ro (AE) 1/2 aO
RY
For the dipole transitions (AI
=
I) (vu) can be written in the following form
< vu >= 1.7410- 7 faoal (Ry/AE)(Ry/T)I/2 (5.1.62)
5.1 Rate Coefficients for Elementary Processes in a Plasma
119
When the argument of Ko does not exceed 3.0 the integral II (x, y) is approximated by the following asymptotic formula (5.1.63) For transitions with small energy spacing in plasmas usually rff ~ AE. Therefore, the Coulomb attraction of the electrons is not important. However, in cases of neutral atoms and ions with low z the effect of normalization can be very substantial. In such cases the formulas given above can be used only for rff~Eo, EI, i.e., when the Born approximation is valid. For multiply-charged ions (z > 3) and rff > AE they give fairly reasonable values of cross sections for the dipole transitions, and allow to estimate the order of magnitude of the cross section for quadrupole transitions. b) Ionization The well-known classical Thomson formula for the cross section of ionization from the shell nolo corresponds to (5.1.22 and 24) when C = 4m(2/0 + 1), ({J = I, DE = Ez and D = 0: aj
2
(Ry)2
= 1tao • 4m Ez
(u
+u 1)2
(5.1.64)
.
To estimate the rate coefficient of ionization for atoms and ions from the ground state, the Seaton formula [5.9] is often used:
(vai)
=
R )3/2 ( 10- 8 x 4.3m; p-1/2exp(-{3) [cm3 S-I], (5.1.65)
{3
= Ez/T, {3
~ 1,
where E z is the ionization potential of an ion X z • This formula corresponds to (5.1.23,24) when z > 1, X = 0 and A = 4.3· (2/0 + 1). Expression (5.1.65) is valid only for {3 2: 1. Sufficiently universal semiempirical formula was suggested by Lotz [5.10]:
(vai) = 10- 8 • 6m
1~~13/2 {3-1/2exp(-{3)f({3)
[cm3 s-I], (5.1.66)
f({3)
=
-{3exp({3)Ei(-{3).
This formula corresponds approximately to (5.1.23,24) when z > I,X = 0.4, and A = 6(210 + 1). The values of the factor f({3) are given in Table 5.3. Table 5.3. Factor f(fJ) fJ f(fJ)
= 1/4 = 0.34
1
4
8
0.59
0.83
0.90
120
5. Some Problems of Excitation Kinetics
The compact semiempirical fonnula which is also often used is given in [5.4]. Classical fonnulas for the ionization cross sections are given in [5.7, II]. c) Dielectronic Recombination A detailed treatment of dielectronic recombination is given in Sect. 5.2. To exhaust the list of analytic fonnulas for bound-bound and free-bound electronic collisional processes we present here a semiempirical fonnula for the rate coefficient of dielectronic recombination proposed by Burgess [5.12]. This fonnula can be written in a fonn similar to (5.1.28) "d(a)
= 1O- 13 BdP3/ 2exp(-PXd)
[cm 3 S-I],
P= (z + 1)2Ry/T ,
(5.1.67)
with Bd = 480jcxocx
Xd
5.2
(
z2
:~3.4 )
1/2
[I
+ O.105(z + l)X + O.015(z + 1ilrl ,
3 )-1 ,
(
= X I + O.Ol\z ~ 1)2
X = (z + 1)2Ry .
(5.1.68)
Dielectronic Recombination
In this section and the following one we discuss some problems related to dielectronic recombination I and fonnation of dielectronic satellites. We have used cgs units here. We recall also that for ions which are members of the isoelectronic sequence of an atom A the designation [A] is used. For example, the designation [H] is used for a set He+, Li 2 + and so on. 5.2.1
Electron Capture and Under threshold Resonances (Simplified Model)
As noted above, the excitation cross section for positive ions has a nonzero value at threshold due to the long-range Coulomb attraction. This attraction also allows the excitation of an ion Xz+ I at an energy below threshold, the electron being captured on some level nl ofthe ion Xz • For example, at an energy lower than the excitation threshold for the resonance level of the He-like ion 06+, the following process is possible: 06+(li) + e
--t
05+(1s2p nl) .
The doubly excited state which is the result of electron capture is unstable, and may decay either through autoionization or spontaneous emission of the resonance 1 Dielectronic recomb~tion is widely discussed in the literature, see e.g. the review articles [5.13-15]. In [5.15] one can find an excellent historical review and numerous references to original articles.
5.2 Dielectronic Recombination
121
photon 2p - Is. In the latter case, the atom X z is transferred to the stationary state, i.e., recombination occurs. This process is called dielectronic recombination (abbreviated to DR below). Generally, the process of dielectronic recombination of an ion Xz+! via the intermediate doubly excited state of an ion Xz is written in the form (5.2.1)
y = anlLSJ,
y' = a'niL'S'J' .
Below, the LS-coupling scheme is adopted. Besides it is assumed that photon emission occurs due to transition of the "inner" electron a - a', and the state nl of the "outer" electron does not change. Radiative transitions of the "outer" electron cause the complementary satellites (Sect. 5.3), but they do not play an essential role in the total balance of dielectronic recombination. The three most important effects of a DR process are: A. Dielectronic recombination for all ions other than bare nuclei is an additional recombination process. In many actual cases, as shown by Burgess and Seaton [5.16] the rate of DR can considerably exceed the rate of radiative recombination. Therefore, in low density plasmas dielectronic recombination should be necessarily taken into account. B. Satellites to the resonance and other lines of an ion Xz+1 originating from radiative transitions in reaction (5.2.1). C. Complementary excitation of levels a' when the autoionization occurs in reaction (5.2.1) with a' =I- ao. The latter has been considered in detail in Sect. 3.4, the satellites will be discussed in Sect. 5.3. Here we shall consider the intrinsic dielectronic recombination. For simplicity we discuss here only the process (5.2.1) neglecting the secondary ionization of the excited ion Xiy'). Both collisional and radiative secondary ionization in a plasma are considered in [5.17]. In some cases the secondary autoionization of ion Xz(y') is also possible. (For a discussion of the secondary processes see also [5.15].) In Sect. 5.2.1 we confine ourselves to the description of the simplified model making the following assumptions: a) the state of ion Xz is described by quantum numbers ani without specifying the terms LS; b) the value of n is large enough, so that the influence of electron nl on the state a of the core can be neglected; the levels nl can be considered as hydrogenic, and capture cross section can be expressed in terms of excitation cross section for transition ao - a using the correspondence principle; and c) in the process of photon emission, the electron returns to the initial state r:t.o. In this case the formulas for calculation of dielectronic recombination cross
5. Some Problems of Excitation Kinetics
122
sections prove to be sufficiently simple. Discussion of these assumptions will be given in Sect. 5.2.3. The general case will be discussed in Sect. 5.2.2. Within the frame of our simplified model, DR process is written in the form /' X;(aonl)
XZ+I (lXo) + e ---- X;*(a nl) '\.
+ hw (5.2.2)
Xz+1(IXO) + e , the lower branch of the reaction (autoionization) being the competing process. Therefore the cross section for dielectronic recombination via the state IXnl is A(a, IXQ) (I) , Wa IXn
I
ad(anl)
= ad(lXQ, anI) A ( IX) +
(5.2.3 )
where A( a, IXQ) is the probability of a radiative transition IX - lXo in an ion Xz+ I, Wa is the autoionization probability for the level anI of an atom X z , A(IX) = LiXJ A(IX, IXd is the total probability of radiative decay of the levela,a~(IXQ,anl) is the cross section for electron capture to the level nl when the transition IXQ - IX is excited. This cross section is represented by a set of resonances at the energies .to (0
~ LIAE _ z2 R2Y < LIAE,
AE
n
= Ea.a.o = Ea. - Ea.o .
(5.2.4)
It is convenient in this section to use again eGS units. The resonance width equals F = hWa • The cross section averaged over the resonances can be obtained
with the aid of the correspondence principle by extrapolating below the threshold the partial cross section for the excitation ao - IX: 2z2Ry n
a~(IXQ, IXnl)F = a(lXQ, 1X1)--3- .
(5.2.5)
Here a(lXQ, IX/) = EAo a(IXQAo, 1X1), where a(IXQAo, 1X1) is the partial cross section for the transition IXQ - IX in the threshold C = AE; Ao, 1 are the orbital momenta of the outer electron. In accordance with condition (b) of the model we should sum the cross section over total angular momenta LTST. The corresponding formulas are given in Sects. 2.3 and 3.2, in which the sum over A. is to be replaced by one definite value of A. = I. The values of Wa and a~(or a) are related to each other as characteristics of direct and reverse processes. To derive this relation it should be noted that at A = 0, the ratio of the populations of Xz+I(IXQ) and Xz(lXnl) is given by the Saha formula. Using this formula, we obtain (21
+ 1)ga. W,(a IXn 1)
= z2C .I:.
1tnn
goa(lXo,1X1)
3
2
1tao
'
(5.2.6)
where ga. and go are the statistical weights of the states a and ao. The rate coefficient of dielectronic recombination is Kd
= E Kd(a), a.
Kd
(a)
= E vad(aO, IX nl)F:#,( C) , ~
(5.2.7)
5.2 Dielectronic Recombination
123
where r is the resonance width, and ff(C) is the Maxwellian distribution for the energies of the electrons. The value of C is given by (5.2.4). Substituting (5.2.3) and (5.2.5) in (5.2.7) we obtain (5.2.8) where ns and
nl
are determined by the relations
( ns)3 n
= Wa(rxnl, rxo) .
(5.2.9)
A(rx, rxo)
One can see that nl is in fact the minimum value of n, i.e., it determines the lowest level at which the capture of an electron is possible in accordance with (5.2.4 ). We now transfer (5.2.8) into a form more convenient for applications. We substitute in (5.2.8) the explicit expression for ff(C) and use the relation (5.2.6), and the relation between A and the oscillator strength /:
g!J.A(rx, rxo)
=
1 (RY) T (.1E)2 Ry go/!J.o!J. .
(5.2.10)
1373
We write the result in the form
Kd(rx)
=
(z
+ 1)2Ry
=
{3
1O-13Bd(rx){33/2exp(-{3x) ,X =
T
[cm3 s-I], (5.2.11)
.1E (z + 1)2Ry ,
where {33/2exp (-{3X) provides the main temperature dependence of Kd, and Bd(rx) only slightly depends on temperature and is equal to
, z 21 + 1 Bd(rx)=C ·4·/"0!J. I: exp(J{3)I: 1+( / )3 nl n>nl l
= ns(l) = 137 ( 2 ~i(1( rxo, rxl) n ao(21
C'
=
+ 1)/!J.0!J.
1013 x 4n 3/2aoli (_z_)3 1373 m z+1
) 1/3,
= 0.53
J{3
=
I: Bn exp(J{3) , n>nl
Zn2~TY ,
(_Z_)3 [cm3 z+1
(5.2.12)
S-I] .
The value of ns separates all the levels into two parts. For n > ns(l), Wa < A and after the capture of an electron the ion Xz transfers to a stable state, i.e., recombination occurs. The contribution of these levels to Kd is ,
Kd(rx) ~
LIE
f
I: V(1( rxo,rxl)ff(C)dC, Es =
LlE-IEsl I
z2Ry --2 .
(5.2.13)
ns
For n < ns(l), Wa > A and most of captures are followed by autoionization; only a small part rv (n/ns)3 provides the DR. Nevertheless these levels (n < ns)
124
5. Some Problems of Excitation Kinetics
contribute mainly to the total rate "d. If we temporarily omit the factor exp (c5P) in (5.2.12), then all levels with n < ns(l) will almost equally contribute to "d. If, as usually is the case, ns ~ 1 the ratio of contributions of the levels with n < ns and n > ns is
"
,-
led '" led
2ns -
ns
n)
,....,
-
2
.
If now we take into account the factor exp(c5p), this ratio will be even larger since c5p '" n- 2 • The levels n < ns( I) of the ion Xz are evidently in thermodynamical equilibrium with the ion Xz+) and hence the rate of DR is proportional to the probability of radiative transition, A( IX, ao) oc tJE2 j fY.{ja. oc ni 4 j fY.{ja., in accordance with (5.2.12). As seen above DR proceeds mainly in the levels n) - ns , and since in most cases ns ~ 1 the condition (b) of our model (n ~ 1) is justified. The exception is the case of the Is - 2p transition at z ~ 20 when ns < n) and n > ns for all possible values of n. We consider now as an illustrative example the recombination of a [Li] ion with excitation of 2s - 2 p transition and recombination of [H] ion with excitation of Is - 2 p transition. In the first case, the energy level distance tJE is small, so that X = tJE/(z + I)Ry '" l/z~l, and u(ao, IXI) is large. That means the factor exp( -PX) ~ 1 in (5.2.11), ns ~n) ~ 1, and a great number oflevels concentrated in very narrow energy band ('" tJE) contribute to "d. Because of the small value of A '" X2 j, the value of led is comparatively small in spite of a great number of levels. In the case of recombination of [H] ion or [He] ion X ~ 3/4, and due to the factor exp (-PX), the rate of DR at small temperatures is negligible. The value of ns isn't large and for z ~ 20, ns is even smaller than n) ~ 2. For this reason, a comparatively small number of levels contribute to Bd in (5.2.12), but the contribution of each one is great because of the high value of A. According to numerical calculations the total values of Bd for the Is - 2 P transition usually exceed those for the 2s - 2 p transition. The value of led, however, is greatly dependent on temperature in the case of the Is - 2 p transition.
5.2.2
General Case
The formulas (5.2.11, 12) obtained above provide a useful method of calculation of the DR rate coefficient within the simplified model. In this section we derive a general expression for the DR rate coefficient without the assumptions of the simplified model. We shall consider the process (5.2.1) again using the detailed balance principle (Sect. 1.2) to derive the general formula for recombination rate coefficient. The total DR rate is (5.2.14)
5.2 Dielectronic Recombination
125
where R(y) is the probability of electron capture into the state y of Xz; and A(y) = E y' A(y, y') and Wa(Y) = E y ' Wa(y, y') are the probabilities of radiative and autoionization decays. Since the latter decay is associated with internal electrostatic interaction, it cannot change the total momenta LSJ. If we suppose that A = 0, and hence the system is in thermodynamical equilibrium, then according to detailed balance principle, we can write
NeNz+lR(y) = Nz(y)Wa(y,tXo) ,
Wa(y,tXo) =
E Wa(y, Yo) , ~
where the ratio Nz+dNz is determined by Saba equation (Sect. 1.2). The value of R, of course, is independent of any assumption concerning the radiative decay associated with an electromagnetic interaction. Therefore we can use the last equation to determine the value of R in the general case, and substituting it in (5.2.14), we obtain
I 8n3/ 2 a3 Kd(Y) = 2go . (z + 1~ p3/2exp (-PX
+ bP)
x gyA(y) Wa(y, tXo) ; bP = AE - EylXo , T A(y) + Wa(Y)
(5.2.15)
the values of P and X being determined by (5.2.11); go and gy are the statistical weights of the states tXo(Xz+1) and y(Xz ), and AE = EalXo and EylXO are the excitation energies of the states IX and y. The difference of these energies bE is equal to the bound energy of the captured electron, (5.2.16) The radiative decay probability A(y) summed over all final states y' does not depend on LSJ and is denoted below by A(IX). The values of P and bP are in fact also independent of LSJ. The autoionization probability in the LS coupling scheme does not depend on J, but essentially depends on LS. Therefore we shall write the rate coefficient of DR in the form (5.2.11), the factor Bd being equal to Bd(lX) = C
E exp(bP)q(y),
y = IXnILS,
niLS
C = 1013
4 3/2 3 n ao 3[c m 3 -1] s. go (z+ 1)
(5.2.17)
Due to the nonlinear dependence of Bd on Wa(y) we cannot explicitly sum over LS in (5.2.17). For this reason, the use of this equation requires a great deal of computation. In most applications an approximate formula is used, in which an averaged value of Wa(y),
Wa(lXnl) =
it
(2L + 1)(2S + 1) 2(21 + 1)( 2L a + 1)(2Sa + 1) Wa(Y) ,
(5.2.18)
126
5. Some Problems of Excitation Kinetics
is substituted in the denominator of (5.2.17). After this substitution we can write (5.2.17) in the form Bd(a.) = CEexp(bP)q(rxn/) , nl
(5.2.19)
(a.nl) = 2(21 + l)gIXA(a.) Wa(a.nl,lXo) . A(a.) + Wa(a.n/) q
Calculations with these formulas are much simpler than (5.2.17). Summing of linear expressions of the type (5.2.18) can be accomplished analytically, and only the sum over nl has to be done numerically. Besides, the expression for Wa(rxn/) is much simpler than that for Wa(Y) (Sect. 5.2.3). Approximation (5.2.19) corresponds to the assumption (a) of the simplified model. If n ~ 1 [assumption (b)], we can use the relation (5.2.6) and substitute the threshold excitation cross section in place of Wa in (5.2.19). Thus we obtain Bd(a.)
, z
(21+1)B'
= C . 4" . I IXfJIX E exp (bP) E B B'( I nl
n>nl
l
+
n ns
)3'
(5.2.20)
where B' =
E g1X1I1X/1X 1X' go/lXfJlX
B=
(EIXIX/)2 , EIXIXfJ
Wa(a.n/) Wa(rxnl,lXo) ,
(5.2.21 )
C',nJ,ns , being defined by (5.2.9 and 12).
The simplified model (5.2.11,12) is readily obtained from (5.2.20,21) if we assume that B = B' = 1. This corresponds to the assumption (c) with the single final state IXo for all decays. 5.2.3 Formulas for Autoionization Probability In this subsection we shall give the formulas for Wa without using the approximation (5.2.6). First of all we consider the probability Wa(Y) for decay of the state Y = rxnILS.!. The equation for probability of autoionization was derived in Sect. 3.4 on the base of the general theory of the excitation of highly charged atoms. We can obtain the same result more directly as the transition probability Y - Yo in firstorder perturbation theory. The latter way is similar to deriving the formula for the partial Y - Yo excitation cross section of the ion Xz+l. In this case, however, we deal with transitions at given values of LS.! which correspond to total angular momenta LTSTJT in the problem of excitation of the ion Xz+l. Therefore, we cannot use the simple formulas from Sect. 2.3.2 where the cross section was summed over LTSTh. In the case of LS coupling, Wa(Y) does not depend on J,
5.2 Dielectronic Recombination
127
but depends on LS. Using (2.3.27,28) we obtain
2Ry Wa(Y,IXo) = ~
E 1EA"(bsIX()SaR,,d Ao
n
"
" e R"",,) 12 , BSaosa. 'L.J ,,"
(5.2.22)
(5.2.23)
In the radial integrals Rd and Re , the functions F;.(r) for the electron in continuum are replaced by the functions PI(r) for a discrete spectrum, PI being normalized to unity similarily to Plo and Pia. The functions PI and FAo in the exchange integral ~ are orthogonalized functions related to PI and Flo according to (3.2.5). For the averaged quantity Wa(IXnl), we can use simpler formulas, similar to those given in Sect. 2.3.2 for the cross section summed over LTST. Thus we obtain [cf. (2.3.8,9)] Wa(IXnl,IXo) =
2Ry", T ~[Q,,(IX, IXo) Wi1a. nl, 10) I
I
+Q~(IX,IXo) W~/(la.nl, 10)],
W~(la.nl, 10) =
W~/(la. nl, 10) =
( 21 a.
( 2/ a.
+ 1;(21 + 1) ~R~(~ -
(5.2.24)
~R~",,),
+ 1; (21 + 1) ~(~R~""i .
(5.2.25)
Formulas for Q factors are given in Sect. 2.3.2, but the direction of transition has to be reversed to IX - t IXo instead of IXo - t IX. In the limit n~ 1, the expression (5.2.24) is proportional to the partial excitation cross section for the transition 1Xo-<X in the ion Xz+I. To derive an explicit relation we should use the following relation of the discrete and continuous spectra functions: Pnl(r)
-t n--+oo
(
2z2) 1/2 Fkl (k nn
-3
-t
0) .
(5.2.26)
Thus we obtain (5.2.8).
5.2.4 Some Inaccuracies of the Simplified Model The error introduced in the results of calculation of "d due to substitution of the average value Wa(lXnl) in place of Wa(Y) depends on the relation between the
128
5. Some Problems of Excitation Kinetics
probabilities Wa and A. In the case Wa ~A (large z or n), we have
= 2(21 + 1)gl1 Wa ( rx.nl, rx.o) , Lq(y) = L9 y Wa(y, (1.0) = q(rx.nl) , q( rx.nl)
LS
(5.2.27)
LS
the last equality resulting from (5.2.18). Thus the replacement of Wa(Y) by its average value does not introduce any additional errors in this case. The alternative case, Wa ~ A, is more complicated. If Wa ~ A for every possible values of L,S, then q(y) = gyA(rx.) and L q(y) = q(rx.nl), and using the average value Wa(rx.nl) does not introduce any additional error. It is possible, however, that for some values of L,S Wa(Y) = 0 in accordance with selection rules, or Wa(r) is very small, and the terms with these Wa(y) do not contribute to Lyq(y). As an illustration we consider an s- p transition (1.o-rx. in an ion Xz+l with one electron outside the closed shells. At first we consider the orbital momentum only. If Yo = sAo LS, y = pILS, then from orbital momentum and parity conservation it follows that L = Ao = I ± 1 and Wa(y) = 0 for L = I. Therefore we have Lq(y)
=L
L
q(rx.nl)
gyA(rx.)
= (2S + 1)(41 + 2)A(rx.) ,
L-,il
(5.2.28)
= g8 ·3(21 + l)A(rx.) ,
where g8 is the spin part of the statistical weight glXllt. We see that q(rx.nl) overestimates the result by a factor of 1.5. We emphasize that to produce an accurate result isn't a simple problem since LS coupling is replaced by jl coupling with increasing values of n. In jl coupling, the selection rule L =1= I fails. The quantitative treatment of the coupling transfer is difficult. We note however that this inaccuracy is essential only for s - p transitions. In other cases, the inaccuracy introduced by substitution of Wa(rx.nl) in place of Wa(Y) is small with the possible exception of the lowest values of n. If we neglect the above-mentioned change of a coupling scheme, we can derive a sufficiently simple and accurate expression for the DR rate coefficient in an s - p transition. In this case L = Ao, and therefore it is sufficient to average Wu(y) over S and to substitute in the denominator of (5.2.17) the quantity Wa(rx.n/)
2S + 1
3(21 + 1)
= ~ 2(2S + 1) Wa(Y) = 2Ao + 1 I1
Wa(rx.nl).
In the way, which is similar to that used for the derivation of (5.2.20), we obtain for both cases (1.0 = ns and rx.o = ns 2 : (5.2.29)
This formula can be used in place of (5.2.12) n~ differing from ns by the substitution 3(21 + 1) u«(1.o, rx./) = L U«(1.oAo, tx/) -+ 2Ao U(txoAo, rx./) . (5.2.30) Ao +1
5.2 Dielectronic Recombination
129
We consider now the dependence on spin momentum S. For a single electron outside the closed shells, in accordance with (2.3.27,28),
where f and g are the direct and exchange scattering amplitudes. For a ls2p transition, f ~ g (cf. Sect. 3.2.3) and WaeL) is very small. If WaeL)~A, we have
L:q(y) s
= (2L + l)A(oc),
q(ocnl)
= 4gLA(oc) ,
where gL is the orbital part of the statistical weight grxnl. Therefore using q(ocnl) in this case, one can overestimate the result up to a factor of 4, if we assume LS coupling and f ~ g. The second assumption of the simplified model is the use of an extrapolation formula (5.2.16). This formula is applicable for n ;::: 4, but for n = 2 or 3 it may not be sufficiently accurate. In most cases terms with large n make the main contribution to the DR rate coefficient. However at z ;::: 15 for recombination of [H] and [He] ions, the levels with n = 2 and 3 are the most important. Numerical calculations show that in this case the extrapolation formula underestimates the result. The third assumption of the simplified model implies that only transitions to the ground state OCo take place. For the resonance level oc any other transitions are, evidently, impossible. For higher levels the additional radiative transitions oc - oc' lead to some increase of Kd through the factor B' in (5.2.20). As a rule, this effect is small because A <X E;rxl' and Erxrxl ~Erxrxo. On the other hand, the additional channel of autoionization y - oc' can affect the magnitude of the factor B' in (5.2.20) substantially, because Wa(ocnl,oc') increases rapidly with decrease of Erxrx/. As a result, the contribution of the levels nl satisfying the condition
decreases considerably. Accurate treatment of this effect makes the computations considerably more cumbersome (see [5.10]). It can be estimated approximately assuming Wa ~ A in the cases when autoionization to the such level oc' is possible. In other words, summation over n in (5.2.12) can be restricted to 2
n < (z RyjErxrx'
) 1/2
,Erxrx' f ~Erxrxo
An example of such a process is the dielectronic recombination
130
5. Some Problems of Excitation Kinetics
5.2.5 Numerical Calculations and Analytical Approximation Formulas Equation (5.2.11) describes a general temperature dependence of the DR rate coefficient. The temperature dependence of the factors exp (c5P) in Bd (5.2.12), although small, can nevertheless be important in some cases. To include this effect in a simple analytical formula, we replace the quantity X = ,1E/(z + 1fRy by an adjustable parameter Xd, and rewrite (5.2.11,12) in the form Kd(a)
= 1O-13Bd/P/2exp( -PXd) [cm3 S-I] ,
P = (z + ~)2RY,
Bd
=
z= B
n,
Xd
= X -,1
(5.2.31)
.
n:o:::nl
According to (5.2.31) the value of Bd is equal to its limit at high T( c5p = 0). The value of Xd can be determined by the condition that Kd is equal to its true value for some value of T = T l • The value of Bd can be calculated numerically using the simplified model, i.e., via threshold values of the partial cross sections for the transition ao - a. Burgess [5.7] proposed a simple empirical formula for the DR rate coefficient which is given in (5.1.55,56). In spite of the absence of any adjustable parameter the Burgess formula in most cases gives results in a good agreement with the results of numerical calculations. This is due to the general structure of (5.2.12). If we replace exp(c5p) by its average value, the DR rate coefficient is proportional to ,1n(l)
+ = ns - max ( I nl
I)
. (5.2.32)
We can see from (5.2.12) that ns <X (a/f)I/3 and is almost independent of the type of ion and transition. Nevertheless in some cases the error of the Burgess formula isn't negligible.
5.3 Satellites of Resonance Lines in Spectra of Highly Charged Atoms 5.3.1
Excitation by Means of DR
The photon Y-YI(anILSJ-1XQni l L l S I Jz) emitted during DR has an energy slightly different from that of the transition a - 1XQ in the ion X z + l • This corresponds to additional spectral lines in the vicinity of the line a - ao. These lines are called satellites or dielectronic satellites [5.18]. In this section we consider the simplest and most important case of the satellites of [He]- and [H]-ion l resonance lines. I We recall that the designation [H) is used for the hydrogenlike ion, [He] for the heliumlike ion and so on.
5.3 Satellites of Resonance Lines in Spectra of Highly Charged Atoms
131
Satellites of the resonance line 2 p - Is in [H] ions Xz+l correspond to transitions (5.3.1 )
2pnl - lsn/l
in [He] ions X Z • Satellites of the line Is2p I P -ls2 I S in [He] ions X;+ I correspond to transitions ls2pnl - ls2 nil
(5.3.2)
in [Li] ions, and also to numerous transitions in ions of lower charge: ls2s2pnl -
Ii 2sn/l
[Be]
Is2i2pknl-li2s22pk-In/l
(k
=
(5.3.3 ) 1 ... 6)
[B] ... [Ne].
The satellites (5.3.1-3) were observed in the spectra of ions with z ~ 10 in laboratory and astrophysical plasmas. They proved to be an effective method of plasma diagonostics, since the satellite-to-resonance-line intensity ratio is essentially dependent on temperature and in some cases on electron density. At the same time the satellites are situated very close to the corresponding resonance line, and are excited by means of DR from the same initial state as the resonance line, see (5.2.1). These are important features for plasma diagnostics. In a plasma in the state of ionization equilibrium, the satellites (5.3.3) are usually very weak. Their intensity relative to the resonance line becomes considerable at very low temperature when the absolute intensities are negligible. In transient plasmas with small characteristic time the satellites due to ions in the isoelectronic sequences [Be], [B], ... ,[Ne] can be sufficiently strong. They provide a convenient method of the estimation of the ionization state in a plasma. The energy distance between satellites and the resonance line decreases rapidly (as n- 3 ) with increasing n. In fact only satellites with n = 2 or 3 have been resolved. from the resonance line up to now. Satellites with n ~ 4 can however change the shape of the line. Apart from the transition 2 p - Is of an internal electron, the transitions of the outer one (nl - Is) are possible, although less probable. The satellites of the members of principal spectral series np - Is, lsnp - ls2 are due to such transitions. Below we confine ourselves to the most important cases of n = 2 and 3 satellites of the types (5.3.1,2). It was mentioned above that the principal way of satellite excitation is DR of the ion XZ + I . Direct excitation of an inner-shell electron Is of the ion Xz can also provide satellites of the type (5.3.2). We consider now the relative intensity of the satellite .(
I
s yd ) = I./( y, YI ) + I.II( y, YI ) , y, YI ) = TI (''/, ( ires IX, IXo
(5.3.4)
where Is and Ires are the absolute intensities of the satellite due to the transition Y - Yl. and of the resonance line IX - 1Xo. We suppose that y = IXnlLSJ and
132
5. Some Problems of Excitation Kinetics
YI = rx.onItLISIJ\, where II can be unequal to I due to configuration mixing (corresponding satellites usually being weak). The terms i' and i" in (5.3.4) correspond to two mechanisms of excitation, namely DR and direct excitation of the Is electron; for satellites of [H]-ion resonance line, i" = O. We begin with the DR excitation mechanism. In this case, (5.3.5) where Kd(Y, yd is defined by (5.2.15) with substitution of the probability of radiative transition Y - YI in place of A(y) in the numerator. (In this section we shall use the notation W for the radiative transition probabilities instead of A in order to avoid mixing the radiative probabilities and parameters of approximation of collisional rate coefficients.) In our case, rx.o = Is or Isl, IX = 2 p or Is2 p, and only one autoionization channel is possible; hence Wa(y, rx.o) = Wa(Y). Taking this into account and using the approximation from Sect. 5.1 for (vulZQat), we obtain i'(Y,YI) = a'~fJexp(~fJ)q(y,yd, q(y Y ) = 1O- 13 g 'W(Y,YI)Wa(y) , I y W(y) + Wa(Y) ,
~fJ = EIXIZ() - E ylZQ '" ..!!.. T
- n2
(5.3.6)
fJ = (z + I iRy . '
T
Here the factor 10- 13 is introduced for convenience: for z - 20, q is of the order of unity. The factor a' is
a
'=
2.
4
X
I
~2
3/2 3 7r:
2 fJ" ----±.!... _n_. + I goA'Q"
aoe fJ'
4
E (E4E )
e-__3 ~. n2~E
_0
3/2
,(5.3.7)
at
where A', "I, Q' are approximation parameters (Sect. 5.1) for (vulZQat); at large z, l. In the most interesting case fJ' > 1, the dependence of a' on temperature is very slight. Using the results of numerical calculation in the Bom-Coulomb approximation with exchange, we obtain for fJ' = 3, = 1,
e-
e
a' = 0.75 x 10-3 for satellites of [He] ions, a' = 0.47 x 10-3 for satellites of [H] ions . For applications it is very important that for all satellites with given n the dependence of i' on T is practically the same. The value of i'(y, yd is determined by a factor of q(y, yd. For small z the value of Wa exceeds the transition probability W by a factor of the order of (li,c/e 2 )3 '" 106 : (5.3.8)
5.3 Satellites of Resonance Lines in Spectra of Highly Charged Atoms
133
We see that for small z, if ~ 1 but rapidly increases with z. At large z, (5.3.9) and if is almost independent of z. In this case if becomes ~ 1 for lJ{J ~ 1. The transfer from (5.3.8) to (5.3.9) occurs at z "" 20. As an illustration, in Table 5.4 the calculated and experimental results for the satellite structure of the [He]-ion Fe XXV are shown. The value of lJ{J was determined according to the observed value of i for y = Is 2 p2 2D5/2 (the brightest and best separated satellite). The calculations of wavelengths and spontaneous transition probabilities were made using the perturbation theory expansion in the parameter 1/:?E. We note that for :?E = 26 one should take into account all relativistic interactions, even the Lamb shift of the electron Is, which is equal to 0.08 A.
Table 5.4. Wavelengths l and relative intensities for satellites of Fe XXV resonance line in X-ray spectra of the solar corona. The temperature of the plasma was determined from the intensity of l = 1.8662 A satellite Experiment
[5.19]
l[A]
i[%]
l[A]
Transition
1.8510 1.8564 1.8571
100 21 15
1.8579 1.8594 1.8608 1.8618 1.8634
23
1.8660 1.8674 1.8679 1.8700 1.8729
47 38
1.8504 1.8555 1.8566 1.8571 1.8578 1.8595 1.8610 1.8622 1.8630 1.8635 1.8659 1.8674 1.8685 1.8699 1.8727
Is 2p IpI -> Ii ISO Is 2 p 3P2 -> Ii I So a 2SI /2 -> m 2P3/2 b l 2P I/2 -> n 2SI/2 a 2P3/2 -> m 2P I/2 Is 2p 3PI -> Ii ISO b2 2P3/2 -> n 2 SI/2 a 2p3/2 -> m 2P3/2 a 2D3/2 -> m 2P I/2 b2 2P I/2 -> n 2SI / 2 a 2D5/2 -> m 2P3/2 a 2D3/2 -> m 2P3/2 Is 2s 3S1 -> Is2 ISO Is 2p 3 3P I,2 -> Is 22p2 3PI a 4P5/2 -> m 2P3/2
12 22 47
21
Theory
l: a = Is 2p2, m = Is 22p,
b l = Is (2s2ppl), n = li2s.
i'[%}
i"[%]
100 29 4.7 10.2 0.18 0.18 13 32 4.9 47 3.8
2.6 17 19.7
6
14 7.7 127 b2 = Is(2s2pp3),
134
5. Some Problems of Excitation Kinetics
5.3.2
Direct Inner-SheD Excitation
We consider now a direct inner-shell excitation of satellites of the [He]-ion resonance line (5.3.10) In the case of DR, both the resonance line and satellites are excited from the same state, namely the ground state (Xo of the ion Xz+I. In contrast, the initial state for direct excitation is the ground state of the ion X z ; hence the relative intensity i" is proportional to the ratio Nz/Nz+ I of the populations of [Li] to [He] ions. In the case of low-density (e.g., astrophysical) plasma, almost all the X z ions are in the state Is22s. In high-temperature laboratory plasma, the electron density is as high as Ne '" 1020 cm- 3 , and the levels 2s and 2p are populated in accordance with the Boltzmann formula. Since AE~T, N2p/N2s = g2p/g2s = 3. It is evident that the direct excitation of satellite levels isn't effective in the case of [H]-ion resonance line satellites since the population of the corresponding initial state Is 21 of [He] is too small. The relative intensity i" of the [He] resonance line satellite due to the direct inner-shell excitation is i"
= L:Nz("),o) . (vO"YOY). Yo Nz+I
(vO"<X()<x)
W(")',")'I) W(1') + Wi1') .
(5.3.11)
For a low-density plasma,
"v
(vO"i(2s») [I
+ D(T)] ,
D(T)
=
"d ,
"v
(5.3.12)
"v
and "d are the total rate coefficients for radiative and dielectronic where recombination, and (VO"i) is the ionization rate coefficient for the ion X z . Using approximations from Sect. 5.1 for these quantities and the approximate equality, see (5.3.6), (5.3.13) we obtain z NN
z+1
= (JE)2 AA [1 + D(T)]JP exp (JP);; + Xi V I
+ Xv
The relative intensity i" will be written then in the form i" (")" 1'd = a"[1 + D( T)] JP exp (JP) q" ("),,1'1) , "( ) _ A(1'o, 1') • W(1', 1'1) q 1',1'1 W(1') + Wa(1') ,
(5.3.14)
5.3 Satellites of Resonance Lines in Spectra of Highly Charged Atoms
{3'
= E~~o b{3 bE
135
(5.3.15)
.
Here A v, Xv, Ai(yo), Xi(YO), A', X', A(yo, y), and X(Yo, y) are parameters of the approximations (Sect. 5.1) for Kv, (vo"j(yo») , (vO"~o~)' and (va yOY ); the value of ~" --+ 1 at z ~ 1. It is clear that in the low-density case, only the satellites with y = Is 2s 21 are excited, of which only satellites beginning from the levels of electronic configuration Is 2s 2 p can be strong enough. In the case of a high-density plasma both the Is2 2s and Is2 2 p levels are populated. Therefore i"
= Nz Eo (vO"yOY)
W(y, Yl) NZ+l Yo Yo (vO"~o~) W(y) + Wa(y) (5.3.16)
Kv ,,L- gyO (VO"i ( Yo »)' gyO
=
gyO ~ L-gyO Yo
,
and all satellites can be excited. We obtain an equation similar to (5.3.15) with the change
A(yo, y)
--+
Ai(2s) b{3 + Xi(2s)
EOYoA(yo, y) , Yo
--+
Ai(2/o) ~4[b{3 + Xi(2/o)]
(5.3.17)
Substitution of numerical values in the expression for a" in (5.3 .15) shows that the values of a" in both cases of low and high densities are practically the same, and for b{3 = 1, {3' = 3, ~" = 1 are equal to
a"
=
1.4 x 10-3
(z -IOn0.6)4
.
(5.3.18)
By comparing (5.3.15) and (5.3.6), one can see that except for the value of D(T) the temperature dependences i'(T) and i,,(T) are the same. The factor D(T)
corresponds to the influence of DR on the ionization equilibrium. For temperature T '" Tm , at which Ires has the maximum value, D(T) significantly exceeds unity, and hence influences i"(T). However, at lower temperatures, D(T) rapidly decreases as exp (-3b{3) and the dependences i/(T) and i"(T) become similar. If the plasma is in the state of ionization equilibrium, satellite excitation due to DR prevails, especially at z ;:S 15 according to (5.3.18). In the case of transient
136
5. Some Problems of Excitation Kinetics
(ionizing) plasma, the role of direct excitation can be very important at z > 15. It should be noted that the characteristic ionization time increases with increasing z. In Table 5.4, values of i" for the ion Fe XXV in ionization equilibrium are given.
5.4
Populations of Excited Levels in a Plasma
By the intensity of a spectral line is usually understood the energy emitted per second by a unit volume of a plasma as a result of spontaneous transitions. For the transition k -+ i of an atom, this quantity is Iki = "'WkiAkiN(k) [ergcm- 3 s- l ]
,
(5.4.1)
where Aki is the spontaneous emission probability, and N(k) is the population density of atoms excited to the level k. We shall consider the case of an optically thin plasma in which the line radiation may freely escape and does not affect the level populations. The transition probabilities Aki are the atomic characteristics. The excited level populations are, in general case, dependent upon the variety of collisional and radiative processes. In this section we shall consider some approaches to the calculation of the level populations and also the ionization and recombination coefficients S and IX. These coefficients determine the rates of ion production and loss and are expressed in units [cm3 S-I]. Using the example of the hydrogen atom (and hydrogenlike ions) we shall describe below the approach to the numerical solution of this problem. A survey of the analytic methods of calculati~g the populations and recombination coefficients is given in [5.20]. For a detailed discussion of the problem of line intensities and populations, see [5.21-24]. Article [5.24] contains an extensive list of references. Three types of models of a plasma are usually considered: the coronal model in the limit of low density, the model of local thermodynamic equilibrium (LTE) at high density, and the models of a plasma in the intermediate region which are often referred to as the collisional-radiative models. (For the conditions of applicability of the coronal and LTE approximations see Sect. 1.2.) Simple relations between the atomic level populations exist in the high-density limit when relaxation for any atomic level is determined by collisional processes. In LTE plasmas populations are completely determined by the temperature, total density of atoms and chemical composition of a plasma, and are independent of the cross sections of elementary processes, see (1.2.2, 3). A comprehensive discussion of the validity conditions for LTE can be found in [5.25]. When LTE conditions are violated, the populations of atomic levels are determined by all collisional and radiative processes. The processes to be included in calculations are the following: collisional excitation and deexcitation, ionization and the inverse process of three-body recombination, radiative and dielectronic recombination, spontaneous radiative decay, and collisional and radiative cas-
5.4 Populations of Excited Levels in a Plasma
137
cades. When the degree of ionization is not too low, only the electronic collisions are of importance. 5.4.1
Populations of the Hydrogen Levels at Low Plasma Densityl
In the low-density limit (coronal litnit, see Sect. 1.2), decay of the excited
levels is provided exclusively by spontaneous radiative transitions2 • Hence it follows that the population densities for all the levels except the ground state are extremely low. An excited level n is populated by direct processes which are the excitation from the ground state by electron impact and radiative recombination, and by cascade from the higher levels. For nonhydrogenic ions, dielectronic recombination has to be taken into account as a direct process. The steady-state rate equations may be written in the form
2: N(n')An'n + qn . (5.4.2) n'>n In this equation, N(n) is the density of atoms in the level with the principal quantum number n, An = 2:nll
(5.4.3) where N(l) is the population density of the ground level, (VO'ln) is the rate coefficient [cm3 S-I] of excitation by electron impact averaged over the Maxwellian distribution, N(H+) is the density of bare nuclei, and "v(n) is the rate coefficient of radiative recombination to form an atom in level n. It is assumed that all levels with the different orbital quantum numbers are populated proportionally to their statistical weights:
N(nl)
= 21 -; 1N(n)
. (5.4.4) n The solution of the equilibrium equations (5.4.2) may be written in the form N(n) =
" C(n,, n)qn' A1L..J nn'?,n
,
(5.4.5)
where C( n, n) = 1. The element of the cascade matrix C( n', n) is the probability that excitation of n' is followed by all possible cascade radiative transitions to level n. Let P(n', n) be the probability that the direct radiative transition from n' to n takes place:
P(n', n)
= An'n/An'
.
The content of this section is based on [5.26]. The relaxation of metastable levels or of levels with large principal quantum numbers n ~ 1 is determined by collisional processes even at very low density. 1
2
5. Some Problems of Excitation Kinetics
138
For C(n', n), we then have
+ 1, n) =
C(n
P(n + 1, n) , (5.4.6)
C(n +2, n) = P(n + 2, n + 1)C(n + 1, n) +P(n +2, n) ,
C(n + m, n) = P(n + m, n + m - 1) C(n + m - 1, n) +P(n + m, n + m - 2)C(n + m - 2, n) + ... + P(n + m, n) . With C(n, n) = 1 we obtain generally n+m-I
C(n
+ m, n) = E
+ m, n') C(n', n)
P(n
(5.4.7)
.
n'=n
Using (5.4.7) one may calculate similarly the radiative cascade matrix for any other atom once the matrix elements P( n', n) (or radiative transition probabilities) are known. The number n in this case may be considered as an index labelling the atomic levels in the order of increase of the energy. Table 5.5 gives the cascade matrix elements C(n + m, n) for n ~ 10, m ~ 10 calculated by Seaton [5.26]. For m 2:: 5, the calculated values can be fitted to
C(n + m, n) = C(oo, n) + An/m . The quantities C( 00, n) are also given in Table 5.5. For application to the excited levels with n > 10, one may use an analytical formula obtained in [5.27] using the Kramers approximation:
2 ln (n3) C( n + m, n) = n3 2"
x
(1 1) n2 - (n + m)2
-I [
0.5772 -In
(
r
1 1)
n2 - (n + m)2
(5.4.8)
2
Table 5.5. Cascade matrix C( n + m, n) for hydrogen in the case of optically thin plasma m
n
1 2 3 4 5 6 7 8 9 10 C(oo,n)
2
3
4
5
6
7
8
9
10
0.4418 0.4105 0.3991 0.3934 0.3903 0.3883 0.3870 0.3860 0.3853 0.3848 0.3796
0.2978 0.2601 0.2454 0.2380 0.2336 0.2308 0.2289 0.2274 0.2264 0.2255 0.2174
0.2336 0.1947 0.1791 0.1710 0.1661 0.1627 0.1605 0.1589 0.1575 0.1564 0.1468
0.1975 0.1587 0.1430 0.1347 0.1294 0.1260 0.1236 0.1217 0.1203 0.1191 0.1088
0.1744 0.1361 0.1206 0.1120 0.1068 0.1033 0.1008 0.0990 0.0975 0.0964 0.0860
0.1581 0:1203 0.1052 0.0968 0.0916 0.0881 0.0854 0.0835 0.0821 0.0809 0.0703
0.1464 0.1093 0.0942 0.0858 0.0806 0.0771 0.0745 0.0725 0.0710 0.0698 0.0590
0.1369 0.1006 0.0858 0.0775 0.0723 0.0688 0.0662 0.0642 0.0627 0.0615 0.0505
0.1295 0.0939 0.0791 0.0711 0.0660 0.0624 0.0598 0.0578 0.0563 0.0551 0.0441
5.4 Populations of Excited Levels in a Plasma
139
The error of formula (5.4.8) does not exceed 15 percent. When m is large, the error decreases. This is in accordance with the accuracy of the Kramers approximation. The formula (5.4.5) for the population density includes the total spontaneous decay probability An. Let An be written in the form
(5.4.9)
where oc = e2 /fic = 1/137 is the fine-structure constant, c is the velocity of light, and ao = fi2/me 2 = 0.529 x 10- 8 cm is the Bohr radius. The values of r(n) are given in Table 5.6. For n ~ 20, r(n) may be fitted to r(n)c::'3lnn-0.247. For applications, the analytical formulas of the Kramers approximation are often useful: 2AOZ4
Ann' = n3n'( n2 - n'2)'
= Aoz4ln
A
n5
n
(n3 2- n)
According to (5.4.3,5) in the limit of Ne -+ 0 the population density for any excited level is negligibly small compared to the electron density, densities of the ground level atoms and bare nuclei. The total number density of the excited levels is also much smaller than these quantities. Therefore at low density, the ionization rate is provided by the direct collisional ionization from the ground state. The only process of recombination for hydrogen and hydrogenlike ions is radiative recombination. The rate coefficient of recombination is determined by the sum over principal quantum numbers, 00
oc
=
Kv
=
LKv(n) . n=!
Table 5.6. Factor r(n) n
2
3
r(n)
1.911
3.084
n r(n)
10 6.657
11 6.943
4
5
3.929 12 7.205
13 7.442
4.589
8
9
6
7
5.132 14 7.668
5.590
5.989
15 7.876
20 8.740
6.389 25 9.410
140
5. Some Problems of Excitation Kifietics
5.4.2 Intermediate Density. Collisional-Radiative Model of a Plasma At intermediate densities one has to take into account both radiative and collisional cascade transitions. Here we shall also consider hydrogenlike ions. It is assumed that the relationship (5.4.4) is satisfied, the free electrons have a Maxwellian distribution, and that the plasma is optically thin for the line radiation. The rate equations which determine the population densities N(z)(n) of the bound levels of an ion Xz may be written in the form (5.4.10) where rn is the total decay probability of the level n[s-I] including the radiative decay probability An = L:nl
r
_ {Wmn +Amn mn -
Wmn
when m < n , when m < n .
The recombination frequency Rn includes the radiative recombination term NeKv(n) and three-body recombination term Kr(n)N;. N(z+I) is the bare-nuclei number density. The calculation of the instantaneous population densities requires the solution of a set of equations (5.4.10). Due to the electric microfield of a plasma, the higher levels merge into a continuum and the number of bound levels is finite (this problem is beyond the scope of this text, see, e.g. [5.21,28-30]). Nevertheless this number is large enough, especially at low densities. In actual numerical calculations one can confine oneself to considerably smaller principal quantum number no. Here we give a simple explicit estimate of no (for a detailed analysis see [5.31]). The values of no can be chosen taking into account the fact that for n large enough, the collisional processes are- much more important than the radiative processes. The radiative decay probability decreases rapidly with n: An ()( n- 5. The collisional frequency for the transitions n -4 n ± 1 increase ()( n4, and the collisional ionization frequency W~ ()( n2. Therefore the population and decay of highly excited levels are determined by exclusively electronic collisions. When n ~ 1, Wn, n± I ~ W~, and the electron stepwise motion between the highly excited states is like a slow diffusive motion [5.32-34]. Hence for n greater than some value no, the populations are determined by the balance of three-body recombination and ionization by electron impact, and therefore satisfy
5.4 Populations of Excited Levels in a Plasma
141
the Saha-Boltzmann equations, see (1.2.3,4),
N(z)(n)
= NE(n) = N(z+l)
Bn(T) =
. NeBn(T) ,
~~ exp (z:~;),
s = 2 (2~;1t y/2 Ne
(5.4.11)
.
The value of no may be roughly estimated from the condition
W~o ~Ano .
(5.4.12)
The frequency of ionization W~ = Ne (VO"j (n )) may be estimated using the classical Thomson formula for the cross section (Sect. 5.1). In this case (VO"i(n)) x[1
IR
= 8Vn~2a~ E~ 13/2 f33/2exp (-13)
+ f3exp(f3)Ei(-f3)],
For highly excited levels j
Wn~
13 ~ I,
13 = IEnl/T = z 2Ry/n2T
.
(5.4.13)
and it follows from (5.4.13)
8.7 x 10- 8 2 (z2RY) 1/2 3 n -Ne z T
.
(5.4.14)
Using (5.4.9) for estimation of the radiative decay probability An [assuming for simplicity -r(n) = 10] we obtain from the condition (5.4.12) no
~ z (1018 )
1/7
Ne
(~) 1/14
.
z2Ry
(5.4.15)
For the range of electron temperature of 0.01-100 eV and an electron density of 108-IO I5 cm- 3, it follows from (5.4.15) that 2 ~ no/z ~ 30 . To find the level populations and the ionization state of a plasma one has to solve the several sets of equations (5.4.10) for ions of the different stages of ionization z under the conditions that the density of the nuclei of each element is conserved and the plasma is electrically neutral. If temperature and density change not too rapidly, the computational problem can be simplified. 5.4.3
Quasi-Stationary Approach for Hydrogen
The small perturbations from the steady state relax in a time of order 1/ r n. The relaxation time of any of the excited levels is always much shorter than that of the ground level l . Hence the time in which the population densities ofthe excited 1 The estimate for the relaxation time given above is rather rough. In actual cases the relaxation time for one level depends on that for all other levels and on initial conditions, and may be an order of magnitude larger than 1/ Tn [5.35]. For metastable levels of atoms and ions other than hydrogen and hydrogenlike ions the relaxation time can be great.
142
5. Some Problems of Excitation Kinetics
levels come into correspondence with the instantaneous population density of the ground level, free electrons and bare nuclei H+, is very short. Thus the quasisteady approximation is obtained by setting dN(z)(n)/dt = 0 for all the levels except the ground level. The population density of the ground level should change comparatively slow, on a time scale much longer than the longest relaxation time for the excited levels, but in general will not be necessarily in equilibrium with the electron density and the number density of bare nuclei. The quasi-stationary approach given in the works of Bates et al. [5.36,37] enables population densities and coefficients of recombination and ionization to be tabulated in a wide range of electron temperature and density. These quantities are tabulated for hydrogen and hydrogenlike ions (see, e.g. [5.37-41]. More recent values are given in [5.40]. New results for helium and additional references may be found in [5.42]. It is convenient to express the populations in terms of Saba-Boltzmann equilibrium values NE(n), see (5.4.11), b(n)
= N(z)(n)/NE(n)
.
For hydrogen N(z+l) in (5.4.11) is equal to N(H+). Using this notation the rate equations for the levels with 2 :s; n :s; no can be rewritten b(n)rn - L:b(m)NE(m) rmn - N(H+) Rn min NE(n) NE(n)
=0 .
(5.4.16)
Taking into account (5.4.11) and the relationship NE(1)Wln = NE(n)Wnl ,
(5.4.16) may be reduced to Bm(T)
b(n)rn-
Rn
~b(m)Bn(T) • rmn= NeBn(T)
N(l)
+ Ndl)Wnl.
(5.4.17)
m¥1
The first term in the right-hand side of (5.4.17) corresponds to the direct recombination to the level n and depends on Ne and Te only. The second term corresponds to the excitation from the ground state and is proportional to N(1). The solution of this set of no - 1 equations may be expressed by the sum of two terms N(n) N(1) b(n) = NE(n) = ro(n) + rl(n) NE(1) .
(5.4.18)
The first term determines both direct and cascade populating from the continuum and the second term corresponds to the direct and stepwise excitation from the ground state. With the use of (5.4.18) the differential equation for N(1) may be written in the form (5.4.19)
5.4 Populations of Excited Levels in a Plasma
143
The quantity IX =
1 [ Ne Rl
NE(n)
+ n~lN(H+{o(n)rnl
]
,
following the works by Bates et at. [5.36,37] is referred to as the collisionalradiative recombination coefficient, and the quantity S
=
1 [ Ne r
l -
NE(n)
n~lNE(1{l(n)rnl
]
is referred to as collisional-radiative ionization coefficient. The steady-state value of N(1) is given by the relation N(1)=N(H+):§ .
(5.4.20)
As was noted in Sect. 1.2, the total population of all the excited levels is usually considerably smaller than the ground level population densityl LN(n)~N(1) , Ne , N(H+) .
(5.4.21 )
n>l
Therefore the coefficients IX and S may be regarded as the total rate coefficients of recombination and ionization2 • When one of the inequalities (5.4.21) is not satisfied the steady state solution may not be valid. In the low-density limit the net ionization rate is equal to the rate coefficient of ionization from the ground state (VO"i (1»), and IX is equal to the radiative recombination rate. At low densities, Wnl
rl(n) = -A ex: Ne , nl
and ro(n) depends on T only. In the high-density limit, collisional cascades are of major importance and the quantities ro and rl become independent of Ne . Some numerical data for ro, rl, IX, and S from the work by Johnson and Hinnov [5.39] are given in Table 5.7 (for more recent results see [5.40]). The quasi-steady level population densities at a given temperature T are determined by (5.4.18) on substituting the values of electron density N e, the density of protons N(H+) and the population density of the ground level N (I). In a plasma composed of hydrogen only Ne = N(H+). The steady-state population densities are to be found with the condition (5.4.20) taken into account. The steady-state populations for the ground level are given in [5.43].
I The problem of an upper limit of n for the sum over excited levels in (5.4.21) is outside the scope of this text. 2 S and 0( do not correspond to coefficients giving the rate at which electrons leave the ground level and come to it. They are smaller than such coefficients would be.
109
4.9-6 2.5-17Ne 1.4-3 1.0-17Ne 1.1-2 7.2-18Ne 3.2-2
6.1-18N.
5.8-2 5.5-18Ne 1.2-26 7.9-13
rl(3)
n(5)
ro(6)
rl(6) S
IX
rl(6) S
ro(6)
rl(5)
ro(5)
rl(4)
ro(4)
n(3)
7.5-18 4.9"':13
4.5-18Ne
2.4-1 4.4-7 4.5-1 3.0-7 1.3-17 7.3-13
2.0-2 8.2-18Ne 6.1-2 6.0-18Ne l.l-I 5.0-18Ne 1.5-1
ro(3)
1.5-1 4.8-8 2.4-1 4.1-8 1.0-17 6.1-13
1.9-17N.
rl(2)
2.6-2 8.2-8 8.2-2 5.9-8
1.2-3
ro(2)
1.8-3 1.9-6 3.3-2 8.1-7 l.l-I 5.7-7
1.5-3 1.9-7
0
Ne
2.0-17 1.0-12
7.9-1 1.2-{j
5.5-1 2.7-{j
5.0-2 8.0-6 2.2-1 5.1-{j
2.5-3 1.9-5
10
lOll
1010
IX
ro(5)
rl(4)
ro(4)
12
3.1-3 1.0-6 2.8-2 7.1-7 1.0-1 5.7-7 2.7-1 4.3-7 3.2-26 1.7-12
2.2-3 1.0-7 1.8-2 7.2-8 5.5-2 6.0-8 1.1-1 5.2-8 2.1-26 1.2-12
ro(3)
rl(2)
ro(2)
1.1-5 2.5-{j
1011
7.6-6 2.5-7
1010
6.2-6 2.5-8 1.8-3 1.0-8 1.5-2 7.2-9 4.2-2 6.0-9 8.1-2 5.4-9 1.6-26 1.0-12
Ne
0
Table 5.7. Parameters ro(n), rl(n) and coefficients S and IX
1013
10 14
8.6-1 1.0-5 2.1-25 7.1-12
T = 8 x 103K. 4.5-3 1.3-2 1.9-3 1.9-4 1.2-1 4.3-1 7.7-5 6.1-4 5.6-1 8.3-1 3.1-5 1.7-4 9.5-1 8.4-1 1.1-5 5.0-5 9.4-1 9.8-1 1.7-5 4.0-6 4.3-17 1.5-16 1.7-12 3.9-12
1013
6.4-1 2.3-{j 6.5-26 2.9-12
T = 4 x 103K. \.9-5 4.9-5 2.5-5 2.5-4 2.2-2 6.0-3 1.0-5 1.0-4 3.1-1 7.3-2 5.7-5 6.9-6 3.3-1 6.8-1 4.4-{) 2.5-5
10 12
7.1-2 1.8-2 7.2-1 4.5-3 9.3-1 l.l-3 9.8-1 3.2-4 9.9-1 1.1-4 9.4-16 1.4-11
10 15
9.4-1 7.2-5 1.3-24 2.7-11
2.4-4 2.5-3 \.3-1 1.1-3 6.0-1 4.8-4 8.5-1 1.8-4
10 14
3.7-1 1.0-1 8.5-1 2.4-2 9.6-1 5.9-3 9.9-1 1.7-3 1.0 5.9-4 5.0-15 7.1-11
10
16
9.6-1 7.7-4 1.4-23 1.6-10
9.0-1 2.0-3
2.2-3 2.4-2 3.5-1 1.3-2 7.4-1 5.3-3
10 15
1.0 3.3-3 1.0 1.1-3 9.5-15 3.2-10
7.0-1 2.0-1 9.3-1 4.7-2 9.8-1 1.1-2
10 17
\.8-2 2.0-1 4.2-1 1.1-1 7.7-1 4.5-2 9.2-1 1.6-2 9.7-1 6.5-3 1.2-22 1.4-9
10 16
1.0-14 2.4-9
1.0 3.6-3 1.0 1.2-3
7.7-1 2.2-1 9.5-1 5.1-2 9.9-1 1.2-2
10
18
6.2-2 6.7-1 4.5-1 3.9-1 7.9-1 1.5-1 9.2-1 5.6-2 9.7-1 2.2-2 4.0-22 1.3-8
10 17
2.3-27Ne
1.0 3.6-3 1.0 \.3-3 1.1-14
7.1-1 2.2-1 9.5-1 5.2-2 9.9-1 1.3-2
00
9.7-1 3.0-2 5.4-22 1.3-25Ne
m ~
9.2-1 7.7-2
0
on
(")
:t.
[
0 ::I
~.
...o.
....0
I'D
a"
a'"C
(II
8
til
8on
y.
-t
8.5-2 9.2-1 4.7-1 5.3-1 7.9-1 2.1-1
00
for optically thin hydrogen plasma [5.39]. T=103 K. 4.9 -6 denotes 4.9x 10- 6 •
S ex
ro(6) rl(6)
ro(5) rl(5)
ro(4) rl(4)
n(3)
ro(3)
ro(2) rl(2)
S ex
ro(6) rl(6)
n(5)
ro(5)
8.6-11 2.1-13
7.3-11
6.7-11
1.8-13
1.8-13
5.3-1 3.1-8
1.9-13
5.7-1 3.4--6 8.0-1 1.5--6 9.1-1 6.0-7
3.4-1 6.3--6
4.1-1 4.5-7 5.5-1 3.2-7 7.2-1 1.9-7
2.7-1 6.8-8
3.7-1 4.8-8 4.5-1 3.8-8
1.5-1 1.5-5
4.4-13 4.3-13
1.4-1 1.5--6 2.9-1 6.7-7
3.6-13
6.0-1 2.2-7 3.4-13
1.6-1 6.8--6 3.9-1 4.0--6 7,0-1 1.8--6 8.7-1 7.7-7
3.5-2 1.6-5
10 12
1.3-1 1.5-7
6.2-11
3.6-18Ne
1.3-1 1.5-17Ne 2.5-1 6.9-18Ne 3.4-1 5.0-18Ne 4.0-1 4.1-18Ne 4.5-1
3.0-13
3.8-1 3.4-8 3.0-13 3.3-13
4.0-1 3.5-7
2.4-1 4.9-7
2.0-1 5.1-8 2.9-1 4.1-8
ro(4) rl(4)
ro(3) rl(3)
n(2)
2.9-2 1.6-6 1.3-1 7.0-7
2.6-2 1.6-7 1.1-1 7.1-8
2.3-2 1.6-17Ne 9.8-2 7.2-18Ne 1.8-1 5.2-18Ne 2.4-1 4.4-18Ne 2.9-1 3.8-18Ne 2.6-13
ro(2)
1011
1010
0
Ne
Table 5.7. (continued) 10 14
9.9-1 6.6-6 1.7-12 9.2-13
9.8-1 1.9-5
9.2-1 7.1-5
2.4-13
8.4-1 1.4-5 9.5-1 4.2--6 9.8-1 1.5--6 1.1-10
5.0-1 4.9-5
3.1-13
2.0-10
1.0 3.8--6
9.6-1 4.2-5 9.9-1 1.1-5
8.2-1 2.1-4
T = 3.2 x 104 K. 1.9-1 2.8-1 1.5-4 1.3-3
7.4-1 1.9-5 9.1-1 5.9--6 9.7-1 2.1--6 7.1-13 5.7-13
T = 1.6 x 104 K. 4.9-2 9.6-2 1.5-3 1.6-4 3.0-1 6.8-1 5.9-5 3.3-4
lOB
4.9-10 4.8-13
7.0-13
7.6-10
1.0 1.8-5
1.0 5.5-5
1.0 3.4-5 1.0 1.1-5
1.0 2.1-4
9.9-1 1.2-3
9.2-1 1.3-2
1.0 2.0-5 8.2-10 9.0-12
1.5-12
1.0 6.0-5
1.0 2.3-4
1.0 1.3-3
9.8-1 1.4-2
8.0-11
1.0 8.4-5 1.9-11
1.0 9.6-4 1.0 2.5-4
1.0 5.1-3
9.6-1 4.0-2
lOIS
1.0 2.0-5 8.2-10
1.0 5.9--6
1.0 2.3-4
1.0 1.3-3
9.8-1 1.4-2
1.0 8.3-5 1.8-11 1.2-11
1.0 6.8-5 1.5-11 4.8-12
1.0 9.4-4 1.0 2.5-4
9.9-1 4.9-3
9.4-1 3.9-2
1O l7
9.9-1 7.8-4 1.0 2.0-4
9.7-1 4.1-3
7.8-1 3.2-2
10 16
9.9-1 1.3-4
9.5-1 7.3-4
6.1-1 7.2-3
2.0-12
1.0 2.7-5 6.1-12
9.8-1 3.0-4 9.9-1 8.1-5
8.9-1 1.6-3
3.2-1 1.1-2
10 15
8.3-30Ne
1.0 2.0-5 8.2-10
1.0 5.0-5
1.0 2.3-4
1.0 1.3-3
9.9-1 1.4-2
7.5-29Ne
1.0 8.5-5 1.9-11
1.0 2.5-4
1.0 9.6-4
1.0 5.1-3
9.6-1 4.0-2
00
t""'
~
VI
-
I»
'"3
5i
'tI
I»
'"S·
< g.
C1l
0..
C1l
a·
ttl ><
'"0 ....,
::s
...5io·
~
>c:I
0
:,:.. 'tI
VI
5.6--14
6.7-9
5.6--14
1.5 2.3-17Ne
S
IX
ro(2) n(2) ro(3) rl(3)
IX
S
ro(4) n(4) ro(5) rl(5) ro(6) rl(6)
1.1 4.5-7
1.2 5.3-8
1.1 4.4-8 2.8-8 1.5-14
1.1 5.0-18Ne 2.8-8 1.5-14
2.9-8 1.5-14
1.1 2.9-7
1.2 6.3-7
1.5 2.3-6 1.3 9.5-7
5.7-14
7.2-9
9.0-1 2.1-7
7.9-1 5.2-7 8.4-1 3.6--7
1.2 6.7-8
1.5 2.3-7 1.3 9.7-8
7.7-1 5.6--8 8.0-1 4.4-8 8.2-1 3.6--8
7.4-1 7.8-7
6.9-1 1.8-6
1011
1.2 7.0-18Ne 1.2 5.7-18Ne
1.3 1.0017Ne
6.9-9
7.6--1 5.9-18Ne 7.8-1 4.8-18Ne 7.9-1 4.2-18Ne
ro(4) rl(4) ro(5) rl(5) ro(6) rl(6)
7.3-1 8.1-8
6.9-1 1.8-7
6.8-1 1.8-17Ne 7.2-1 8.2-18Ne
ro(2) rl(2)
ro(3) rl(3)
1010
0
Ne
Table 5.7. (continued)
3.0-8 1.5-14
1.0 9.8-7
1.1 2.2-6
1.1 4.6-6
1.5 2.3-5 1.2 8.8-6
5.7-14
7.7-9
7.0-1 1.8-5 7.7-1 7.2-6 8.5-1 3.7-6 9.3-1 1.6-6 9.7-1 6.7-7
10 12
1.2-8
1.0 7.5-6
1.0 3.5-6
3.3-8 1.5-14
1.0 6.2-6 1.0 2.4-6
1.1 1.9-5
1.0 5.3-6 4.1-8 1.5-14
1.0 1.5-5
1.0 5.2-5
5.8-8 1.5-14
1.0 1.1-5
1.0 1.1--4 1.0 3.1-5
1.1 6.3-3 1.0 6.0--4
1.9-8 6.5-14
1.0 8.1-5
9.9-1 4.5--4
9.2-1 5.1-3
1.0 2.2-5
6.1--41 T = 5.12 x IO sK. 1.4 1.5 1.7-3 2.2--4 1.0 1.1 6.5-5 2.5--4
8.9-9 5.9-14
9.5-1 1.4-5 9.8-1 4.3-6 9.9-1 1.6-6
x IO sK. 7.9-1 1.4-3
T = 1.28 7.3-1 1.7--4 8.5-1 5.1-5
lOIS
9.5-1 1.9--4 9.9-1 3.6--5 1.0 1.0-5
10 14
1013
6.7-8 1.5-14
1.0 1.4-5
1.0 3.9-5
1.0 1.4--4
1.0 8.7-3 1.0 7.6--4
7.2-14
2.2-8
1.0 9.5-6
1.0 1.0--4 1.0 2.8-5
1.0 5.8--4
9.8-1 7.0-3
10 16
1.0 1.4-5 6.8-8 2.4-14
1.0 4.0-5
1.0 1.5--4
1.0 9.0-3 1.0 7.9--4
1.4-13
2.2-8
1.0 9.8-6
1.0 1.1--4 1.0 2.8-5
1.0 6.0--4
9.9-1 7.3-3
10 17
1.0 1.4-5 6.8-8 1.2-13
1.0 4.0-5
1.0 1.5--4
1.0 9.0-3 1.0 7.9--4
7.7-13
2.2-8
1.0 9.8-6
1.0 1.1--4 1.0 2.9-5
1.0 6.0--4
9.9-1 7.3-3
10 18
6.8-8 1.0-31Ne
1.0 1.5--4 1.0 4.0-5 1.0 1.4-5
1.0 9.0-3 1.0 7.9--4
7.0-31Ne
2.2-8
1.0 9.8-6
1.0 1.1--4 1.0 2.9-5
1.0 6.0--4
9.9-1 7.3-3
00
0
'"
(1)
e. 0
~
::I
e. 0
O.
><
-'"
tTl
0
'"....,
!3
0
0-
...'"ti 0
(1)
!3
en
VI
0'1
. j>.
3.4 1.6-6 2.4 6.4-7
1.5 4.S-S
3.4-S
3.4-15
3.4 1.6-7 2.5 6.5-8
1.9 3.5-8
I.S 3.O-S 2.5-S 6.5-16
1.6 5.1-ISN.
1.5 4.4-ISN.
3.3-8
3.4-15
3.4 1.6-17N.
2.5 6.6-ISN.
2.2 4.5-1SN.
2.0 3.7-ISN.
1.9 3.2-ISN. 2.5-8 6.5-16
ro(5) n(5)
ro(6) n(6)
S
ex
ro(2) rl(2)
ro(3) n(3)
ro(4) rl(4)
ro(5) rl(5) ro(6) n(6)
ex
S
3.4-15
1.7 6.1-8
1.7 6.3-1SN.
ro(4) rl(4)
2.1 4.4-8
1.5 4.O-S
1.9 S.9-8
1.9 0.9-ISN.
2.6-8 6.5-16
1.7 2.4-7
1.9 3.2-7
2.1 4.2-7
3.4-S
1.3 3.0-7
1.5 4.3-7
1.6 5.S-7
1.9 S.7-7
2.4 2.2-6
2.4 2.2-7
2.5 2.2-17N.
1011
ro(2) n(2) ro(3) rl(3)
1010
0
N.
Table 5.7. (continued)
2.6-8 6.4-16
1.3 1.1-6
1.6 2.1-6
1.9 3.7-6
3.3 1.6-5 2.4 6.1-6
3.3-15
3.2-15
4.7-8
1.0 7.0-6
1.0 1.9-5
4.6-8 5.8-16
1.0 I.S-5
1.0 4.S-5
5.8-S 5.7-16
1.0 2.6-5
1.0 7.2-5
1.0 2.5-4
1.0 1.2-3
l.l S.0-4 1.0 1.6-4
1.2 1.3-2
3.0-15
7.7-8
1.0 2.1-5
1.0 5.7-5
2.0 7.2-3
3.0-15
6.5-S
1.0 1.5-5
1.0 4.3-5
1.0 1.5-4
l.l 6.3-5 1.0 2.0-4
1.0 1.0-3
l.l 7.6-4
1.2 2.8-4
1016 l.l 1.1-2
1015 1.4 7.4-3
T = S.l92 x 106 K. 3.2 2.9 1.4-3 1.6-4 2.1 1.5 5.2-5 2.7-4 1.5 l.l 2.0-5 6.4-5 1.2 1.0 7.5-6 2.0-5 l.l 1.0 3.1-6 7.5-6 3.3-S 2.S-8 6.4-16 6.2-16
3.9-8 3.3-15
1.0 3.0-6
l.l 1.2-6
1.2 2.2-5
1.6 6.5-5
1.1 7.6-6
3.6-8
1014
T = 2.04S x 106 K. 2.1 1.4 2.1-4 1.7-3
1013
1.3 2.4-6
1.5 4.7-6
I.S S.2-6
2.3 2.1-5
1012
6.O-S 6.6-16
1.0 2.8-5
1.0 7.6-5
1.0 2.6-4
1.0 1.3-3
1.0 1.4-2
4.1-15
7.S-8
1.0 2.1-5
1.0 5.9-5
1.0 2.1-4
1.0 1.1-3
1.0 1.2-2
10 17
6.0-8 1.6-15
1.0 2.8-5
1.0 7.7-5
1.0 2.7-4
1.0 1.3-3
9.9-1 1.4-2
1.5-14
7.9-8
1.0 2.1-5
1.0 5.9-6
1.0 2.1-4
1.0 1.1-3
9.9-1 1.2-2
1018
6.6-S 1.1-33N.
1.0 2.8-5
1.0 7.7-5
1.0 2.7-4
1.0 1.3-3
9.9-1 1.4-2
1.2-32N.
7.9-8
1.0 2.1-5
1.0 5.9-5
1.0 2.1-4
1.0 1.1-3
9.9-1 1.2-2
00
.".
-I
-
1>0'>
!3
1>0'> fI.I
:g
1>0'>
S·
fI.I
a.
<
~
8-
!3.
>e
-
trI
0
fI.I
= ....
1>0'>
g.
E.
.g
~
'"C
VI
5. Some Problems of Excitation Kinetics
148
5.4.4 Hydrogen6k.e Ions Both in the coronal limit and at high density, the temperature at which the ions Xz exist is proportional to the ionization potential Ez. For hydrogenlike ions, Ez = z 2Ry. When T <X z2, the quantities (va) <X z-3. The spontaneous radiative transition probabilities Ann' <X z4. Therefore the reduced density and temperature fie
= Ne/z7, f = T/z2
are convenient when considering the ions. At given fie and f, the quantities ro, rio rx./z, and z 3S do not depend on z. The Saba-Boltzman equation (5.4.11) may be rewritten in the form
NE(n) = where Q density
~ n28~/2 :~ (z2:y) 3/2 exp ( ; )
,
(5.4.22)
= Ne/N(z+I). From (5.4.18), it follows that the reduced population
fI(n) = QN(z)(n)/zll
(5.4.23)
will not depend on z. Table 5.8 gives some values of ro, rio rx./z, and z 3S from data of the work by McWhirter and Hearn [5.38). The population densities are obtained by substituting NE(n) from (5.4.22) into (5.4.18) with N(z+l) instead of N(H+). The more recent quantitative results can be found in [5.40,43). The difference between two sets of coefficients ro, rl given by Tables 5.7 and 5.8 is great at low temperature T ~z2Ry. It can be explained by different threshold behaviour of the cross sections for neutral atom and for ion (the excitation cross Table s.s. Parameters ro(n),rl(n) and coefficients S and thin plasma [5.38]. 4.7--6 denotes 4.7 x 10-6 1/e
0
108
1010
1012
ro(2)
4.7--6
5.9-6 1.2-8
8.8--6 1.2--6
3.6-5 1.2-4
1.6-4 1.2-3
1.3-3
1.6-3 5.5-9
2.5-3 5.5-7
1.5-2 5.5-5
1.0-2
1.4-2 5.1-9
2.2-2 5.0-7
2.9-2
3.9-2 4.3-9
7.9-2
1013
ro(3)
rl(3) ro(4)
rl(4) ro(5)
rl(5) ro(7)
rl(7)
for hydrogenlike ions in the optically lOIS
1016
1018
00
103z 2K. 1.4-3 1.2-2
1.3-2 1.1-1
6.1-2 5.1-1
1.1-1 8.9-1
1.1-1 8.9-1
9.6-2 5.7-4
3.2-1 6.4-3
4.3-1 6.0-2
4.7-1 2.9-1
5.0-1 5.1-1
5.0-1 5.1-1
2.1-1 4.2-5
5.2-1 2.9-4
6.9-1 2.9-3
7.5-1 2.7-2
7.7-1 1.3-1
7.8-1 2.2-1
7.8-1 2.2-1
7.0-2 4.1-7
5.5-1 2.3-5
7.8-1 1.3-4
8.7-1 1.3-3
8.9-1 1.2-2
9.0-1 5.8-2
9.0-1 1.0-1 I
9.0-1 1.0-1
1.1-1 3.4-9
3.2-1 2.7-7
8.8-1 6.3--6
9.5-1 3.0-5
9.7-1 3.0-4
9.8-1 2.8-3
9.8-1 1.4-2
9.8-1 2.4-2
9.8-1 2.4-2
T
rl(2)
IX
=4 x
1014
S ·z3
9.1-26
1.1-25
1.9-25
1.0-24
6.1-24
4.6-23
3.7-22
2.0-21
3.5-21
3.8-21
IXlz
7.9-13
9.2-13
1.4-12
5.2-12
2.0-11
1.1-10
8.6-10
8.0-9
7.6-7
7.6-251/e
5.4 Populations of Excited Levels in a Plasma
149
Table 5.8. (continued) fIe
0
108
1010
1012
ro(2) n(2)
1.1-3
1.3-3 8.9-9
1.5-3 8.9-7
ro(3) rl(3)
1.9-2
2.2-2 4.2-9
2.7-2 4.1-7
3.1-3 8.8-5 6.9-2 4.0-5
ro(4) n(4)
5.9-2
6.7-2 3.5-9
7.5-2 3.4-7
3.3-1 2.6-5
ro(5) rl(5)
1.0-1
1.2-1 3.2-9
6.5-1 1.3-5
ro(7) rl(7)
1.8-1
2.2-1 2.5-9
1.6-1 3.0-7 4.0-1 2.0-7
S ·z3
4.9-17
5.3-17
(lIz
4.8-13
ro(2) n(2)
1013
1014
10 15
1016
1018
2.1-1 6.4-2 7.7-1 1.8-2
6.0-1 1.9-1
7.6-1 2.4-1
8.9-1 5.1-2
9.4-1 6.5-2
7.6-1 2.4-1 9.4-1 6.5-2
9.3-1 5.5-3
9.7-1 1.6-2
9.8-1 2.0-2
9.8-1 2.0-2
00
T=8xI03~K.
7.4-3 8.8-4 2.5-1 3.6-4 6.9-1 1.4-4
3.4-2 8.5-3
9.5-1 3.1-4 9.9-1 5.9-5
9.8-1 2.0-3
9.9-1 5.7-3
9.9-1 7.3-3
9.9-1 7.3-3
9.2-1 3.3--6
8.8-1 5.4-5 9.8-1 9.9--6
1.0 3.8-4
1.0 1.1-3
1.0 1.4-3
1.0 1.4-3
6.8-17
1.7-16
4.1-16
2.2-15
1.6-14
4.5-14
4.5-14
5.1-13
6.1-13
1.2-12
2.5-12
7.6-12
3.7-11
3.8-14 1.7-10
1.0-8
1.0-26,,_
2.2-2
2.4-2 6.8-9
8.6-1 5.7-2
9.4-1 6.3-2
9.4-1 6.3-2
9.3-2
1.0-1 3.2-9
9.7-1 5.8-3
9.8-1 9.9-3
9.9-1 1.1-2
9.9-1 1.1-2
ro(4) n(4)
1.7-1
1.8-1 2.6-9
2.0-1 2.5-7
9.8-1 1.5-3
9.9-1 2.5-3
1.0 2.8-3
1.0 2.8-3
ro(5) rl(5)
2.3-1
2.5-1 2.3-9
2.9-1 2.2-7
T = 1.6 x 104~K. 5.7-2 1.5-1 3.6-2 6.7-5 6.6-4 6.0-3 3.8-1 1.8-1 7.4-1 3.0-5 2.4-4 1.3-3 4.3-1 9.3-1 7.6-1 1.8-5 8.6-5 3.6-4 7.1-1 9.1-1 9.8-1 3.2-5 9.3--6 1.2-4
5.2-1 3.2-2
ro(3) rl(3)
2.6-2 6.8-7 1.1-1 3.2-7
9.9-1 4.9-4
1.0 8.4-4
1.0 9.1-4
1.0 9.1-4
ro(7) rl(7)
3.1-1
3.5-1 1.8-9
4.8-1 1.5-7
9.3-1 2.1--6
9.8-1 5.7--6
1.0 2.1-5
1.0 8.5-5
1.0 1.5-4
1.0 1.6-4
1.0 1.6-4
S
1.3-12
1.4-12
1.5-12
2.4-12
4.2-12
1.2-11
4.3-11
7.2-11
7.8-11
7.8-11
(lIz
2.9-13
3.0-13
3.2-13
4.3-13
6.3-13
3.0-12
7.9-12
3.1-10
3.1-28".
ro(2) rl(2)
1.2-1
1.3-1 5.4-9
6.8-1 2.0-2
9.3-1 3.0-2
9.7-1 3.1-2
9.7-1 3.1-2
ro(3) n(3)
2.5-1
2.6-1 2.6-9
1.3-1 5.4-7 2.7-1 2.5-7
1.2-12 4 = 3.2 x 10 z2K. 1.9-1 3.1-1 4.5-3 5.2-4 5.1-1 8.1-1 1.8-4 8.8-4
9.5-1 2.9-3
9.9-1 4.2-3
1.0 4.4-3
1.0 4.4-3
ro(4) n(4) ro(5) rl(5)
3.3-1
3.5-1 1.9-9 4.1-1 1.7-9
ro(7) rl(7)
4.6-1
5.0-1 1.3-9
S ·z3
2.4-10 1.7-13
2.4-10 1.8-13
'Z3
(lIz
3.9-1
T 1.5-1 5.4-5 3.3-1 2.4-5
6.1-1 2.6-3 8.7-1 8.4-4
3.7-1 1.9-7 4.4-1 1.6-7 5.9-1 1.1-7
5.4-1 1.4-5 7.5-1 7.6--6
8.1-1 6.4-5 9.3-1 2.3-5
9.5-1 2.3-4 9.8-1 7.4-5
9.9-1 6.8-4 1.0 2.2-4
1.0 9.8-4 1.0 3.1-4
1.0 1.0-3 1.0 3.3-4
1.0 1.0-3 1.0 3.3-4
9.4-1 2.0--6
9.9-1 4.1--6
1.0 1.2-5
1.0 3.6-5
1.0 5.1-5
1.0 5.4-5
1.0 5.4-5
2.5-10
3.2-10
4.4-10
8.5-10
2.8-9
2.9-9
2.9-9
1.8-13
1.8-13
2.0-13
2.4-13
2.0-9 3.3-13
5.0-13
2.9-11
2.9-29".
5. Some Problems of Excitation Kinetics
150
Table 5.8. (continued) 1015
1016
10 18
00
5.2-1 3.6--3
7.8-1 1.5-2
9.5-1 2.3-2
9.8-1 2.4-2
9.8-1 2.4-2
6.5-1 1.5--4
8.6--1 7.1--4
9.7-1 2.1-3
9.9-1 2.9-3
1.0 3.1-3
1.0 3.1-3
6.7-1 1.2-5
8.6--1 5.5-5
9.6--1 1.8--4
9.9-1 4.8--4
1.0 6.7--4
1.0 7.0--4
1.0 7.0--4
6.2-1 1.1-7
8.1-1 5.9-6
9.4-1 2.0-5
9.9-1 5.8-5
1.0 1.5--4
1.0 2.1--4
1.0 2.2--4
1.0 2.2--4
6.6--1 9.2-10
7.1-1 7.9-8
9.6--1 1.3-6
9.9-1 3.3-6
1.0 9.7-6
1.0 2.4-5
1.0 3.4-5
1.0 3.5-5
1.0 3.5-5
3.4-9
3.5-9
4.0-9
4.8-9
7.3-9
1.4-8
1.8-8
1.8-8
1.8-8
1.0-13
1.1-13
1.2-13
1.6--13
2.1-13
5.6--12
5.6--30'1e
= 2.56 x
105z2 K.
'1e
0
108
1010
10 12
= 6.4 x
104z2 K.
ro(2) rl(2)
3.1-1
3.5-1 4.5-9
3.6--1 4.5-7
3.8-1 4.4-5
4.2-1 4.3--4
ro(3) rl(3)
4.6--1
4.8-1 2.1-9
4.9-1 2.1-7
5.3-1 1.9-5
ro(4) rl(4)
5.3-1
5.5-1 1.5-9
5.7-1 1.5-7
ro(5) rl(5)
5.7-1
6.0-1 1.2-9
ro(7) rl(7)
6.2-1
s. Z3
3.4-9
1013 T
rx/z
1.0-13
1.0-13
1.0-13
T
10 14
ro(2) n(2)
1.1
1.1 3.5-9
1.1 3.5-7
1.1 3.5-5
1.1 3.4--4
1.1 2.9-8
1.0 1.4-2
9.8-1 2.4-2
9.7-1 2.6--2
9.7-1 2.6--2
ro(3) rl(3) ro(4) rl(4)
1.0
1.0 1.6--9 1.0 1.1-9
1.0 1.6--7 1.0 1.1-7
1.0 1.5-5 1.0 9.2-6
1.0 1.3--4 1.0 5.2-5
1.0 6.7--4 1.0 1.8--4
1.0 2.0-3 1.0 4.5--4
1.0 3.0-3 1.0 6.8--4
1.0 3.2-3 1.0 7.2--4
1.0 3.2-3 1.0 7.2--4
ro(5) rl(5)
9.9-1
1.0 6.0-10
1.0 5.8-8
1.0 3.9-6
1.0 1.8-5
1.0 5.4-5
1.0 1.4--4
1.0 2.1--4
1.0 2.2--4
1.0 2.2--4
ro(7) rl(7)
9.7-1
1.0 4.6--10
1.0 4.1-8
1.0 9.0-7
1.0 3.0-6
1.0 8.5-6
1.0 2.2-5
1.0 3.2-5
1.0 3.2-5
1.0 3.2-5
1.0
section for a neutral atom at the threshold is equal to zero, but, for ions, the threshold value is not zero: see Sect. 3.2). In the range T rv z2Ry, the values of ro, rl from the Tables 5.7 and 5.8 are found to be in reasonable agreement. 5.4.5 Population Densities of Highly Excited Levels at High Density; Steady-Flow Regime The highly excited bound levels with n ~ no are populated and evacuated exclusively by collisions. After an electron has been transferred to a level through three-body recombination it may be either reionized through electron impact, or transferred to another bound level through inelastic or super-elastic (quenching) collision. If n > no, the collisional transition frequency between the bound levels is n2 times larger than the frequency of reionization. The most probable are
5.4 Populations of Excited Levels in a Plasma
151
collisional transitions between adjacent levels, followed by transfer of a small energy amount. The electron wandering between the highly excited levels can be treated as diffusion in the space of quantum numbers which can be described by Focker-Planck equation [5.32-34,44]. Neglecting the radiative processes the electron flux j(n) [cm- 3 s- l ] in the space of quantum numbers can be determined by 00
j(n) =
L:
L:[N(n + k' + l)Wn+k'+I,n-k - N(n - k)Wn-k,n+k,+d, (5.4.24)
k'~Ok~O
the first term in the square brackets representing the electron flux via n directed to the ground state, the second term representing the flux directed to the continuum. Using the ratio N(n)/NE(n) = b(n) which shows the departure of the level population from the Saba-Boltzmann population density, (5.4.24) may be rewritten in the form
j(n) = N(Z+I)-S2 L:[(n + k' k,k'
+ 1iexp (En+k,+dT)b(n + k' + l)Wn+k'+I,n-k
-(n - kiexp (En-k/T) b(n - k)Wn-k,n+k,+d ,
(5.4.25)
where S = z383/2/4n3/2aijNe, 8 = T/z 2Ry. Assuming b(n + k) = b(n) + kob/on, retaining the terms of the order and neglecting the weak functions of n, one can obtain from (5.4.25)
j(n) =
N(Z+I)Ne~exp
(ETn)
~b n2 L: k 2 (vun,n+k)
un
Ikl~1
.
rv
k 2,
(5.4.26)
In n ~ 1 the sum with respect to k in (5.4.26) may be extended to infinity. Let the basic dependence of (VUn,n+k) on temperature and the numbers n and k, which determine the rate coefficient order of magnitude, be written in explicit form (Sect. 3.5) 2
2
4
2 e nao -1/2n (VUn,n+k ) -_ .jn'h--;'38 k 3 cp(n, k, 8) ,
(5.4.27)
where cp(n, k, 8) is a weak function of its arguments. It is convenient to introduce the continuous variable e = 1/n2. Using (5.4.27) we can write the formula for the flux as
'() __ N(Z+I)N232n2e2 58-2-3/2 (~)LOb ] e e z6 Ii, ao e exp 8 oe'
(5428) . .
The factor L = L:k k-1qJ(n = e- I/2 , k,8) is a weak function of e and 8. (In reference [5.20] it is estimated to be ~ 0.2). Using the variable e the diffusion equation can be written
2e3/2 d~~) = q(e) - N(e)fB .
(5.4.29)
Here q(e) [cm- 3 s-I] is the rate for the direct population of the level e, and
152
5. Some Problems of Excitation Kinetics
f e[s -I]
is the total frequency of electron transfer to the continuum and to the lower levels n' with n' < no. The collisional transfer to the highly excited levels is already taken into account in the expressions (5.4.26,28) for the electron flux j(e) and should be excluded from fe. In order to obtain b(e) and j(e), the equation (5.4.29) should be supplemented with appropriate boundary conditions. The boundary condition at I'. = 0 is found easily. In the limit of I'. ~ 0 (n ~ 00), the function b( e) should correspond to the continuum distribution. Wlien Maxwellian velocity distribution is valid, limb(e)
e..... O
=
I .
(5.4.30)
The second boundary condition in general must be chosen by fitting the solution of (5.4.29) to the solution of the set of rate equations (5.4.10) for lower levels where the discrete structure and radiative transitions are of importance. In some cases it is possible to obtain the explicit form of this boundary condition. Somewhat later we shall consider low-temperature recombining plasmas when the condition of total absorption at some value 1'.1 can be treated as the second boundary condition. Without any particular pumping or evacuation of the highly excited levels, q( e) is equal to the rate of three-body recombination to the levell'., and f B is the probability of the inverse process, ionization by electron impact. Assuming the departure of b(e) from the Saha-Boltzmann equilibrium value (equal to unity) to be small, the right-hand part of (5.4.29) may be put equal to zero, because q(e) ~ N(e)fe due to detailed balance. Thus we obtain the constant-flow approximation j(e)
= const. = j
Then solving the equation (5.4.28) together with the boundary condition (5.4.30) yields the relationship b(e)
=
z 6Le 2 e I - j N(Z+llNic[(e')3/2 exp
(
-
1'.') e
de'
(5.4.31)
C = 32n2 aije2 jh .
If
e~e
. z 6Le2
b(e) ~ 1- ] N(z+I>N2Ce
5/2
(5.4.32)
e
The flux value should be determined using the second boundary condition. Now we shall consider low-temperature recombining plasmas. The flux j( e) is positive definite, and b( e) decreases with e. As the second boundary condition for equation (5.4.29), one can use the condition of total absorption of the flux at some value 1'.1, b(eJ)
=0
.
(5.4.33)
5.4 Populations of Excited Levels in a Plasma
153
If we deal only with low temperature e ~ 81, the value of j determined from (5.4.31) and (5.4.33) does not depend on 8t, and the integration with respect to 8' may be extended to infinity. Thus j = N(z+I)Ne a. ,
(5.4.34)
where
N. 27
3/2
2
a. = ~ _7t_ ~a~e-9/2 z6 3 Ii. =
N ez3
4V27t3/ 2 e 10 3 ml/2T9/2L
(5.4.35)
is the recombination coefficient. The order of magnitude and the dependence of the coefficient a. on temperature appear to be in agreement with the results of numerical calculations by Johnson and Hinnov, and Bates et al. given in Tables 5.7 and 5.8.
6 Tables and Formulas for the Estimation of Effective Cross Sections
In this chapter, tables of cross sections and rate coefficients of excitation and
ionization by electron impact and rate coefficients of dielectronic recombination are given. The cross sections and rate coefficients are presented in the form of products of angular and radial factors, the latter being expressed in analytical form containing two or three adjusted parameters. The tabulated parameters are obtained from the results of numerical calculations. The first section contains a description of the contents of the tables and relevant fitting formulas. In the second and third sectins of the chapter the formulas for angular factors are given which are necessary for applying the tables.
6.1 6.1.1
Tables of Numerical Results Methods of Calculations and Survey of the Tables
In this section the results of numerical calculations for the cross sections a, collision rate coefficients (va), and dielectronic recombination rate coefficient /Cd are given. The calculations are made using the Born method (see Sects. 2.3 and 3.1) and its modifications which are described in Sect. 3.2. The atomic wave functions are assumed to be constructed from single electron wave functions in accordance with a specific scheme of angular momenta coupling. A singleconfiguration approximation is used. The radial wave functions for all levels of a given electronic configuration are assumed to be the same. Under these assumptions the cross sections may be expressed in the form (2.3.4,8). In this chapter, however, we use the formulas somewhat different from (2.3.8). For the excitation cross sections of the transitions ao ---+ al we write in the general case a(ao,
ad = a'(ao, ad + a"(ao, ad = I: Q~(ao,ada~(lo, Id K
+ I: Q~(ao,ada~(lo, Id
(6.1.1 )
K
where a' consists of the direct plus interference terms, and a" is the purely exchange contribution to the cross section (Sects. 2.3,3.1,2). A summary of formulas for the Q-factors is given in Sect. 6.2. In order to simplify the use of the tables given below the subsequent subsections comprise the specific formulas for analytical approximation and Q-factors which can be used for specific tables. The exchange cross sections are given either summed over /C or for those cases in which index /C has a single value. Therefore, in most cases the exchange
I. I. Sobel'man et al., Excitation of Atoms and Broadening of Spectral Lines © Springer-Verlag Berlin Heidelberg 1995
6.1 Tables of Numerical Results
155
cross sections can be determined only for transitions between the atomic terms as a whole, so (6.1.2) where index K is not included, and a"(lo, 1\) = ~Ka~(lo, 1\). The calculated quantities a~, a~ have been approximated by means of simple analytic formulas which contain the two or three fitting parameters: C, cp, D for a and A, X, D for (va). The fitting parameters have been found from the results of numerical calculations by the method of least squares. The errors of analytic approximation R are also given in the tables. We pass on to a brief description of the tables and of the approximate methods which have been used for calculations. The Born approximation with normalization has been used for calculation of the cross sections for hydrogen atom summed over 10 and 1\ (Table 6.1). Tables 6.2 and 6.3 contain the fitting parameters for cross sections and rate coefficients calculated in the Born approximation with the Bates-Damgaard approximation for the atomic wave functions. The Bates-Damgaard approximation used for calculations of Tables 6.2 and 6.3 is most valid in cases when the maxima of both radial functions lie outside the atomic core. This condition is usually formulated explicitly as
no = no
Vz2Ryi lEo I >
ni
> nc ,
10 + 1/2,
nr = Vz 2Ry/lEd > 1\ + 1/2,
(6.1.3) (6.1.4)
> nc ,
where nc is the largest of the principal quantum numbers of the electrons of the atomic core. The condition (6.1.4) is sometimes stricter than (6.1.3). However, in many cases when conditions (6.1.3) are fulfilled, but (6.1.4) are not fulfilled, the error does not exceed the factor of 2. Such errors are inherent in the Born method itself. The excitation cross sections for specific atoms and ions (Tables 6.1,4-10), have been normalized with the use of the K matrix. For calculation of radial BOO
t 600 N<§'400
-!:: b
200
o
....
3d-4f
- .J
'
I
I I,
Y
1
2
.........
,
r----,_
-
---- -eV
B
Fig. 6.1. Effective excitation cross section for the transition 3d-4f of the H atom: (1) Normalized cross section; (2) Born approximation
156
6. Tables and Formulas for the Estimation of Effective Cross Sections
integrals, the semiempirical numerical wave functions [6.1] have been used. These functions provide considerably better accuracy in all cases, especially for transitions from the shells of equivalent electrons, than the Bates-Damgaard radial functions. In the case of neutral atoms, the normalized Born cross sections are tabulated for transitions without spin change. For intercombination transitions the method of orthogonalized functions (Sect. 3.2) with normalization has been used. In case of ions for transitions with no change of spin the normalized CoulombBorn cross sections have been calculated for Table 6.4. The Coulomb-Bomexchange method (Sect. 3.2) has been used for the cross sections tabulated in Tables 6.5-10. The exchange interaction has been taken into account within the framework of the method of orthogonalized functions. The ionization cross sections have been calculated in the Coulomb-Born approximation. We shall give a brief description of corrections to the Born approximation which are induced by treating the Coulomb attraction and the exchange interaction, and by normalization of the cross sections. The difference between the Born and Coulomb-Born cross sections is great only near the threshold 8::6 11E, T::6 11E; see Figs. 3.5, 6.2, 6.3. The treatment of exchange affects the value of the cross section for transitions with no change of spin also not far from the threshold (see Fig. 3.6). Therefore the treatment of exchange and Coulomb attraction are necessary for the cross sections of excitation from the ground state of ions. In the LS-coupling approximation, the intercombination-transition excitation is solely due to exchange. The effect of normalization upon the cross sections of excitation from the ground state is not substantial.
2s 3p
z=lO
30r-=:::::::::~~:;"';';;'_J------I-'~-~---H
~C>
t>
~
~~10~------~----~~------~~----~ Bom opproximotion
A,
O~----~~----~-------L------~
10-2
10-1
1
10
102
u=(lo-M)/M-
Fig. 6.2. Effective cross section for the transition 23-3 p of the hydrogen and hydrogenlike ions. (- • - • -) Born approximation. The effect of nonnalization is very small even for neutral hydrogen
6.1 Tables of Numerical Results
157
2s-3p
1 10 TlIlE=l/P_
Fig. 6.3. Excitation rate coefficient (vu) for the transition 2s-3 p of the hydrogen and
hydrogenlike ions
For transitions between the excited levels of neutral atoms, first order perturbation theory can give considerably overestimated results at low energies 8 < Ry (Figs. 3.7, 6.1). Normalization removes this deficiency. In the case of multiply charged ions, the matrix element of interaction of the outer electron with the bound one is z times smaller than the interaction of the bound electron with the atomic core. In Coulomb units, this matrix element is proportional to the parameter 1/z. Therefore at z ~ I (actually at z > 3) the normalization effect is negligible even for transitions between closely spaced levels. The Coulomb attraction for such transitions is also not important. Hence when 8 > AE, T > AE, the Born cross sections may be used for multiply charged ions. In cases not covered by the tables which are given in this section, one can use the semiempirical formulas given in Sect. 5.1. 6.1.2
Excitation Cross Sections for Neutral Hydrogen. Transitions no - nl (Table 6.1)
The tabulated cross sections are the sums of normalized Born cross sections for nolo - t nlll transitions. They are fitted by means of the following formula
1ta~ (no i
C 4)'(u) ,
(1
=
U
= (c - AE)/Ry .
nl) n~ U + qJ
(6.1.5)
The rate coefficients are given by A G'(P) exp(-pP) [cm3 /s], (V(1) = 10- 8 ( -no) 2-pnl no + X
P=
Ry/T,
p
= AE/Ry.
(6.1.6)
158
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.1. Normalized Born cross sections for neutral hydrogen Transition
C
qJ
D
R
A
3.26 2.70 2.58 2.53 2.50
0.00 0.00 0.00 0.00 0.00
0.07 0.08 0.08 0.08 0.08
X
D
R
0.26 0.38 0.42 0.44 0.45
0.00 0.00 0.00 0.00 0.00
0.01 0.01 0.02 0.02 0.02
no-nl
1-2 1-3 1-4 1-5 1-6
68.28 39.61 33.62 31.27 30.10
32.17 25.66 23.82 23.03 22.61
2-3 2-4 2-5 2-6
1275.0 454.0 318.0 268.0
1.23 0.62 0.53 0.50
0.00 0.00 0.00 0.00
0.10 0.16 0.16 0.15
332.0 316.0 281.0 264.0
0.70 0.59 0.52 0.43
3.80 0.80 0.30 0.00
0.02 0.02 0.02 0.02
3-4 3-5 3-6
8928.0 2298.0 1435.0
0.88 0.08 0.09
0.00 0.70 0.60
0.08 0.17 0.14
1437.0 1337.0 1202.0
0.96 1.19 1.02
9.90 3.30 1.60
0.02 0.02 0.01
4-5 4-6
35494.0 8492.0
0.19 0.06
0.70 0.70
0.13 0.12
7505.0 4201.0
1.14 1.59
9.90 5.50
0.04 0.02
5-6
118366.0
0.42
0.00
0.19
30951.0
1.49
9.90
0.04
The formulas for 1P'(u) and G'(P) are expressed by (5.1.12, 13 and 16). The set of parameters C, qJ, D is adjusted for the range 0.02 < u < 16, and the set A, X, D for 0.25 < P < 8. For the transitions no -+ no + 1 with no > 5 the quasiclassical cross sections given in Tables 3.3 and 3.4 may be used. 6.1.3 Born Cross Sections Calculated in the Bates--Damgaard Approximation for Atomic Wave Functions (Tables 6.2, 6.3) The cross sections for transitions with no change of spin of the atom, L1S = 0, are tabulated in a form analogous to the tables of oscillator strengths in BatesDamgaard approximation given in [6.2]. The quantities a and (va) are expressed in the form 2 (
a(ao,ad = 7tao
/2
Ry ) ( E ll, ) Eo 2/0 + 1 ~ Q,,(ao,ad 1P,,(u), u
L1E
=
If - L1E
L1E
'
(6.1.7)
(va(ao, ad) = 10
-8
(RY i/2 (EI i/2 exp( -P) , L1E) Eo) 2/ + 1 ~ Q,,(ao, ad
xG,,(P) [cm3 s- l ]
,,= 110 -
0
,p = L1E/T
111, 1/0 -/11 + 2,···1/0 + 111 .
(6.1.8)
6.1 Tables of Numerical Results
159
Table 6.2. Transitions with no change of spin AS = 0; Born cross sections in the Bates-Damgaard approximation for atomic wave functions. Asterisks indicate cases where the errors exceed 10%. Parameters C and q>. The effective principal quantum number An
0.5
1.0
1.5
2.0 Transition s - s, parameter C. a )
0.6 0.7 0.8 0.9 1.0
67 + 1 72+ I 69+ 1 58 + 1 42+ 1
55 + 1 55 + 1 49+ 1 39+ 1 26+ 1
57 + 55 + 48 + 37 + 25 +
1.1
16 + 1 67+0 60+0* 13 + 1* 27 + 1 41 + 1 52+ 1 57 + 1 54+ 1 43 + 1
15 + 1 81 +0 65 +0* 10+ 1 17 + 1 25 + 1 30+ 1 31 + 1 28 + 1 21 + 1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 4.1 4.2 4.3 4.4
1 1 1 1 1
14+ 1 84+0 68+0 97+0 15 + 1 21 + 1 25+ 1 26+ 1 23 + 1 18 + 1 15 + 1 13 + 1 11 + I 71 +0 78+0 73+0 57 +0* 60+0* 58+0 12 + i* 84+0 75+0 24+ 1 14 + 1 11 + 1 38 + 1 20+ 1 16+ 1 50+ 1 26+ 1 20+ 1 55 + 1 27 + 1 21 + 1 54+ 1 25 + 1 20+ 1 45 + 1 19 + 1 16 + 1 15 + 1 12 + 1 10+ 1 72+0 76+0 69+0 56+0* 58 +0* 54+0 11 + 1* 79+0 68+0 23 + 1 13 + 1 10 + 1 37 + 1 19 + 1 14 + 1 49 + 1 24+ 1 18 + 1 55 + 1 26+ 1 19+ 1 54+ 1 24+ 1 18 + 1 46+ 1 19 + 1 15 + 1 15 + 1 12 + 1 10+ 1 72+0 76+0 66+0 56+0* 57 +0* 52+0 11 + 1* 76+0 65+0
61 + 57 + 49+ 37 + 24+
no
2.5 I I 1 1 1
66+ 61 + 51 + 38 + 25 +
3.0 1 1 1 1 1
14 + 1 85 +0 69+0 94+0 14 + 1 19 + 1 22 + 1 22 + 1 20+ 1 15 + 1
15 + 1 87+0 70+0 93 +0 13 + 1 18 + 1 21 + 1 21 + 1 18 + 1 14 + 1
10 + 1 68+0 54+0 68+0 10 + 1 13 + 1 16 + 1 17 + 1 16 + 1 12 + 1
99+0 64+0 52+0 63+0 91 +0 12 + 1 14 + 1 15 + 1 14 + 1 11 + 1
91 +0 61 +0 49 -0 59+0 87 +0 12 + 1 14 + 1 15 + 1 14 + 1 11 + 1 84+0 57+0 46 -0 55 +0
82+0 55 +0 45 -0 53 +0 76+0 10 + 1 12 + 1 13 + 1 12 + 1 10+ 1 74+0 51 + 0 42 -0 48 -0
71 + 65 + 54+ 40+ 26+
4.0
3.5 1 1 1 1 1
77+ 69+ 57+ 42+ 27+
1 I 1 1 1
15 + 1 90+0 72+0 94+0 13 + 1 18 + 1 20+ 1 20+ 1 18 + 1 13 + 1 95+0 63 +0 50+0 60+0 86+0 11 + 1 13 + 1 14 + 1 13 + 1 10 + 1
16+ 1 94+0 75+0 96+0 13 + 1 18 + 1 20+ 1 20+ 1 17 + 1 13 + 1 93+0 62+0 49-0 58+0 82+0 11 + 1 13 + 1 13 + 1 12 + 1 10+ 1
76+0 52+0 42 -0 49-0 69+0 93+0 11 + 1 11 + 1 11 + 1 91 +0
72+0 49-0 40-0 46-0 64+0 86+0 10+ 1 11 + 1 10+ 1 84+0 62+0 43 -0 35 - 0 40-0
67+0 47 -0 38 -0 44-0
83 + 1 74+ 1 60+ 1 44+ 1 28 + 1 16 + 1* 97+0 77+0 98+0 14 + 1 18 + 1 20+ 1 20+ 1 17 + 1 13 + 1 93 +0* 61 +0 49-0 58+0 80+0 10 + 1 12 + 1 13 + 1 12 + 1 96+0 69+0* 48-0 39 -0 44-0 61 +0 81 +0 98+0 10 + 1 96+0 79+0 58 +0* 41-0 ·33 - 0 38 -0
4.5
5.0
89+ 1 79+ 1 64+ 1 46+ 1 30 + 1 17 + 1* 10 + 1* 80+0 10 + 1 14 + 1 18 + 1 20+ 1 20+ 1 17 + 1 13 + 1 93 +0* 61 + 0* 49-0 57+0 79+0 10+ 1 12 + 1 12 + 1 11 + 1 94+0 67 +0* 47 -0* 38-0 43 -0 59+0 78+0 93 +0 98+0 92+0 75 +0 55 + 0* 39 - 0* 32 -0 36-0
95 + 1 84+ 1 67+ 1 49+ 1 31 + 1 18 + 1* 10+ 1 83+0 10+ 1 14 + 1 18 + 1 21 + 1 20+ 1 18 + 1 13 + 1 94+0* 62+0* 49-0 57+0 79+0 10+ 1 12 + 1 12 + 1 11 + 1 92+0* 66+0* 46+0* 37 -0 42-0 57+0 76+0 90+0 95+0 88+0 72+0* 54+0* 38 - 0* 31- 0* 35 - 0
This table can be applied to transitions between the levels of two different electronic configurations ns-n's with no change of any of the angular quantum numbers
a)
160
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number no Lin
0.5
0.6 0.7 0.8 0.9 1.0
92+0 88+0 85 +0 84+0 84+0
80+0 78+0 78+0 81 + 0 89+0
76+0 78+0 81 +0 89+0 10 + 1
1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
10 + 1 15 + 1 15 + I" 10 + 1 78+0 70+0 68+0 69+0 72+0 81 + 0
12 + 1 15 + 1 12 + 1 77+0 62+0 60+0 62+0 68+0 76+0 89+0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
93 +0 15 + 1 20 + I" 13 + I" 10 + 1 91 +0 85 +0 82+0 81 + 0 81 +0 89+0 13 + 1 20 + I" 13 + I· 10+ 1 91 +0 85 +0 82+0 81 + 0 81 + 0
99+0 13 + 1 15 + I" 10 + 1 78+0 68+0 66+0 67+0 70+0 78+0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
88+0 13 + 1 20 + I· 13 + I· 10 + 1 91 +0 85+0 82+0 81 + 0 81 + 0
4.1 4.2 4.3 4.4
88+0 13 + 1 20 + I· 14 + I'
1.0
1.5
2.5
3.0
3.5
78 +0 82 +0 89+0 10 + 1 11 + 1
81 + 0 88 + 0 97+0 11 + 1 13 + 1
86+0 94+0 10 + 1 12 + 1 15 + 1
91 + 10 + 11 + 13 + 17 +
16 + 1 18 + 1 12 + 1 67 +0 55 +0 57 +0 65 +0 75 +0 90+0 11 + 1
19 + 1 20 + 1 12 + 1 66+0 53 +0 57 +0 67+0 80+0 98+0 12 + 1
11 + 1 13 + 1 12 + 1 81 + 0 61 +0 57+0 59+0 65 +0 73+0 85 +0
14 + 1 16 + 1 11 + 1 69+0 56+0 57 +0 63 +0 71 + 0 83 +0 10+ 1 12 + 1 14 + 1 12 + 1 74+0 56+0 55 +0 59+0 67 +0 78+0 95 +0
14 + 1 16 + 1 12 + 1 74+0 55 +0 54+0 60+0 70+0 84+0 10 + 1
15 + 1 18 + 1 13 + 1 74+0 53 +0 53 +0 61 +0 73 +0 90+0 11 + 1
21 + 1 23 + 1 13 + 1 64+0 52+0 58+0 69+0 85+0 10 + 1 13 + 1 17 + 1 20+ 1 14 + 1 73 +0 52+0 53+0 63 +0 77+0 97+0 12 + 1
96+0 13 + 1 15 + I· 10 + 1 78+0 68+0 65+0 66+0 69+0 78+0
10+ 1 13 + 1 12 + 1 82+0 61 + 0 56+0 58+0 63+0 71 +0 84+0
11 + 1 14 + 1 12 + 1 76+0 57 +0 54+0 58+0 65 +0 76+0 92+0
13 + 1 15 + 1 12 + 1 77+0 55 +0 53 + 0 58+0 68+0 81 + 0 10 + 1
14 + 1 17 + 1 13 + 1 77+0 54+0 52+0 59+0 70+0 87+0 11 + 1
16+ 1 18 + 1 14 + 1 77+0 53+0 52+0 60+0 73+0 93 +0 11 + 1
95 +0 13 + 1 15 + I" 10 + 1
10 + 1 12 + 1 12 + 1 82+0
11 + 1 13 + 1 12 + 1 77+0
12 + 1 15 + 1 12 + 1 79+0
14 + 1 16 + 1 13 + 1 79+0
15 + 1 18 + 1 14 + 1 79+0
Transition s - s, parameter
2.0
4.0
4.5
96+0 10 + 1 12 + 1 15 + 1 18 + 1
10 + 11 + 13 + 16 + 20+
5.0
qJ
0 1 1 1 1
1 1 1 1 1
24 + I· 26 + I" 25 + 1 27 + I" 13 + 1 14 + 1 64+0 63 +0 52+0 52+0 59+0 60+0 72+0 75 +0 90+0 96+0 11 + 1 12 + 1 15 + 1 16 + 1 19 + I" 21 + I" 21 + 1 23 + I" 15 + 1 15 + 1 73 +0 73 +0 51 + 0 51 + 0 53 +0 54+0 64+0 67+0 81 + 0 86+0 10+ 1 11 + 1 13 + 1 14 + 1 17 + I" 19 + I" 20 + 1 22 + I" 15 + 1 15 + 1 78+0 78 + 0 52+0 52+0 52+0 52+0 61 +0 63 +0 77+0 81 + 0 99+0 10 + 1 13 + 1 14 + 1 16 + I· 18 + I· 19 + 1 21 + I· 15 + 1 15 + 1 80+0 81 + 0
10 + 12 + 14 + 17 + 22+
1 1 1 1 1
29 + I· 30+ I" 14 + 1 62+0 52+0 62+0 79+0 10 + 1 13 + 1 17 + 1 23 + I" 25 + I· 16 + 1 73 +0 51 + 0 55+0 69+0 90+0 12 + 1 16 + I· 21 + I" 24+ I" 16 + 1 79+0 52+0 53+0 65+0 85+0 11 + 1 15 + I· 19 + I· 22 + I' 16 + 1 82+0
161
6.1 Tables of Numerical Results Table 6.2. (continued) The effective principal quantum number no Lin
0.5
1.0
1.5
2.0
2.5
3.0
3.5
4.0
4.5
5.0
Transition s - p, parameter C 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
11 +2 14+2 15 + 2 15 +2 13 +2
II + 1 27 + 1 49 + 1 73 + 1 96+ 1 11 +2 11 +2 11 +2 93 + I 69 + 1
16 + 1 37 + 1 59 + 1 80 + 1 97 + 1 10 + 2 10+2 94 + 1 75 + 1 52 + l'
21 + 1 44 + 1 67 + 1 86 + 1 10+2 10+2 98 + 1 84 + 1 63 + I" 41 + l'
25 + 1 50+ 1 73 + 1 92 + 1 10 +2 10+2 96+ 1 80 + l' 59 + l' 37 + I"
29+ 1 56 + 1 80+ 1 98 + 1 10+2 10+2 95 + 1 77 + l' 55 + I" 34 + I"
32 + 1 61 + 1 86 + 1 10+2 11 +2 10+2 96+ l' 77 + l' 54 + I' 32 + l'
36 + 1 67 + 1 92 + 1 10+2 11 +2 11 +2 97 + l' 77 + l' 53 + I' 31 + l'
39 + 1 72 + 1 98 + 1 II +2 12 +2 11 +2 99 + l' 77 + l' 53 + I" 31 + l'
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
30+2 25 +2 18 + 2 10+2 51 + 1 14 + 1 10- 0 76+0 26+ 1 48 + 1
10+2 61 + 1 27 + 1 71 +0 53 + O' 19 + I" 42+ 1 68 + 1 87 + 1 95 + I
46 + 1 23 + 1 74+0" 43 -0 11 + 1 24+ 1 38 + 1 47 + 1 49 + 1 44+ 1
30 + l' 12 + 1 42 -0 55 + O' 13 + l' 24+ 1 34 + 1 39 + 1 38 + 1 31 + 1
22 + I" 86 +0" 37 - 0 63 + 0" 13 + I" 22 + 1 29 + 1 32 + 1 29 + 1 23 + l'
19 + 1 68 +0" 37 - 0 70+ 0" 14 + l' 21 + 1 27 + 1 29 + 1 26 + l' 20 + l'
16 + 58 + 38 75 + 14 + 21 + 25 + 26 + 23 + l7 +
1 O' 0" O' l' 1 1 l' l' I'
15 + l' 53 + 0" 40 - 0" 80+0' 14 + l' 21 + l' 25 + l' 25 + I' 21 + l' 15 + I"
14 + l' 50 +0" 43 - 0" 84 +0' 14 + I" 20 + I" 24 + l' 24 + l' 20 + I' 14 + I"
13 + I" 48 - 0" 45 - 0" 88 +0" 15 + l' 21 + l' 24 + l' 23 + I" 19 + l' 13 + I"
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
19+2 18 + 2 14+2 10+2 54 + 1 20 + 1 31 - 0 28 -0 15 + I 33 + I
80 + 1 55 + 1 29+ I 10 + 1 37 -0 11 + 1 30 + 1 52 + I 73 + 1 84+ 1
36 + 1 21 + 1 87+0 34-0 72+0 16 + l' 27 + 1 36 + 1 40 + 1 37 + 1
21 + l' 11 + 1 42 -0 34 - O· 77 +0 15 + 1 23 + 1 29 + 1 30 + 1 26+ I
15 + I" 74+0 30 - O· 35 - O· 77 + O· 13 + 1 19 + 1 22 + 1 22 + 1 18 + I"
12 + 1 55 + O' 26 -0 37 - O· 76+0' 12 + I l7 + 1 19 + 1 18 + l' 15 + l'
10 + 1 45 - O· 24-0 38 - O· 75 + 0" 12 + l' 15 + 1 17 + l' 16 + l' 12 + I"
91 +0 39 - 0" 24-0 39-0 74+0' II + l' 14 + l' 16 + I" 14 + I' 11 + l'
82+0 35 - 0" 24-0 40 -0 74 +0' 11 + l' 14 + l' 14 + I" 13 + I' 10 + I"
75 +0 32 - O· 24- 0 41 - 0 74+0' 11 + I" 13 + I" 14 + l' 12 + l' 93 +0'
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
16+2 16 +2 13 +2 96 + 1 55 + 1 32 + I 46-0 16 - O· 11 + 1 27 + 1
73 + 1 53 + 1 30 + I 11 + 1 35 - 0 93 +0 25 + 1 47 + 1 67 + 1 80+ 1
32 + 1 20 + 1 90+0 34-0 59+0 13 + l' 23 + 1 32 + 1 36 + 1 34 + 1
18 + l' 10 + I 41 - O· 28 - O· 62+0 12 + I" 20+ 1 25 + 1 26 + I 23 + 1
12 + I" 67+0 28 -0 28 - O· 59 + O· 10 + l' 15 + 1 18 + 1 18 + l' 15 + l'
10 + 1 49 - 0" 23 -0 28 - 0" 57 +0' 99 +0' 13 + 1 16 + 1 15 + I" 13 + I"
81 + O· 39 - O· 20-0 28 - O· 55 +0" 90+0' 12 + 1 13 + I 13 + I' 10 + I·
70+0' 32 - 0" 19 - 0 27 - O· 53 + 0" 85 +0' 11 + I 12 + I" 11 + l' 93 +0·
61 +0 28 - O· 18 - 0 27 - O· 51 + O· 80+0· 10 + 1 11 + l' 10 + 1· 81 +0'
55+0 25 - O· l7 -0 28 - O· 50+0' 77 +0' 98+0 10 + I" 97 +0· 74+0·
4.1 4.2 4.3 4.4
15 + 2 15 + 2 13 +2 94+ 1
71 + 52 + 30 + 11 +
31 + 1 17 + 1 20+ 1 99+0 92+0 41 - O· 34- 0 26 - O·
11 + I" 62+0 27.-0 25 -0
89+0 45 - O· 21 - 0 24 - O·
71 +0 35 - 0" 18 - 0 23 - O·
59+0 29 - 0" 16- 0 22 - O·
51 + 25 15 22 -
46-0 22 - O· 14 - 0 22 - O·
1.1
1 1 1 1
0 O· 0 O·
162
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number no Lin
0.5
1.0
1.5
2.0
Transition s - p, parameter 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
2.5
3.0
3.5
4.0
4.5
5.0
qJ
22+ 1 25 + 1 28+ 1 32+ 1 37 + 1
lO+ 1 14 + 1 17 + 1 21 + 1 25 + 1 29+ 1 34+ 1 40+ 1 47 + 1 58 + 1
11 + 1 16 + 1 21 + 1 25 + 1 30+ 1 36+ 1 42+ 1 50 + 1 61 + 1 75 + 1*
12 + 18 + 24+ 29+ 36 + 43 + 51 + 62 + 76 + 93 +
1 1 1 1 1 1 1 1 1* 1-
13 + 1 20 + 1 27 + 1 34+ 1 41 + 1 49+ 1 60+ 1 73 + 1* 89 + 111+2*
15 + 1 22 + 1 30+ 1 38 + 1 46+ 1 56+ 1 68 + 1 84 + 1* 10+2* 12 +2*
16+ 1 24+ 1 33 + 1 42+ 1 52+ 1 63 + 1 77 + 194+ 111 +2* 14+2*
17 + 1 26+ 1 36+ 1 46+ 1 57 + 1 70+ 1 85 + l' lO+212+2* 15 + 2*
1.4 1.5 1.6 1.7 1.8 1.9 2.0
26+ 1 29+ 1 33 + 1 38 + 1 47 + 1 70+ 1 57+0 45 -0 16 + 1 23 + 1
44+ 1 56 + 1 73 + 1 37 + 1 10- 015 - 0* 10 + 1 17 + 1 23 + 1 29+ 1
70+ 1 85 + 1 38 + 1* 10-0 10-0 74+0 16 + 1 25 + 1 34+ 1 45 + 1
II +2* 61 + 1* lO-O lO - 0* 37 - 0* 14 + 1 26+ 1 38 + 1 53 + 1 69 + 1*
12 +2 40 + 110-0 10 - 0* 59+018 + 1 31 + 1 45 + 1 62 + 1* 81 + 1*
12+2 27 + 1* 10 -0* 10 - 0* 79+0* 21 + 1 40 + 1* 52 + 1* 71 + 1* 92 + 1*
13 +2* 19 + 110-010 - 098+024+ 1* 40+ 1* 58 + 1* 79+ 1* 10+2*
12 +2* 14+ 1* lO-O* lO-O* 11 + 127 + 1* 45 + 1* 65 + 1* 88 + 1* 11 + 2*
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
24+ 1 28 + 1 32+ 1 57 + 1 46+ 1 63 + 1 73 + 1 lO-O 11 + 1 20+ 1
37 + 1 48 + 1 64+ 1 59+ 1 10 - 0 10 - 0 69+0 14 + 1 21 + 1 27 + 1
86 + 1* 68 + 1* 44 -0* 10 - 0 10 - O' 91 +0 20+ 1 32 + 1 46+ 1 62 + 1*
lO+2 19 + 1* 10 - 0 10-0 63 -0* 21 + 1* 38 + I' 59 + I' 82 + I' 10 + 2*
35 + 1 46+ 1 61 + 1 63 + 1 10-0 10-0 54+0 13 + 1 27 + 1 27 + 1
78 + I' 67 + 1 80+0 10 - O' lO -0* 69 +0* 17 + 1 29+ 1 42 + 1* 58 + 1*
10+2 39 + I' 10-0 10 - O· 23 - O· 14 + I' 27 + 1 43 + I' 61 + 1* 80 + I' 92 + 1* 44 + I' 10-0 10 - 0* 10-0* 11 + 1* 24+ 1 39+ 1 56 + I' 74 + I'
lO+2 23 + 1* lO-O lO-O 50 - O· 18 + I' 35 + 1* 53 + 1* 75 + 1* 97 + 1*
23 + 1 27 + 1 32 + 1 37 + 1 45 + 1 61 + 1 88+ 1 10 - O' 91 + O· 19 + 1
96+ 1 53 + 1* 10-0 10 -0' 10 -0* 11 + 1 23 + 1 37 + 1 53 + I' 7l + I' 86 + 1* 56 + 1* 21 - 0 10 - 0* 10 - O' 90+0' 20 + 1 34+ 1 49 + 1* 66 + 1*
10+2 30 + 1* 10-0 lO-O 37 - 0* 16 + 1* 31 + 1* 48 + I' 68 + 1* 89 + 1*
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
23 + 27 + 31 + 37 +
34+ 45 + 60+ 64+
63 + 71 + 25 + 10 -
73 + I' 66+ 1 10+ 1 10-0
81 + 1 56 + I' 70-0 10 -0*
87 + 1 45 + I' 10-0 10 - O'
96+ 1 n + I' 10-0 10 - 0* 24-0* 15 + 1* 30+ 1 48 + 1* 68 + 1* 89+ I' 90+ 1 91 + 1* 36 + I' 29 + 1* lO-O 10-0 10 - O' lO-O*
95 + 1 22 + 1* 10- 0 10- 0* 35 - 0* 17 + 1* 33 + 1 52 + 1* 74+ 1* 96 + 1*
4.1 4.2 4.3 4.4
56 + 1 71 + 1 56+ 1 10 -0 lO-O 33 - 0* 12 + 1 21 + 1 30+ 1 41 + 1 52 + 1 67 + 1 59 + 1 10-0 10-0 18 - 0* lO+ 1 19 + 1 28 + 1 38 + 1 57 + 1 65 + 1 61 + 1 20-0
93 + I84+ 1 49-0 10 -0* 13 - 0* 11 + 1 21 + 1 31 + 1 43 + 1 57 + 1 73 + 1* 78 + 1 17 + 1 10 - O' 10-0 67+0 16 + 1 26+ 1 38 + 1 51 + 1 67 + 1* 74+ 1 23 + 1* 10 - 0* lO-O 49 -0* 14 + 1 24+ 1 35 + 1 48 + 1
18 + 1 28+ 1 39 + 1 50+ 1 62 + 1 76+ 1 94+ 111 + 2* 14 + 2* 17 +2* 11 +2* 10 + 1* lO - 0* 10 - 0* 13 + 1* 30 + 1* 50 + 1* 71 + 1* 96 + 1* 12 +2*
1.1
1.2 1.3
1 1 1 1
1 1 1 1
1 1 1* 0*
95 + 1 34 + 1* lO-O lO- 0* 14 - 0* 13 + 1* 27 + 1 43 + 1* 62 + I' 82 + 1*
91 + 1 24+ 1* lO-O lO- 0*
6.1 Tables of Numerical Results
163
Table 6.2. (continued) The effective principal quantum number LIn
0.5
1.0
1.5
2.0
no
2.5
3.0
3.5
4.0
4.5
5.0
1 1 1 1 1
28 - 0 79+0 15 + 1 25 + 1 37 + 1 49+ 1 59 + 1 66 + 1 67 + 1 65 + 1
47 -0 11 + 1 21 + 1 32 + 1 43 + 1 53 + 1 60 + 1 63 + 1 61 + 1 54+ 1
63 +0 15 + 1 26 + 1 37 + 1 48 + 1 57 + 1 62 + 1 62+ 1 57 + 1 51 + 1
79+0 18 + 1 30 + 1 42 + 1 52 + 1 60+ 1 63 + 1 61 + 1 55 + 1 45 + 1
93+0 21 + 1 33 + 1 46+ 1 56 + 1 62 + 1 64+ 1 61 + 1 53 + 1 48 + 1
10 + 23 + 37 + 50 + 60+ 65 + 66 + 61 + 53 + 41 +
99 + 1 10+2 95 + 1 80 + 1 60 + 1 34 + 1 16 + 1 91 +0 12 + 1 23 + 1
74 + 1 63 + 1 49 + 1 33 + 1 19 + 1 11 + 1 89+0 13 + 1 21 + 1 31 + 1
54 + 1 42 + 1 29 + 1 18 + 1 11 + 1 90+0 11 + 1 17 + 1 24+ 1 29+ 1
43 + 1 31 + 1 21 + I" 13 + 1 93 +0 96+0 13 + 1 18 + 1 22 + 1 25 + 1
37 + 1 26 + I" 17 + 1 11 + 1 90+0 10 + 1 14 + 1 18 + 1 21 + 1 23 + 1
34 + I" 23 + 1 15 + 1 10 + 1 92+0 11 + 1 14+ 1 18 + 1 20 + 1 20+ 1
31 + I" 21 + I" 13 + 1 99 +0" 95 +0 11 + 1 15 + 1 18 + 1 20 + 1 20+ 1
30 + I" 20 + I" 13 + 1 98 + 0" 99+0 12 + 1 15 + 1 18 + 1 19 + 1 18 + I"
33 + 1 46 + 1 55 + 1 57 + 1 51 + 1 35 + 1 20 + 1 10 + 1 90+0 15 + 1
38 + 1 40+ 1 37 + 1 29 + 1 20+ 1 12 + 1 84+0 90+0 14 + 1 22 + 1
30 + 1 28+ 1 23 + 1 16 + 1 11 + 1 80+0 83+0 11 + 1 16 + 1 21 + 1
24+ 1 21 + 1 16 + 1 11 + 1 83 +0 71 + 0 85 + 0 11 + 1 15 + 1 18 + 1
21 + 1 17 + I" 13 + 1 95 +0 72+0 70+0 88 +0 11 + 1 14 + 1 16 + 1
18 + 1 15 + I" 11 + I" 83 +0 67+0 71 + 0 90+0 11 + 1 13 + 1 14 + 1
17 + I" 13 + I" 10 + I" 75 +0 65+0 72+0 91 +0 11 + 1 13 + 1 13 + 1
16 + I' 12 + I" 94+0" 71 +0 64+0 73+0 92+0 11 + 1 12 + 1 12 + I"
Transition s - d, parameter C 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
39 + 53 + 66 + 75 + 78 +
Ll
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
1 1 1 1 1 1 1 1 I" I"
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
26+2 14+2 60 + 1 15 + 1 83 - 1 29 - 0 11 + 1 19 + 1 23 + 1 23 + 1
14+2 11 +2 75 + 1 40 + 1 16 + 1 40 -0 14 + 1 38 + 1 62 + 1 79 + 1 83 + 1 75 + 1 58 + 1 37 + 1 19 + 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
12 + 2 78 + 1 37 + 1 11 + 1 11- 0 13 -0 66+0 12 + 1 16 + 1 17 + 1
50+0 85 +0 24+ 1 43 + 1 59 + 1 66+ 1 63 + 1 52 + 1 36 + 1 20+ 1
22 + 1 34 + 1 44 + 1 49 + 1 47 + 1 34+ 1 21 + 1 11 + 1 83 +0 12 + 1
29 + 1 33 + 1 32 + 1 27 + 1 20 + 1 13 + 1 85 +0 79+0 11 + 1 19 + 1
23 + 1 23 + 1 20+ 1 15 + 1 10 + 1 77+0 73 +0 96+0 13 + 1 18 + 1
18 + 1 17 + 1 14 + 1 10 + 1 77+0 63 +0 70+0 94+0 12 + 1 15 + 1
16 + 1 14 + 1 11 + 1 85 +0 64+0 59+0 70+0 93 +0 11 + 1 13 + 1
14 + 1 12 + I" 96+0' 72+0 57+0 57+0 69+0 89+0 10 + 1 12 + 1
12 + I" 10 + I' 84+0' 64+0 64+0 56+0 69+0 87+0 10 + 1 11 + 1
11 + I" 98 + 0' 76+0" 59+0 51 +0 55+0 68+0 84+0 97+0 10+ 1
4.1 4.2 4.3 4.4
97 + 1 61 + 1 30+ 1 10 + 1
58+0 66+0 18 + 1 35 + 1
17 + 28 + 39 + 45 +
25 + 29 + 30 + 26 +
20+ 21 + 19 + 15 +
16 + 15 + 13 + 10 +
13 + 1 12 + 1 10 + 1 79+0
11 + 1 10 + I' 86+0 66+0
10 + 1 92+0' 74+0' 58+0
96+0' 83 + 0' 66+0' 52+0
1 1 1 1
1 1 1 1
1 1 1 1
1 1 1 1
164
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number no Lin
0.5
1.0
2.5
3.0
3.5
4.0
72+0 78+0 84+0 91 + 0 10 + I
81 + 0 62+0 63 +0 68+0 74+0 82+0 90+0 10 + 1 11 + 1 14+ 1
70+0 61 +0 66+0 74+0 83 +0 92+0 10 + 1 11 + 1 13 + 1 15 + 1
64+0 62+0 70+0 80+0 91 + 0 10 + 1 11 + 1 13 + 1 15 + 1 22+ I
88+0 94+0 10 + 1 11 + 1 14 + I
85 +0 91 + 0 99+0 10 + I 12 + 1 15 + 1 18 + I 13 + I 56+0 50+0
II + I 12 + 1 14 + 1 17 + I 20+ I 19 + I 89+0 46 -0 48 -0 61 +0
14+ I 16 + 1 19 + 1 22 + I 20 + I 98+0 49-0 47 - 0 60+0 77 +0
17 + 1 21 + 1 24 + I· 24 + 1 15 + I 64+0 45 -0 54+0 71 + 0 93 +0
21 + I 25 + I· 28 + 1 23 + 1 11 + I 53+0 48-0 62+0 83+0 11 + I
1.5
2.0
4.5
5.0
Transition s - d, parameter cp 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
84+0 86+0 90+0 98+0 16 + I 66+0 78+0 85 +0 90+0 96+0
14 + 1 59+0 65+0 71 +0 77+0 84+0 92+0 10 + 1 11 + 1 13 + 1
57 +0 68+0 80+0 92 +0 10 + I 12 + I 16 + I 16 + 1 83 +0 48 -0
75+0 92+0 11 + 1 13 + 1 16 + 1 18 + I 14 + I 62+0 44-0 52+0
96+0 11 + I 14 + 1 17 + 1 19 + 1 14 + 1 67+0 45 - 0 50+0 65+0
11 + 1 14 + I 18 + 1 21 + I 18 + I 10 + I 52 +0 46-0 58+0 76+0
14 + 1 17 + I· 21 + I 22+ 1 15 + 1 76+0 47 -0 50+0 66+0 92+0
62+0 60+0 60+0 64+0 66+0 69+0 74+0 79+0 83 +0 86+0 93 +0 99+0 99+0 10 + 1 11 + 1 11 + I 12 + 1 13 + 1 13 + 1 14 + 1 16 + 1 15 + 1 17 + 1 19 + 1 17 + 1 20 + 1 22 + I· 21 + 1 34+ 1 27 + I· 25 + I· 28 + I· 32 + I· 29 + I 33 + I· 36 + I· 30 + 1 31 + I 31 + 1 20+ I 17 + I· 15 + I' 87+0 74+0 66+0 49 - 0 48 - 0 49-0 52+0 57+0 63 +0 70+0 80+0 90+0 96+0 11 + 1 12 + 1 12 + 1 15 + 1 16 + I· 16 + 1 19 + I· 21 + I· 20 + I" 23 + I" 26 + I" 24 + I· 26 + I" 27 + I· 22 + 1 21 + 1 20+ 1 13 + 1 II + 1 97+0 63 +0 56+0 53 +0 46 -0 48 -0 51 + 0 55 +0 62+0 68+0 76+0 86+0 97 +0 10 + 1 12 + 1 13 + I"
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
86+0 89+0 94+0 10 + 1 16 + 1 57 +0 75+0 83 +0 90+0 96+0
18 + I 62+0 59+0 67+0 74+0 82+0 90+0 10 + I 11 + 1 13 + 1
49 -0 61 + 0 73 +0 86+0 10 + I 12 + I 15 + I 17 + I 10 + I 49-0
65 +0 81 + 0 99+0 12 + I 14 + 1 17 + I 15 + 1 76+0 45 -0 49-0
82+0 10 + 1 13 + I 16 + 1 18 + 1 15 + I 80+0 47 -0 47 -0 60+0
99+0 12 + I 16 + I 19 + 1 18 + 1 11 + 1 59+0 45 -0 53 +0 69+0
II + 1 15 + I 18 + 1 20+ 1 17 + 1 91 +0 51 + 0 47-0 59+0 82+0
13 + I 17 + I· 21 + I" 21 + I 14 + 1 75 +0 48 -0 50+0 67+0 92+0
4.1 4.2 4.3 4.4
87+0 90+0 96+0 10+ 1
19 + 1 68+0 57+0 64+0
47 -0 57+0 70+0 83 + 0
61 +0 76+0 94+0 11 + 1
76+0 97+0 12 + I 15 + 1
90+0 11 + 1 14 + 1 17 + 1
10 + 13 + 17 + 19 +
12 + 16 + 19 + 20+
1.1
1.2 1.3
1.4 1.5 1.6 1.7 1.8 1.9 2.0
I I I 1
I I" 1 1
15 + I· 17 + I" 20 + I· 22 + I" 23 + I" 24 + I' 21 + I 20+ 1 13 + 1 11 + I 65 +0 59+0 47 -0 48 -0 55 +0 60+0 76+0 85 + 0 10 + 1 II + 1 14 + 1 15 + I" 18 + I" 20 + I" 21 + I" 23 + I" 21 + 1 20+ 1
6.1 Tables of Numerical Results
165
Table 6.2. (continued) The effective principal quantum number LIn
1.5
2.0
2.5
3.0
n~
4.0
4.5
5.0
1 1 1 1 1 1 I' I' 1 O·
29 + 1 51 + 1 66+ 1 72 + 1 70 + 1 62 + I' 48 + I' 33 + I' 19 + 1 89 +0'
33 + 1 57 + 1 73 + 1 79+ 1 77 + 1 67 + I' 53 + I' 36 + I' 21 + I' 97 +0'
36+ 1 62 + 1 79+ 1 86 + 1 84+ 1 73 + I' 57 + I' 39 + I' 23 + I' 10 + l'
3.5
Transition p - s, parameter C 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
83 +0 15 + 1 21 + 1 24+ 1 24+ 1 21 + 1 16 + 1 11 + 1 58 +0 24-0
13 + 25 + 33 + 37 + 37 + 33 + 26 + 18 + 10 + 47 -
Ll 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
15 - 0 21 - O· 41 - O· 64+0' 81 + 0 85 +0 75 +0 53 +0 30-0 17 - 0
21 - 0 25 - O· 47 - O· 77 + O· 10 + l' 11 + 1 10+ 1 83 +0 55 +0 29 - O'
26- 0 27 - O· 51 + O· 83 + O· 11 + 1 12 + 1 11 + 1 91 + 0 60+0 31 - O·
30 -0 29 - O' 53 + O· 87 + O· 11 + 1· 13 + 1 12 + l' 10 + I· 68+0 36 - O·
33 - 0 31 - O· 55 + O· 90 +0' 12 + l' 13 + l' 13 + l' 10 + I' 71 +0 38 - O·
36-0 32 - O· 56 + O· 93 + O· 12 + 1· 14 + l' 13 + l' 11 + l' 76+0 41 - O·
39- 0 33 - O· 58 + O· 96+0· 13 + I' 14 + I' 14 + I' 11 + l' 79+0 42 - O·
42 -0 35 - O· 60+0' 99 +0· 13 + I· 15 + I' 14 + I' 12 + I· 83 +0 45 - O·
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
16 - 0 18 - O· 33 - O· 53 - O· 71 + O· 81 + 0 78+0 63+0 43 -0 24 - O·
18 - 0 19 - O· 33 - O· 54+0' 73 +0' 83+0 80+0 65+0 43 -0 24 - O·
19 - 0 19 - O· 32 - O· 52 + O· 72 +0' 83 +0 82+0' 69 +0' 48 - 0 27 - O·
20-0 19 - O· 32 - O· 52 + O· 71 + O· 83 +0 82 +0· 69 +0' 48 -0 27 - O·
21 - 0 19 - O· 31 - O· 51 + O· 71 + O· 83 +0' 83 + O· 70 +0· 50 + O· 28 - O·
22- 0 19 - O· 31- O' 51 + O· 70+0' 83 + O· 83 +0· 70+0' 50+0 28 - O·
22- 0 19 - O· 31 - O· 51 + O· 70+0' 83 +0· 83 + O· 72 +0' 51 + 0 29 - O'
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
12 - O· 17 - O· 32 - O· 49 - O· 63 +0 66+0 58+0 41 -0 23 -0 15 - 0 12 - O· 16 - O· 29 - O· 44 - O· 56+0 59+0 51 + 0 36-0 20- 0 14 - 0
14 - 0 16 - O· 28 - O· 45 - O· 61 + 0 70+0 68+0 56+0 38-0 21 - O·
15 - 0 16 - O· 27 - O· 44- O· 60+ O· 68+0 66+0 54+0 37 - 0 21- 0
15 - 0 15 - O· 25 - O· 41 - O· 57 + O· 67 +0 66+0 56+0 40-0 23 - O·
15 - 0 15 - O· 24 - O· 40 - O· 55 + O· 64+0 64+0 55 + O· 39 - 0 22 - O·
16 - 0 15 - O· 23 - O· 38 - O· 53 + O· 63 +0 63 +0· 55 + O· 39- 0 23 - O·
16 - 0 14 - O· 23 - O· 37 - O· 51 + O· 61 + 0 62+0' 53 + O· 39-0 23 - O·
16 - 0 14- O· 22 - O· 36 - O· 50+0' 60+0 61 + O· 53 + O· 39-0 23 - O·
4.1 4.2 4.3 4.4
11 15 27 42
13 -0 15 - O· 26 - O· 42 - O·
14- 0 15 - O· 25 - O· 40 - O·
14 14 22 36 -
13 13 21 34 -
13 -0 12 - O' 20 - O· 32 - O·
13 -0 12 - O· 19 - O· 30 - O·
13 -0 12 - O· 18 - O· 29 - O·
-
O· O· O· O·
1 1 1 1 1 1 1 1 1 O·
18 + 32 + 43 + 48 + 47 + 42 + 33 + 22 + 13 + 58 +
1 1 1 1 1 1 1 I' l' O·
22 + 39 + 51 + 57 + 56 + 49 + 39 + 27 + 15 + 71 +
1 1 1 1 1 1 I' I' 1 O·
0 O· O· O·
26 + 45 + 59 + 65 + 63 + 56 + 44 + 30 + 17 + 80 +
0 O' O· O·
166
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number An
1.5
3.0
3.5
4.0
4.5
5.0
1 1 1 1 1 1 1 I· 1* I·
14 + 1 21 + 1 29 + 1 37 + 1 46+ 1 58 + 1 72 + 1* 88 + I· 10+2 66 + 1*
15 + 1 23 + 1 32 + 1 41 + 1 51 + 1 64+ 1 80 + I· 99 + 1* 11 +2 72 + 1*
16 + 1 25 + 1 34+ 1 45 + 1 57 + 1 71 + I· 89 + I· 11 +2· 12 +2 84+ 1*
17 + 1 27 + 1 37 + 1 49+ 1 62+ 1 78 + I· 97 + I· 12 +2· 14+ 2· 90 + 1*
18 + 1 29+ 1 40+ 1 53 + 1 67 + 1 84 + I· 10+2· 13 +2· 15 +2* 98 + 1*
10-0 10- O· 10-0* 66+0· 15 + 1· 25 + 1 36+ 1 47 + 1 51 + 1 27 + 1·
29-0 10 - 0* 10 - 0* 69+0* 17 + 1 28 + 1 41 + 1 54+ 1 57 + 1 27 + 1·
52+0 10 - 0* 10 - 0* 72+0· 18 + 1· 31 + 1 46 + I· 61 + 1· 68 + 1 40 + 1·
70+0 10-0· 10 - O· 77+0· 20 + 1* 34 + 1* 50 + 1· 67 + 1· 75 + 1 42 + 1·
86+0 10 - 0* 10 -0* 82 +0* 21 + 1* 37 + 1* 55 + 1· 74 + 1· 85 + 1 51 + 1*
99+0 10- 0* 10- 0* 88+0· 23 + 1* 40 + 1· 59 + I· 80 + I· 92 + 1 54 + 1·
11 + 1 10 - 0* 10-0* 94+0· 25 + 1* 43 + 1· 64+ 1* 87 + I· 10+2 60 + 1*
10-0 10- O· 10 - O· 43 - 0* 12 + 1* 22+2 32+ 1 42+ 1 44+ 1 22 + 1*
10 - 0 10 - O· 10 - O· 41 - O· 13 + 1· 24+ 1 35 + 1 46+ 1 47 + 1 19 + 1·
28-0 10 - O· 10 - O· 41 - O· 14 + I· 26+ 1 39 + 1· 52 + I· 57 + 1 33 + I·
42 -0 10 - O· 10 - O· 42 - 0* 15 + 1· 28 + 1 43 + 1* 57 + I· 62 + 1 33 + I·
57+0 10 - O· 10 - O· 44 - 0* 16 + I· 20 + 1* 46 + 1* 63 + 1· 70+ 1 41 + 1·
68+0 10 - 0* 10 - 0* 46 - 0* 17 + 1· 32 + 1* 50 + I· 68 + I· 76+ 1 42 + I·
79+0 10 - O· 10 - 0* 49 - 0* 18 + I· 34 + 1* 53 + 1· 73 + I· 83 + 1 48 + I·
10-0 10 - O· 10 - O· 34- O· 11 + 1 20+ 1 30+ 1 39+ 1 41 + 1 20+ 1·
10 - 0 10 - 0* 10 - O· 32 - O· 12 + 1* 22+ 1 33 + 1 43 + 1 42 + 1 16 + 1 10 - 0 10 - 0* 10 - O· 27 - O·
17 - 0 10 - O· 10 -0· 30 - 0* 12 + 1· 23 + 1 36+ 1 48 + 1 52+ 1 29 + 1· 12 - 0 10 - O· 10 - O· 25 - O·
30-0 10 -0· 10 - O· 30 - O· 13 + I· 25 + 1 39+ 1 53 + 1 56+ 1 28 + 1· 23 -0 10 -0· 10-0· 24-0·
43 -0 10 - O· 10 - O· 31- 0* 14 + I· 27 + 1 42+ I· 57 + I· 64+ 1 36 + 1· 35 - 0 10 -0· 10 -0· 24-0·
53+0 10 - O· 10 - O· 32 - O· 14+ I· 29+ 1 45 + 1· 62 + I· 68 + 1 37 + 1· 45 -0 10 - O· 10 -0· 24-0·
63+0 10- O· 10 - O· 33 - O· 15 + 1· 30+ 1 48 + I· 66+ I· 74+ 1 43 + 1·
2.0
2.5
Transition p - s, parameter 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 Ll
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 4.1 4.2 4.3 4.4
10+ 1 14 + 1 19 + 1 24+ 1 30+ 1 37 + 1 46+ 1 55 + 1 52 + 1 11 + 1 10-0 10- O· 10- O· 67 +0· 14 + 1 23 + 1 32 + 1 38 + 1 27 + 1 10-0 10- O· 10 - O· 10- O· 49-0* 12 + 1 20+ 1 28 + 1 33 + 1 19 + 1 10-0 10 - O· 10- 0* 10-0· 42 -0· 11 + 1 19 + 1 27 + 1 30 + 1 14 + 1 10-0 10-0* 10 - O· 10 - O· 39- O·
no
11 + 17 + 22+ 28+ 35 + 44+ 54+ 66+ 74+ 45 +
1 1 1 1 1 1 1 1 1 1·
10 - 0 10- 0* 10- O· 30- O·
12 + 19 + 25 + 33 + 41 + 51 + 63 + 78 + 87 + 49 +
qJ
54+0 10 - O· 10 - O· 25 - O·
167
6.1 Tables of Numerical Results Table 6.2. (continued) The effective principal quantum number no LIn
2.0
1.5
3.0
3.5
4.0
4.5
5.0
16+2 15 +2 13 +2 10+2 73 + 1 44+ 1 26+ 1 19 + 1 22+ 1 33 + 1 45 + 1 54+ 1 56+ 1 51 + 1 41 + 1
19+2 17 + 2 14+2 11 +2 77 + 1 46+ 1 27 + 1 20+ 1 24+ 1 35 + 1 47 + 1 55 + 1 56 + 1 51 + 1 40+ 1
21 +2 19 +2 16+2 12 +2 81 + 1
23 +2 21 +2 17+2 12 +2 86+ 1
27+2 24+2 19 +2 14+2 96+ 1
49+ 1 28 + 1 21 + 1 25 + 1 36+ 1 48 + 1 56+ 1 57 + 1 51 + 1 40+ 1
51 + 1 30+ 1 22+ 1 27 + 1 38+ 1 50+ 1 58 + 1 58 + 1 51 + 1 40+ 1
25+2 22+2 18+2 13+2 91 + 1 54+ 1 31 + 1 23 + 1 28+ 1 40+ 1 52+ 1 59+ 1 59+ 1 52+ 1 41 + 1
28 + 19 + 14 + 16 + 22 + 30 + 36 + 39 + 36 + 30 +
28 + 19 + 14 + 15 + 22 + 29 + 35 + 38 + 35 + 29 +
1 1 1 1 1 1 1 1 1 1
28+ 1 19 + 1 14 + 1 16 + 1 22 + 1 29+ 1 35 + 1 37 + 1 34+ 1 28+ 1
28 + 1 19 + 1 14 + 1 16 + 1 22+ 1 29+ 1 35 + 1 37 + 1 34+ 1 28 + 1
29+ 1 19 + 1 14+ 1 16 + 1 22+ 1 29+ 1 35 + 1 36+ 1 34+ 1 27 + 1
21 + 1 14 + 1 11 + 1 12 + 1 16+ 1 22 + 1 27 + 1 29+ 1 27 + 1 23 + 1
20+ 1 14 + 1 11 + 1 12 + 1 16 + 1 21 + 1 26+ 1 28 + 1 27 + 1 22 + 1
20+ 14 + 11 + 11 +
21 + 1 15 + 1 11 + 1 12 + 1 17 + 1 23 + 1 28 + 1 30+ 1 29+ 1 25 + 1 18 + 1 13 + 1 10 + 1 11 + 1
17 + 1 12 + 1 10+ 1 10+ 1
17 + 1 12 + 1 96+0 10+ 1
20+ 1 14+ 1 11 + 1 11 + 1 16 + 1 21 + 1 25 + 1 27 + 1 26+ 1 22+ 1 16 + 1 12 + 1 93+0 99+0
2.5
Transition p - p, parameter C ,,=0 0.6 0.7 0.8 0.9 1.0
10+2 11 +2 10+2 87 + 1 65 + 1
14+2 13 +2 12+2 96+ 1 67 + 1
1.1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
39 + 22+ 14+ 16 + 26+ 39 + 51 + 58 + 57+ 49+
1 1 1 1 1 1 1 1 1 1
42 + 25 + 18 + 21 + 31 + 43 + 52+ 55 + 51 + 41 +
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
31 + 20+ 13 + 13 + 20+ 31 + 42+ 49+ 50+ 45 +
1 1 1 1 1 1 1 1 1 1
30+ 1 20+ 1 15 + 1 16 + 1 22 + 1 31 + 1 39+ 1 43 + 1 41 + 1 34+ 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 4.1 4.2 4.3 4.4
29+ 1 19 + 1 13 + 1 12 + 1 18 + 1 28+ 1 39+ 1 46+ 1 48+ 1 44+ 1 28+ 1 19 + 1 13 + 1 12 + 1
26+ 1 18 + 1 14 + 1 14 + 1 19 + 1 27 + 1 34+ 1 38 + 1 37 + 1 31 + 1
29+ 1 19 + 1 14 + 1 15 + 1 22+ 1 30+ 1 38 + 1 41 + 1 39 + 1 33 + 1 24+ 1 16 + 1 12 + 1 13 + 1 18 + 1 25 + 1 32 + 1 35 + 1 34+ 1 29 + 1
24+ 17 + 13 + 13 +
21 + 15 + 11 + 12 +
1 1 1 1 1 1 1 1 1 1
1 1 1 1
1 1 1 1
1 1 1 1 1 1 1 1 1 1
22 + 1 16 + 1 12 + 1 13 + 1 17 + 1 24+ 1 29+ 1 32+ 1 31 + 1 26+ 1 1 1 1 1
57 + 32 + 24+ 29+ 41 + 54+ 61 + 61 + 53 + 41 +
1 1 1 1 1 1 1 1 1 1
168
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number no LIn
1.5
2.0
2.5
Transition p - P. parameter K=O
3.0
3.5
4.0
4.5
5.0
qJ
0.6 0.7 0.8 0.9 1.0
90+0 84+0 81 +0 80+0 82+0
77+0 77+0 80+0 87+0 10 + 1
78+0 82+0 90+0 10 + 1 12 + 1
83+0 90+0 10 + 1 11 + 1 14 + 1
88+0 97+0 11 + 1 13 + 1 16 + 1
94+0 10+ 1 12 + 1 14 + 1 19 + 1
99+0 11 + 1 13 + 1 16+ 1 22+ 1
10 + 12 + 14 + 18 + 24+
1.1
94+0 13 + 1 20+ 1 17 + 1 11 + 1 85+0 74+0 70+0 69+0 72+0 82+0 11 + 1 17 + 1 17 + 1 11 + 1 86+0 73+0 68+0 67+0 69+0
12 + 1 16 + 1 15 + 1 92+0 64+0 57+0 58+0 62+0 71 +0 84+0
15 + 1 18 + 1 14+ 1 74+0 56+0 55+0 60+0 69+0 81 +0 99+0 12 + 1 15 + 1 14 + 1 83 +0 57+0 53 +0 56+0 64+0 75+0 92+0
18 + 1 21 + 1 14 + 1 70+0 54+0 56+0 63 +0 75 +0 91 +0 11 + 1
22 + 1 25 + 1 14 + 1 67+0 53 +0 57+0 67+0 81 +0 10 + 1 13 + 1
26+ 1 28+ 1 14+ 1 64+0 52+0 58+0 71 +0 88+0 11 + 1 15 + 1
29+ 1 31 + 1 13 + 1 61 +0 51 +0 60+0 75 +0 96+0 12 + 1 17 + 1
34+ 1 34+ 1 13 + 1 59+0 52+0 62+0 80+0 10+ 1 13 + 1 19 + 1
15 + 1 18 + 1 15 + 1 81 +0 56+0 52+0 58+0 68+0 83 +0 10 + 1
17 + 1 21 + 1 15 + 1 77+0 53 +0 52+0 60+0 73+0 92+0 12 + 1
20+ 1 24+ 1 16+ 1 74+0 51 +0 52+0 63 +0 79+0 10 + 1 13 + 1
23 + 1 27 + 1 16 + 1 72+0 50+0 53 +0 66+0 85+0 11 + 1 15 + 1
26+ 1 30+ 1 16 + 1 70+0 50+0 55 +0 70+0 92+0 12 + 1 17 + 1
78+0 10+ 1 16+ 1 17 + 1 12 + 1 87+0 73+0 67+0 66+0 68+0 76+0 10+ 1 12 + 1 17 + 1
10 + 1 13 + 1 13 + 1 97+0 65+0 54+0 53 +0 57+0 64+0 76+0
11 + 1 14+ 1 13 + 1 87+0 59+0 52+0 55+0 62+0 73 +0 89+0 11 + 1 14 + 1 13 + 1 88+0
13 + 1 17 + 1 15 + 1 86+0 57+0 51 + 0 56+0 65+0 80+0 10 + 1
16 + 1 19 + 1 15 + 1 83 +0 54+0 51 + 0 57+0 69+0 87+0 11 + 1
21 + 1 25 + 1 17 + 1 78+0 51 +0 51 +0 62+0 80+0 10+ 1 14 + 1
23 + 1 27 + 1 17 + 1 76+0 50+0 52+0 65+0 86+0 11 + 1 16+ 1
13 + 1 16 + 1 15 + 1 89+0
15 + 1 19 + 1 15 + 1 85+0
18 + 1 22+ 1 16 + 1 80+0 52+0 51 +0 59+0 74+0 96+0 12 + 1 17 + 1 21 + 1 16 + 1 83 +0
19 + 1 23 + 1 17 + 1 81 +0
22+ 1 26+ 1 17 + 1 80+0
1.2 1.3
1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0 3.1 ~.2
3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 4.1 4.2 4.3 4.4·
10 + 1 13 + 1 14 + 1 96+0 64+0 55+0 54+0 58+0 66+0 79+0
97+0 12 + 1 13 + 1 97+0
1 1 1 1 1
169
6.1 Tables of Numerical Results Table 6.2. (continued) The effective principal quantum number no LIn
1.5
2.0
2.5
3.0
3.5
4.0
4.5
5.0
Transition p - p, parameter C
K=2 O.l 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
19 - 0 47 - 0 83+0 12 + 1 15 + 1 18 + 1 19 + 1 18 + 1 15 + 1 12 + 1
42 -0 93 +0 14 + 1 19 + 1 23 + 1 25 + 1 25 + 1 22 + 1 19 + 1 14 + 1
59+0 12 + 1 19 + 1 25 + 1 29 + 1 30 + 1 29 + 1 26 + 1 21 + 1 16 + 1
76+0 15 + 1 23 + 1 30 + 1 34 + 1 35 + 1 33 + 1 29 + 1 23 + 1 17 + 1
91 +0 18 + 1 27 +11 34 + 1 38 + 1 39 + 1 37 + 1 31 + 1 25 + 1 18 + 1
10+ 1 21 + 1 31 + 1 38 + 1 43 + 1 43 + 1 40 + 1 34+ 1 27 + 1 19 + 1
12 + 1 24+ 1 35 + 1 43 + 1 47 + 1 47 + 1 43 + 1 37 + 1 29 + 1 21 + 1
13 + 26+ 38 + 47 + 51 + 51 + 47 + 39 + 31 + 22 +
1.1
1.4 1.5 1.6 1.7 1.8 1.9 2.0
84+0 57+0 43 -0 44-0 59+0 79+0 99+0 11 + 1 10 + 1 96+0
10 + 1 73 +0 60+0 64+0 79+0 99+0 11 + 1 12 + 1 11 + 1 97 +0
11 + 1 80+0 67 +0 72+0 88+0 10 + 1 12 + 1 12 + 1 11 + 1 10 + 1
12 + 1 86+0 72 +0 78 +0 94+0 11 + 1 12 + 1 12 + 1 11 + 1 10 + 1
12 + 1 91 +0 76+0 83 +0 10 + 1 11 + 1 13 + 1 13 + 1 12 + 1 10 + 1
13 + 1 95 +0 81 + 0 87 +0 10 + 1 12 + 1 13 + 1 13 + 1 12 + 1 10+ 1
14 + 1 10 + 1 84+0 92+0 11 + 1 12 + 1 14 + 1 14 + 1 12 + 1 10 + 1
15 + 1 10 + 1 88+0 96+0 11 + 1 13 + 1 14 + 1 14 + 1 13 + 1 11 + 1
2.l 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
70+0 52+0 40- 0 39-0 50 + 0 67+0 84+0 96+0 98+0 90+0
78+0 62 +0 52 +0 53 +0 64+0 78+0 91 +0 98+0 95 +0 84+0
80+0 63 +0 55 +0 56+0 66+0 80+0 91 + 0 97 +0 94+0 83 +0
82+0 65 + 0 56 + 0 58+0 67 +0 80+0 91 +0 95 +0 91 +0 81 + 0
83 +0 65 +0 57+0 59+0 68+0 81 +0 91 + 0 94+0 90+0 80+0
84+0 66+0 57 +0 59+0 69+0 81 +0 90+0 94+0 89+0 79+0
86+0 67 +0 58 + 0 60+0 70+0 82+0 91 +0 94+0 89+0 78+0
87+0 68+0 59+0 61 +0 71 +0 83 +0 91 +0 94+0 89+0 78+0
3.l 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
66+0 58 + 0 39 - 0 38 - 0 47 -0 63+0 79+0 92+0 95+0 87+0
70+0 57 +0 49 -0 50+0 58+0 71 + 0 83 + 0 89+0 87+0 78+0
69+0 56+0 49 -0 50+0 58 + 0 69+0 80+0 85 +0 84+0 76+0
68+0 56+0 49 -0 50+0 57 +0 68 + 0 77 +0 81 + 0 79+0 72+0
67 +0 55 +0 48 -0 49 - 0 56+0 66+0 75 +0 79+0 77+0 69+0
66+0 54+0 48 -0 49 - 0 56+0 65 +0 73 +0 76+0 74+0 67+0
65 +0 53 + 0 47 - 0 48 -0 55 +0 64+0 72+0 75+0 72+0 65 +0
65 +0 53 +0 47 -0 48 - 0 55+0 63 +0 71 +0 74+0 71 +0 64+0
4.l 4.2 4.3 4.4
64+0 49-0 39-0 37 - 0
66+0 54+0 47 -0 48 - 0
63 +0 53 + 0 47 - 0 47 -0
61 51 45 46
59+0 49 -0 44-0 45 - 0
57 +0 48 -0 42 -0 43 -0
55 +0 46-0 41 - 0 42 -0
54+0 45 -0 40 -0 41 - 0
1.2 1.3
+0 +0 -0 - 0
1 1 1 1 1 1 1 1 1 1
170
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number no LIn.
1.5
2.0
2.5
Transition p - p, parameter ,,=2
3.0
3.5
4.0
4.5
5.0
qJ
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
18 + 1 10 + 1 79+0 70+0 68+0 70+0 75+0 84+0 96+0 11 + 1
13 + 1 75 +0 64+0 65 +0 71 + 0 79+0 91 + 0 10 + 1 12 + 1 14 + 1
98 +0 64+0 63 + 0 70+0 79+0 91 +0 10 + 1 12 + 1 14 + 1 17 + 1
81 + 0 61 + 0 66+0 76+0 88 + 0 10 + 1 12 + 1 14 + I 17 + I 20 + 1
71 + 0 61 + 0 70+0 83 +0 98 +0 11 + 1 13 + 1 16 + 1 20 + 1 24 + 1
66+0 63 +0 75 + 0 89+0 10 + 1 12 + 1 15 + 1 19 + 1 23 + 1 27 + 1
62+0 65 +0 79+0 97+0 11 + 1 14 + 1 17 + 1 22 + 1 27 + 1 32 + 1
60+0 68 +0 84+0 10 + 1 12 + 1 15 + 1 19 + 1 24+ 1 30 + 1 35 + 1
1.1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
14 + I 16 + 1 12 + 1 72+0 49-0 46-0 51 + 0 61 + 0 73 +0 90+0
16 + 1 14 + 1 87+0 51 + 0 42 -0 47 -0 58+0 72+0 90+0 10 + 1
18 + I 14 + 1 84+0 49 -0 43 - 0 49 -0 63 +0 80+0 10 + 1 12 + 1
21 + 1 15 + 1 83 +0 48 - 0 43 -0 53 +0 69+0 91 + 0 11 + I 14 + 1
24 + 1 16 + 1 82+0 47 - 0 45 - 0 57+0 77+0 10 + I 13 + 1 16 + 1
26 + 1 17 + 1 80+0 47 -0 47 -0 61 +0 85 +0 11 + 1 15 + 1 18 + 1
29 + I 17 + 1 79+0 47 -0 49 - 0 66+0 94+0 13 + 1 17 + 1 21 + 1
32 + 1 17 + 1 78+0 48 -0 52+0 72+0 10 + 1 14 + 1 19 + 1 23 + 1
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
11 + 1 13 + 1 12 + 1 78+0 58+0 44-0 48 - 0 56+0 68+0 83 +0
12 + 1 12 + 1 88+0 56+0 43 -0 44 -0 52 +0 65 +0 81 + 0 98 +0
14 + 1 12 + 1 88 +0 55 + 0 43 -0 45 - 0 55 +0 70+0 89+0 11 + 1
16 + 1 13 + 1 89+0 54+0 43 -0 47 - 0 60+0 78 +0 10 + 1 12 + 1
18 + 1 14 + 1 90+0 53 +0 43 - 0 49 -0 65 +0 87+0 11 + 1 14 + 1
20+ 1 15 + 1 89+0 52+0 44 - 0 52 +0 71 + 0 97 +0 12 + 1 16 + 1
22 + 1 16 + 1 89+0 52+0 45 -0 56+0 77+0 10 + 1 14 + 1 18 + 1
24 + 1 16 + 1 88+0 51 + 0 46-0 59+0 84+0 11 + 1 16 + 1 20 + 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
10 + 1 12 + 1 12 + 1 79+0 51 +0 44-0 47 - 0 54+0 66+0 80+0
11 + 1 11 + 1 87+0 58+0 44-0 43 -0 50+0 62+0 77+0 94+0
12 + 1 12 + 1 88 +0 57+0 43 -0 44-0 52 + 0 66+0 84+0 10 + 1
14 + 1 13 + 1 90+0 56+0 43 -0 45 -0 56+0 73 +0 95 +0 11 + 1
15 + 1 13 + 1 91 + 0 55 +0 43 - 0 47 -0 60+0 81 + 0 10 + 1 13 + 1
17 + I 14 + 1 91 + 0 55 +0 44 - 0 49 -0 65 +0 89+0 11 + 1 14 + 1
19 + I 15 + 1 92+0 54+0 44-0 52 +0 70+0 98 +0 13 + 1 16 + 1
21 + 1 16 + 1 91 +0 54+0 45 -0 55 +0 76+0 10 + 1 14 + 1 18 + 1
4.1 4.2 4.3 4.4
10 + 1 12 + 1 11 + 1 80+0
10 + 1 10 + 1 86+0 58+0
11 + 1 11 + 1 87 + 0 58+0
13 + 1 12 + 1 90+0 58 +0
14 + 1 13 + 1 92+0 57 +0
16 + 1 14 + 1 92+0 56+0
17 + 1 14 + 1 92+0 55 +0
19 + 1 15 + 1 93 +0 55 +0
6.1 Tables of Numerical Results
171
Table 6.2. (continued) The effective principal quantum number no ,1n
3.0
3.5
4.0
4.5
5.0
22+2 27+2 30+2 30+2 28+2
24+ 1 58 + 1 10 + 2 15 + 2 20+2 23 +2 25 +2 25 +2 23 +2 19 + 2
37 + 1 80 + 1 13 +2 17 +2 22+2 24+2 25 +2 24+2 20 +2' 15 + 2'
47 + 1 98 + 1 15 + 2 19 + 2 23 +2 25 +2 25 +2 22 +2' 18 + 2' 13 + 2'
57 + 1 11 +2 16 + 2 21 +2 24+2 26+2 25 + 2' 21 + 2' 17 + 2' 11 + 2'
65 + 1 12 +2 18 + 2 23 +2 26+2 26+2 25+2* 21 + 2' 15 + 2' 99 + I'
73 + 1 13 +2 19 + 2 24+2 27 +2 27 +2' 25 + 2' 20 +2' 14 + 2' 89 + I'
1.4 1.5 1.6 1.7 1.8 1.9 2.0
34+2 31 + 2 26+2 19+2 12 +2 50 + I' 99+0 76 +0' 31 + 1 68 + 1
23+2 16+2 94 + I' 40+ 1 10 + 1 14 + l' 38 + I' 73 + 1 11 +2 13+2
14 + 2' 86 + I' 40+ 1 10 + I' 10 + I' 25 + I' 49+ 1 73 + 1 89 + 1 93 + 1
10 + 55 + 17 + 83 + 16 + 34 + 55 + 74 + 82 + 78 +
2' I' I' 0' I' I' 1 1 1 1
79 + I' 39 + 1 10 + I' 96 +0' 20 + I' 37 + 1 55 + 1 68 + 1 71 + I' 63 + I'
67 + I' 26 + I' 91 + 0' 11 + I' 23 + I' 40+ 1 56 + 1 66 + I' 66 + I' 55 + I'
61 + I' 18 + I' 87 +0 13 + I' 25 + I' 41 + 1 55 + I' 62 + I' 59 + I' 47 + I'
56 + I' 15 + I' 89+0 14 + I' 27 + I' 43 + I' 55 + I' 61 + I' 55 + I' 42 + I'
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
13 +2 16+2 16+2 14+2 10+2 58 + 1 20 + I' 41- 0 13 + I' 39 + 1
13+2 11 +2 80 + I' 44 + I' 14 + 1 79 +0' 19 + I' 43 + 1 74+ 1 10+2
86 + I' 64 + I' 37 + I' 13 + I' 65 +0' 12 + I' 27 + 1 45 + 1 61 + 1 69 + 1
63 + 41 + 19 + 67 + 79 + 17 + 31 + 46 + 56 + 57 +
1 1 1 0' 0' I' 1 1 1 I'
48 + I' 29 + I' 10 + I' 57 +0 94+0' 18 + I' 30 + 1 41 + 1 47 + I' 45 + I'
39 + I' 22 + 1 76 +0' 58 + 0' 10 + I' 20 + I' 31 + 1 39 + I' 43 + I' 39 + I'
33 + I' 16 + I' 62 +0' 62 +0' 11 + I' 20 + I' 30 + I' 37 + I' 38 + I' 33 + I'
30 + I' 12 + I' 56 + 0' 66+0' 12 + I' 21 + I' 30 + I' 35 + I' 35 + I' 29 + I'
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
94+ 1 12 + 2 13 +2 12+2 10+2 61 + 1 24 + I' 47 -0 88 + 0' 28 + 1
10+2 98 + 1 74+ 1 45 + 1 18 + 1 70+0 13 + I' 33 + 1 61 + 1 89 + 1
69 + 1 55 + I' 35 + I' 15 + 1 57+0 92+ 0' 20 + I' 36 + 1 50 + 1 59 + 1
49 + I' 35 + I' 18 + 1 65 +0' 59 +0' 12 + I' 24 + 1 36 + 1 46 + 1 48 + 1
37 + I' 24 + I' 10 + I' 48 - 0 66 +0' 13 + I' 22 + 1 31 + 1 37 + I' 37 + I'
30 + 19 + 71 + 45 73 + 14 + 22 + 30 + 34 + 32 +
I' 1 0' 0' 0' I' 1 1 I' I'
25 + I' 14 + 1 54+0' 44 - 0' 78 + O· 14 + I' 21 + I' 27 + I' 29 + I' 27 + I'
22 + I' 10 + I' 46 - O· 45 - 0' 82 +0' 14 + I' 21 + I' 26 + I' 27 + I' 23 + I'
4.1 4.2 4.3 4.4
77 + 1 10+2 12 + 2 11 +2
97 + 91 + 71 + 45 +
62 + 51 + 34 + 15 +
43 + I' 31 + I' 18 + 1 64 +0'
32 + 22 + 10 + 45 -
25 + I' 17 + I' 68 +0' 39-0
21 + I' 12 + 1 50+0' 37 - 0'
18 + I' 99+0' 41 - 0' 37 - 0'
1.5
2.0
2.5
Transition p - d, parameter C K = 1 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1
1.2 1.3
1 1 1 1
1 I' I' 1
I' I' 1 0
172
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number no
An
1.5
2.0
2.5
3.0
3.5
4.0
4.5
5.0
14+ 1 19 + 1 24+ 1 29 + 1 35 + 1 41 + 1 50+ 1 60+ 1 74 + 1* 94 + 1* 11 +2* 14+ 2* 49 + 1* 12 - 0* 24 - 0* 10 + 1* 20+ 1 31 + 1 45 + 1 62+ 1 85 + 1* 11 +2 91 + 1 90+0* 10 - 0* 55 +0* 14 + 1 24+ 1 37 + 1 52 + 1*
15 + 1 21 + 1 27 + 1 34+ 1 41 + 1 50 + 1 62 + 1 76 + 1* 96 + 1* 11+2* 14 +2* 14+2 16 + 1* 10 - 0* 52+0* 15 + 1 27 + 1 41 + 1 59 + 1* 81 + 1*
16 + 1 23 + 1 30+ 1 38 + 1 48 + 1 59+ 1 73 + 1* 92 + 1* 11+2* 13+2* 17 +2* 93 + 1* 70+0* 10 - 0* 81 + 0* 19 + 1 33 + 1 51 + 1* 72 + 1* 97 + 1*
17 + 1 25 + 1 34+ 1 43 + 1 55 + 1 68+ 1 86 + 1* 10 +2* 12+2* 15 +2*
18 + 1 27 + 1 37 + 1 48+ 1 62+ 1 78 + 1* 98 + 1* 12 +2* 13 +2* 16 +2*
20+2* 54+ 1* 35 - 0* 22 - 0* 11 + 1* 24+ 1 40+ 1* 61 + 1* 85 + 1* 11 + 2*
10+2* 13 +2* 42 + 1* 21- 0 14 - 0* 87 +0* 19 + 1 31 + 1 48 + 1* 68 + 1*
12 +2* 12 +2* 20 + 1* 10 - 0* 33 - 0* 12 + 1* 24+ 1 39 + 1* 59 + 1* 82 + 1*
14 + 2* 92 + 1* 11 + 1* 10 - 0* 53 +0* 15 + 1* 29 + 1* 47 + 1* 70 + 1* 95 + 1*
22+2* 35 + 1* 22-0 36 -0* 14 + 1* 28 + 1* 47 + 1* 70 + 1* 96 + 1* 12 + 2* 16 + 2* 63 + I· 67+0* 10 - 0* 73 +0* 19 + 1* 35 + 1* 56 + 1*' 80 + 1* 10 + 2*
73 + 1* 98 + 1* 98 + 1 15 + 1* 10 - 0* 36 - 0* 11 + 1 21 + 1 33 + 1 48 + 1 67 + 1* 91 + 1* 98 + 1 20+ 1*
92 + 1* 11+2* 57 + 1* 48 -0 10 - 0* 63 +0* 15 + 1 27 + 1 42 + 1* 62 + 1*
10+2* 12 +2 30 + 1* 15 - 0* 17 - 0* 92+0* 20+ 1 34+ 1 52 + 1* 75 + 1*
12 + 2* 10+2 16 + 1* 10 - O· 32 - 0* 12 + 1* 24 + 1* 41 + 1* 62 + 1* 87 + 1*
14+2* 79 + 1* 10 + 1* 10 - 0* 49-0* 15 + 1* 29 + 1* 48 + 1* 7l + 1* 96 + 1*
85 + 1* 10+2* 66+ 1 68+0
10+2* 11 + 2* 36 + 1* 25 -0
11 + 2* 10+2 21 + 1* 10 - 0*
12 + 2* 87 + 1* 13 + 1* 10-0*
Transition p - d, parameter (() ,,=1 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
28+ 1 32+ 1 37 + 1 43 + 1 54+ 1 83 + 1* 57+ 1 10 - 0* 85+0 15 + 1
52 + 1 66+ 1 88 + 1* 98+ 1 10+ 1 10-0* 67+0* 14+ 1 21 + 1 29+ 1
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
21 + 1 26+ 1 32+ 1 39+ 1 49+ 1 69+ 1 96+ 1* 28-0 34- 0* 11 + 1
38+ 1 50+ 1 68 + 1* 88 + 1* 40+ 1 10 - 0* 25 - 0* 98+0 17 + 1 25 + 1
13 + 1 16 + 1 20+ 1 24+ 1 28 + 1 33 + 1 39 + 1 46+ 1 56+ 1 69 + 1 87 + 1* 11+2* 12 +2 15 + 1* 10 - 0* 56+0* 14 + 1 23 + 1 33 + 1 46+ 1 61 + 1* 83 + 1* 10 + 2* 47 + 1* 11 - 0* 17 - 0* 90+0 17 + 1 27 + 1 39+ 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
18 + 1 24+ 1 30+ 1 37 + 1 46+ 1 65 + 1 93 + 1* 12 + 1 13 - 0* 94+0
34+ 1 45 + 1 61 + 1 81 + 1 58+ 1 25 -0 10 - 0* 78+0 15 + 1 23 + 1
53 + 1 73 + 1* 95 + 1* 64+ 1 35 -0 10 - 0* 69+0* 15 + 1 24+ 1 36+ 1
4.1 4.2 4.3 4.4
17 + 1 23 + 1 29+ 1 36+ 1
32+ 1 43 + 1 58 + 1 77+ 1
49 + 68 + 90 + 71 +
1.1
24+ 28+ 32 + 36 + 42+
1 1 1 1 1
1 1* 1* 1
173
6.1 Tables of Numerical Results Table 6.2. (continued) The effective principal quantum number no Lin
2.0
3.0
3.5
4.0
4.5
5.0
95 +0 12 + 1 14 + 1 15 + 1 15 + 1
10 - 0 26- 0 47 -0 73 +0 10 + 1 12 + 1 14 + 1 15 + 1 14 + 1 13 + 1
16 - 0 38 - 0 64+0 93 +0 11 + 1 14 + 1 15 + 1 15 + 1 14 + 1 12 + 1
22- 0 48 - 0 78+0 10 + 1 13 + 1 15 + 1 16 + 1 15 + 1 14 + 1 12 + 1
27 -0 57 +0 91 +0 12 + 1 15 + 1 16 + 1 17 + 1 16 + 1 14 + 1 12 + 1
31 - 0 66+0 10 + 1 31 + 1 16 + 1 17 + 1 18 + 1 16 + 1 14 + 1 12 + 1
35 - 0 74+0 11 + 1 14 + 1 17 + 1 18 + 1 18 + 1 17 + 1 15 + 1 12 + 1
1.6 1.7 1.8 1.9 2.0
13 + 1 12 + 1 11 + 1 90+0 63 +0 37 -0 20-0 15 - 0 21 - 0 34-0
13 + 1 10 + 1 82+0 58 + 0 42 -0 36 -0 41- 0 54+0 70+0 84+0
11 + 1 88 +0 66+0 50+0 44-0 46 - 0 54+0 65 +0 74+0 79+0
10 + 1 79+0 60+0 49 -0 46-0 50+0 59 + 0 68+0 73 +0 73 +0
98+0 76+0 59+0 50+0 49 -0 54+0 61 +0 68+0 72+0 70+0
97+0 75 +0 60+0 53 +0 54+0 59+0 66+0 70+0 71 +0 68+0
98 +0 76+0 62+0 55 + 0 57+0 62+0 68 +0 72+0 72+0 67+0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
59+0 71 + 0 76+0 71 +0 60+0 40-0 24-0 16 - 0 16- 0 24-0
88+0 83 + 0 71 + 0 56+0 42 -0 35 - 0 35 - 0 43 -0 56+0 70+0
77 +0 68+0 57 +0 46- 0 40-0 39 - 0 43 - 0 51 + 0 59+0 65 +0
68+0 60+0 50 + 0 42 -0 39-0 40-0 45 -0 52+0 57+0 59+0
64+0 56+0 47 -0 41- 0 39-0 41- 0 45 -0 51 + 0 54+0 55 +0
97+0 75 +0 59+0 51 + 0 51 + 0 57 +0 64+0 7(}+0 71 + 0 69+0 62+0· 54+0 46-0 41 - 0 40-0 42 -0 46-0 51 + 0 53 +0 53 +0
61 +0 52+0 45 -0 40-0 39-0 42 -0 46-0 49-0 51 + 0 51 + 0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
44-0 57+0 64+0 65+0 57+0 41 - 0 26-0 17 -0 15 - 0 20-0
75+0 74+0 66+0 54+0 42 -0 34 -0 33 - 0 38 - 0 50+0 63 +0
66+0 61 + 0 52+0 44 - 0 38 - 0 36-0 39 -0 46- 0 53 +0 59+0
57 + 0 52+0 45 -0 39 - 0 35 - 0 36 - 0 40-0 45 -0 50+0 52+0
53 +0 47 -0 41 - 0 37 - 0 34-0 35 - 0 39-0 43 -0 47 -0 48 -0
50+0 45 -0 40-0 36-0 35 - 0 36 -0 39-0 44-0 46-0 46-0
48-0 42 -0 38 - 0 34-0 33 - 0 33 - 0 38 -0 41- 0 41 - 0 43 -0
60+0 52+0 45 - 0 41- 0 41- 0 44-0 47 - 0 50+0 52+0 50+0 46 -0 42-0 38 - 0 33 - 0 34-0 37 -0 40-0 40-0 43 -0 43 -0
4.1 4.2 4.3 4.4
38-0 50+0 59+0 61 +0
70+0 70+0 64+0 54+0
61 +0 57+0 50+0 42 - 0
51 + 0 47 -0 42 -0 37 - 0
47 -0 43 -0 38 -0 34-0
44-0 41 - 0 36-0 34-0
41 -0 37 -0 33 -0 30-0
39 -0 37 -0 33 - 0 28-0
1.5
2.5
Transition p - d, parameter C K=3 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1
1.2 1.3 1.4 1.5
174
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number no 3.0
3.5
4.0
4.5
5.0
64+0 56+0 51 + 0 49 -0 48 -0
35 + 1 13 + 1 81 + 0 60+0 51 + 0 47 -0 46- 0 46-0 48 - 0 51 + 0
23 + 1 90+0 58+0 48 -0 45 -0 45 -0 47 - 0 49 -0 52+0 56+0
17 + I 68+0 49-0 45 - 0 45 - 0 47 - 0 49- 0 52+0 56+0 62+0
13 + 1 57+0 45 -0 45 - 0 46-0 49 -0 52+0 56+0 61 +0 68 +0
11 + 1 51 + 0 44-0 45 - 0 48 - 0 51 + 0 55 +0 60+0 67+0 76+0
92 +0 47 - 0 44-0 46- 0 49- 0 53 +0 58 + 0 64+0 73+0 84+0
1.6 1.7 1.8 1.9 2.0
62+0 56+0 53 +0 51 + 0 51 + 0 56+0 76+0 10 + 1 89+0 67+0
48 -0 51 + 0 57 +0 67 +0 78 +0 78+0 63 +0 51 + 0 45 -0 43 -0
55 + 0 60+0 66+0 69+0 63 +0 53 + 0 45 - 0 42 - 0 42 - 0 43 - 0
61 + 0 67 +0 71 + 0 70+0 60+0 50+0 44-0 42 -0 42 -0 45 -0
68+0 75 +0 79+0 73 +0 60+0 49 - 0 43 -0 42 -0 43 - 0 47 -0
77 +0 84+0 86+0 75 +0 60+0 48 -0 43 -0 42 - 0 45 -0 49 -0
86+0 94+0 92+0 77 +0 59+0 47 -0 42 -0 43 -0 46-0 53 +0
95+0 10 + 1 98+0 78+0 57 +0 46-0 42 -0 44 -0 49-0 56+0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
60+0 53 + 0 49 - 0 48 -0 48 - 0 51 + 0 63 +0 86+0 90+0 78+0
43 - 0 45 - 0 49 - 0 56+0 65 +0 70+0 64+0 53 + 0 45 - 0 42 -0
46-0 49 -0 54+0 58 +0 59+0 54+0 48 - 0 43 -0 42 - 0 42 -0
48 -0 53 +0 58 +0 62+0 60+0 54+0 47 -0 43 -0 42 -0 43 -0
52+0 58 + 0 65 +0 67+0 62+0 54+0 47 - 0 43 -0 42 -0 44- 0
56+0 64+0 70+0 71 + 0 63 +0 53 +0 46 -0 42 -0 42 -0 45 -0
61 + 0 70+0 77 +0 75 +0 64+0 54+0 45 - 0 42 -0 43 - 0 48 - 0
66+0 77+0 85 +0 78 +0 65 +0 54+0 43 - 0 42 -0 44- 0 49- 0
3.l 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
60+0 52+0 48-0 46-0 47 - 0 49-0 59 + 0 78+0 88+0 71 + 0
42 -0 44-0 47 -0 53 +0 60+0 66+0 63 +0 53 +0 46 -0 42 -0
44-0 47 - 0 50+0 55 +0 56+0 54+0 49 -0 44 - 0 42 - 0 42 - 0
45 -0 49-0 54+0 58 +0 59+0 55 +0 48 -0 44-0 42 -0 42 -0
47 - 0 53 +0 59+0 63 +0 62+0 55 + 0 48 - 0 44-0 42 -0 43 -0
50+0 57+0 64+0 67 +0 62+0 52+0 46-0 43 -0 43 -0 45 -0
53 +0 62+0 69+0 69+0 59+0 48 -0 48 -0 44-0 40-0 44-0
59+0 68+0 86+0 77 +0 77 +0 73 +0 56+0 39 -0 37 -0 46-0
4.1 4.2 4.3 4.4
60+0 52+0 48 - 0 46-0
42 43 46 51
43 - 0 45 -0 49-0 53 +0
44 -0 48 -0 52+0 56+0
46-0 51 + 0 57+0 61 +0
48 - 0 55 +0 61 +0 64+0
50+0 59+0 67+0 71 + 0
47 -0 60+0 63 +0 68+0
LIn
1.5
2.0
2.5
Transition p - d, parameter cp
K=3 O.l 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1
1.2 1.3 1.4 1.5
- 0 -0 -0 +0
6.1 Tables of Numerical Results
175
Table 6.2. (continued) The effective principal quantum number nO' LIn
2.5
3.0
3.5
4.0
4.5
5.0
Transition d - s, parameter C 0.1 0.2 30.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
17 - 0 31 - 0 41 - 0 45 -0 45 -0 41 - 0 34 - 0 27 -0 21 - 0 30 - 0'
33 - 0 60+0 79+0 88+0 87 +0 79+0 66+0 52 +0 40 -0 31 - 0
48 -0 88 + 0 11 + 1 12 + 1 12 + 1 11 + 1 97 +0 76+0 57 +0 13 + I'
62 +0 11 + 1 15 + 1 16 + 1 16 + 1 15 + 1 12 + 1 99+0 74+0 55 +0
76+0 14 + 1 18 + 1 20+ 1 20 + 1 18 + 1 15 + 1 12 + 1 90+0 16 + I'
89+0 16 + 1 21 + 1 24 + 1 24+ 1 22 + 1 18 + 1 14 + 1 10 + 1 76+0
1.4 1.5 1.6 1.7 1.8 1.9 2.0
16 16 17 19 19 19 18 16 14 25 -
0 0 0 0 0 0 0 0 0 O·
26 -0 26 -0 28 -0 31 - 0 33 - 0 33 - 0 31 - 0 28 - 0 24-0 21 - 0
36 - 0 34-0 36 - 0 40-0 43 - 0 43 - 0 41 - 0 37 - 0 32 - 0 33 - O'
44-0 41 - 0 43 -0 48 - 0 51 + 0 52+0 50+0 44-0 38 - 0 33 - 0
51 + 0 47 - 0 49- 0 54+0 59+0 60+0 57+0 51 + 0 44- 0 44 - O·
58 + 0 52+0 54+0 60+0 66+0 67 +0 65 +0 58 +0 49 -0 41 - 0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
13 13 14 15 16 16 15 14 13 14 -
0 0 0 0 0 0 0 0 0 0'
20- 0 20 - 0 22 - 0 23 - 0 24-0 25 - 0 24-0 22 - 0 20- 0 18 - 0
25 - 0 25 - 0 26 -0 29 - 0 31 - 0 31 - 0 30-0 28 - 0 25 - 0 23 - 0
29 -0 29 -0 30 -0 33 - 0 35 - 0 36 - 0 35 - 0 32 - 0 29 -0 26 -0
33 - 0 31- 0 33 - 0 36-0 39 - 0 40 -0 39 - 0 36 -0 32 -0 29- 0
36 -0 34-0 35 - 0 38 - 0 42 -0 43 -0 42 -0 39 - 0 35 - 0 30 - 0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
12 12 13 14 14 14 14 13 12 13 -
0 0 0 0 0 0 0 0 0 0'
18 - 0 18 - 0 19 - 0 20 - 0 21 - 0 21 - 0 21 - 0 20- 0 18 - 0 17 - 0
21 - 0 21 - 0 23 - 0 24 -0 26 - 0 26 -0 26 -0 24 - 0 22 - 0 21 - 0
24-0 24-0 25 - 0 27 -0 29 -0 29 -0 29 -0 27 -0 24 -0 22 -0
26-0 25 - 0 27 -0 29- 0 31- 0 32 - 0 31 - 0 29 - 0 26 -0 25 -0
27 -0 27 - 0 28 -0 30 -0 32 - 0 34 - 0 33 - 0 31 - 0 28 -0 25 - 0
4.1 4.2 4.3 4.4
11 12 12 13 -
0 0 0 0
16 17 18 19 -
19 - 0 19 - 0 20 - 0 22 -0
21 - 0 21 - 0 22 -0 24 -0
22 -0 22 -0 23 - 0 25 - 0
23 -0 23 -0 24 -0 26 -0
1.1
1.2 1.3
0 0 0 0
176
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number no An
2.5
Transition d - s, parameter
({J
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
76+0 63+0 70+0 80+0 92+0 10 + 1 11 + 1 12 + 1 13 + 1 10 -0*
68+0 62+0 72+0 84+0 98+0 11 + 1 13 + 1 14 + 1 14 + 1 12 + 1
1.1
1.4 1.5 1.6 1.7 1.8 1.9 2.0
81 +0 61 +0 52+0 53 +0 59+0 68+0 79+0 92+0 10 + 1 58 + 1*
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 4.1 4.2 4.3 4.4
1.2 1.3
4.0
4.5
5.0
63 +0 63 +0 75+0 89+0 10 + 1 12 + 1 14 + 1 16 + 1 17 + 1 93 + 1*
61 +0 66+0 79+0 95 +0 11 + 1 13 + 1 16 + 1 18 + 1 19 + 1 17 + 1
59+0 68+0 84+0 10+ 1 12 + 1 14+ 1 17 + 1 20+ 1 22+ 1 87 + 1*
59+0 71 +0 88+0 10 + 1 13 + 1 16 + 1 19 + 1 23 + 1 25 + 1 22+ 1
90+0 59+0 47 -0 47-0 56+0 69+0 84+0 96+0 10 + 1 92+0
10 + 1 63+0 47 -0 47 -0 57+0 73 +0 91 +0 10+ 1 11 + 1 22 + 1*
11 + 1 69+0 48 -0 48-0 59+0 77+0 99+0 12 + 1 13 + 1 12 + 1
13 + 1 75+0 49-0 48-0 61 +0 82+0 10+ 1 13 + 1 14+ 1 24 + 1*
15 + 1 81 +0 51 +0 49-0 63 +0 86+0 11 + 1 14 + 1 16 + 1 15 + 1
71 +0 59+0 52+0 51 +0 54+0 62+0 72+0 85+0 97+0 21 + 1*
73+0 55+0 46-0 46-0 52+0 62+0 74+0 85+0 89+0 82+0
82+0 59+0 47 -0 46-0 53 +0 65 -0 80+0 95 +0 10 + 1 12 + 1
10+ 1 68+0 49-0 47-0 55+0 71 +0 92+0 11 + 1 12 + 1 14+ 1
11 + 1 73+0 51 +0 47-0 57+0 75+0 98+0 12 + 1 13 + 1 13 + 1
68+0 58+0 51 + 0 50+0 53+0 60+0 70+0 82+0 96+0 25 + 1*
68+0 53+0 46-0 45 -0 50+0 60+0 71 +0 80+0 84+0 78+0 65 +0 52+0 45 -0 45 -0
75 +0 57+0 46-0 45 -0 51 + 0 62+0 76+0 89+0 96+0 11 + 1 72+0 56+0 46 -0 45 -0
93+0 64+0 48 -0 46-0 54+0 68+0 86+0 10 + 1 11 + 1 10+ 1 84+0 61 +0 48 -0 46-0 52+0 65+0 81 +0 96+0 10+ 1 98+0 79+0 59+0 47 -0 45 -0
92+0 65+0 49-0 46-0 53+0 67+0 86+0 10+ 1 11 + 1 13 + 1 87+0 63+0 49-0 46-0
10+ 1 69+0 50+0 47 -0 54+0 70+0 91 +0 11 + 1 12 + 1 11 + 1 95 +0 67+0 50+0 46-0
66+0 57+0 51 + 049-0
3.0
3.5
6.1 Tables of Numerical Results
177
Table 6.2. (continued) The effective principal quantum number no
An
2.5
3.0
3.5
4.0
4.5
5.0
46+ 1 76+ 1 94+ 1 99+ 1 93 + 1 78 + I· 59 + I· 38 + I· 19 + 1 74+0 49-0 66+0· 10 + I· 14 + 1 17 + I" 17 + 1* 15 + 1* 11 + 1 68+0 37 - 0*
55 + 1 90+ 1 11 +2 11 +2 11 +2 93 + I· 69 + I· 46 + I· 22 +'1 85 +0·
62+ 1 10+2 12 +2 13 +2 12 + 2· 10+2· 79 + I· 53 + I· 26 + I· 97 +0·
55+0 73 +0· 11 + I· 16 + 1 19 + 1* 20 + 1* 18 + 1* 13 + 1 77+0 41 - O·
60+0 78 -0· 12 + I· 17 + I· 21 + I" 22 + I· 20 + I· 15 +1· 88 +0· 45 - 0*-
23 -0 30- O· 44-0* 60+0· 73 +0· 78+0 71 +0 55+0 35 -0 22 - O·
32 - O· 42 - 0* 63 +0· 87+0 10+ 1 11 + 1· 10 + 1· 79+0 48 -0 29-0 24 - O· 31 - O· 46-0· 63+0 77+0 82+0 76+0 59+0 37 -0 23 -0
34 -0· 43 -0· 65 +0· 92+0· 11 + 1· 12 + 1· 11 + I· 89+0· 54+0· 31 - o· 25 - O· 31 - O· 47 - O· 65 +0· 81 + O· 87 +0· 82 +0· 65 +0· 40-0· 24-0·
20 - O· 26 -0· 37 - O· 51 +0·
21- 0 26- O· 38 - O· 52+0
21 - O· 26 - O· 38 -0· 53 +0·
Transition d - p, parameter C ,,=1 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
16 + 1 25 + 1 38 + 1 31 + 1 27 + 1 22 + 1 15 + 1 87+0 44-0 30-0 27 - O· 37 -0· 50+0· 59+0 61 +0 56+0 43 -0 31- 0 24-0 24-0 21 - O· 27 - O· 34- O· 39 - O· 39-0 35 - 0 28-0 22 -0 20-0 23 -0 19-0 24-0 29-0 32-0 31-0 28-0 23 -0 19 - O· 19 - O· 24-0·
4.1 4.2 4.3 4.4
18 - O· 23 -0· 27 -0 29-0
1.1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
27 + 1 44+ 1 54+ 1 57 + 1 53 + 1 44+ 1 33 + 1 21 + 1 10 + 1 45 - O· 34-0· 47 - O· 73 +0· 98+0 11 + 1 11 + 1 99+0 72+0 43 -0 26-0 23 - O· 31 - 0* 45 - O· 60+0 70+0 72+0 63+0 48-0 31 - 0 20-0 19 - O· 25 - 0* 36 - O· 47 -0 55+0 57+0 50+0 38-0 26-0 18 - 0 17 - O· 22 -0· 31 - O· 41-0
37 + 1 62 + 1 75 + 1 79+ 1 74+ 1 62 + 1 46 + I· 29 + I· 14 + 1 59+0 43 -0 60+0 92+0 12 + 1 14 + 1 14 + 1 12 + 1 92+0 53 +0 32 -0 28 -0· 37 - 0* 54+0· 73 +0 86+0 88+0 77+0 57+0 36-0 24-0 22- O· 29 -0· 42 -0· 56+0· 65+0 67+0 59+0 44-0 29-0 21 - 0 20 -0· 26 - O· 36- O· 48-0
30- O· 39 -0· 59+0· 81 +0 98+0 10 + 1 94+0 73 +0 45 -0 27 -0
178
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number no LIn
2.5
3.0
Transition d - p, parameter ,,=1 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 Ll
1.2 1.3
1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 4.1 4.2 4.3 4.4
13 + 1 18 + I 24+ I 31 + 1 40+ I 50+ I 56+ I 43 + 1 14 + I 13 - 0 10 - 0* 15 - O· 61 +0* 11 + 1 18 + I 22 + I 20+ I 11 + I 25 -0 10-0 10-0* 13 - 0* 48 -0* 92+0* 13 + 1 15 + 1 12 + 1 52+0 10-0 10-0 10-0 14 -0 45 -0 83 +0 11 + 1 12 + 1 87+0 30 -0· 10 - O· 10 - O· 10 - 0* 14 - O· 44-0 78+0
14 + 1 20+ I 27 + I 36+ 1 46+ I 60+ I 76+ I 85 + I 55 + I 12 + I· 10 - 0* 10- 0* 61 + O· 13 + I 22 + I 33 + I 44+ I 45 + I 26+ 1 67+0 10 - O· 10 - O· 46 -0* 10 + I 18 + 1 27 + 1 35 + 1 34+ I 19 + 1 51 +0 10 -0· 10 - O· 40 - 0* 96+0 16 + I 24+ I 31 + I 29+ I 16 + I 43 -0 10 - O· 10 - O· 37 -0 90+0
3.5
4.0
4.5
5.0
16 + 1 25 + 1 34+ 1 46+ 1 61 + 1 80+ 1· 10+2· 12 + 2* 88+ 1 18 + 1 11- 0 12 - 0* 74+0· 16 + 1 29+ 1 45 + 1* 62 + 1· 70+ 1 42 + 1 10 + I· 10 - O· 10 - O· 54+0* 13 + 1 24+ I 37 + 1 50+ 1 54+ 1 31 + 1 83 +0 10-0 10- O· 48 -0* 11 + 1* 21 + 1* 33 + 1 45 + 1 46+ 1 26+ 1 72+0 10- O· 10- 0* 44-0* 11 + I·
17 + I 27 + I 37 + I 51 + 1 68+ I 90 + I· II +2* 14 +2· 10+2 19 + 1·
19 + 1 29+ 1 41 + 1 56+ 1 75 + I· 10 +2· 12 +2* 15 +2* 11+2* 23 + 1* 21 - 0 17 - O· 87 +0* 20 + 1* 36 + I· 56 + I· 79 + 1· 94 + 1· 56 + I· 14 + I·
qJ
15 + I 23 + I 31 + 1 41 + 1 53 + 1 70 + 1 90 + I· 10 + 2* 64+ 1 12 + I 10 - 0 11- 0 68+0 15 + 1 26 + 1 39 + 1 52+ 1 53 + 1 27 + I 61 +0 10 - 0* 10 - O· 51 + O· 12 + 1 21 + I 32 + 1 41 + I 38+ 1 19 + I 41-0 10 - 0* 10-0* 45 -0* 10 + 1* 19 + I 28 + 1 36+ 1 32 + 1 15 + 1 31 - 0 10 - O· 10 - O· 42 - 0* 10 + 1
15 - 0 15 - O· 80+0* 18 + 1 32 + 1* 51 + 1· 70+ 1· 80+ I 46+ 1 11 + 1* 10 - O· 10- 0* 59+0· 14+ I 26+ 1 41 + 1· 57 + 1* 61 + I 33 + 1 83+0 10- O· 10-0* 52+0· 13 + 1* 23 + 1 37 + I 50+ 1 51 + 1 27+ 1 69+0 10-0 10- 0* 48 - O· 12 + I
13 -0· 10 -0· 64+0* 15 + 1· 29 + 1* 46+ 1* 65 + 1* 72 + I· 41 + 1· 11 + 1* 10 - O· 10 - 0* 56+0· 14 + 1· 26 + 1* 41 + 1· 58 + 1* 62 + 1· 35 + 1* 96+0· 10 - O· 10 -0· 51 + O· 13 + 1*
179
6.1 Tables of Numerical Results Table 6.2. (continued) The effective principal quantum number no
Lin
2.5
3.0
3.5
4.0
4.5
5.0
Transition d - p, parameter C ,,=3 13 -0 24-0 33 -0 39-0 42-0 42-0 39-0 34-0 29 -0 25 -0 22-0 20-0 20-0 21- 0 22-0 23 -0 23 -0 22-0 20-0 19 -0
18 - 0 34-0 46-0 55 +0 59+0 58+0 53 +0 46-0 39-0 33 -'- 0
23 -0 43 -0 59+0 70+0 74+0 72+0 66+0 57+0 48 -0 40-0
27-0 51 +0 70+0 83+0 88+0 86+0 78+0 68+0 56+0 46-0
1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
74 -1 13 - 0 18 - 0 22-0 23 -0 23 -0 22-0 20-0 17 - 0 15 - 0 13 -0 13 -0 13 -0 13 -0 14 - 0 15 -0 15 -0 14 -0 14 -0 13 -0
28 26 26 27 28 29 29 27 25 23
39-0 35 -0 34-0 35 -0 37 -0 37 -0 37 -0 36-0 33 -0 30-0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
12 -0 12 -0 12 - 0 12 -0 12 -0 13 -0 13 -0 13 -0 13 -0 12 -0
18 -0 17 -0 17 -0 18 -0 19 -0 19 -0 19 -0 19 -0 18 -0 17 -0
22 -0 21 - 0 21 - 0 21 - 0 22 -0 23 -0 23 -0 22 -0 21 - 0 20-0
34-0 31- 0 30-0 31- 0 33 -0 34-0 33 -0 32-0 29-0 27 -0 25 -0 24-0 24-0 24-0 25 -0 26-0 26-0 25 -0 24-0 23 -0
32-0 59+0 82+0 96+0 10+ 1 99+0 90+0 77+0 64+0 52+0 44-0 39-0 38 -0 39-0 40-0 41- 0 41- 0 39-0 36-0 32-0
27-0 26-0 26-0 26-0 27-0 28-0 28-0 27-0 26-0 24-0
29-0 28-0 28 -0 28-0 29-0 29-0 29-0 29-0 27 -0 24-0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
11-0 11-0 11-0 12 -0 12 -0 12 -0 12 -0 12 -0 12 -0 12 -0
16 -0 16 -0 16 -0 16 -0 17 -0 17 -0 17 -0 17 - 0 16 -0 16 -0
19 -0 19 - 0 18 - 0 19 - 0 20-0 20 -0 20 -0 20-0 19 - 0 18 - 0
21- 0 21- 0 21-0 22-0 22-0 23 -0 23 -0 23 -0 21- 0 20-0
22-0 21- 0 21- 0 22-0 23 -0 23 -0 24-0 24-0 22-0 22-0
23 -0 23 -0 23 -0 23 -0 24-0 24-0 25 -0 23 -0 24-0 22 -0
4.1 4.2 4.3 4.4
11-0 11-0 11-0 11-0
15 - 0 15 -0 15 -0 16 - 0
18 17 17 17 -
20-0 20-0 20-0 20-0
21-0 20-0 19 - 0 20-0
20-0 19 - 0 18 - 0 18 - 0
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
-0 -0 -0 -0 -0 -0 -0 -0 -0 -0
0 0 0 0
180
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.2. (continued) The effective principal quantum number no
An
2.5
3.0
Transition d - p, parameter ,,=3 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
22+ 1 81 +0 52+0 47 -0 49-0 53 +0 58+0 60+0 62+0 61 +0
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
33 + 1 11 + 1 67+0 52+0 51 +0 57+0 66+0 76+0 88+0 77+0 68+0 58+0 53+0 53+0 57+0 62+0 66+0 68+0 66+0 61 +0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
3.5
4.0
4.5
5.0
89+0 46-0 45 -0 47 -0 51 +0 55 +0 61 +0 69+0 77+0 83+0 82+0 72+0 59+0 48 -0 43 -0 43 -0 44-0 51 +0 57+0 61 +0
qJ
12 + 1 54+0 45 -0 46-0 49-0 52+0 55 +0 60+0 65+0 69+0
10 + 1 49-0 44-0 47-0 49-0 53+0 58+0 64+0 71 +0 76+0
59+0 56+0 52+0 50+0 48 -0 47-0 47 -0 47-0 48-0 49-0
16 + 1 63 +0 46-0 46-0 48 -0 52+0 55+0 58+0 61 +0 63 +0 62+0 58+0 52+0 47 -0 44-0 42 -0 43 -0 45 -0 48 -0 51 +0
68+0 62+0 54+0 47-0 43 -0 42-0 43 -0 47 -0 51 + 0 55+0
75+0 67+0 57+0 48-0 43 -0 42-0 44-0 48-0 54+0 59+0
55 +0 52+0 52+0 54+0 59+0 63+0 66+0 65+0 62+0 57+0
51 +0 52+0 51 +0 50+0 48 -0 46-0 45 -0 44-0 45 -0 47 -0
53 +0 53 +0 50+0 47 -0 43 -0 42 -0 42 -0 44-0 46-0 49-0
57+0 56+0 52+0 48 -0 43 -0 42-0 43 -0 45 -0 47 -0 51 +0
63 +0 64+0 60+0 51 +0 45 -0 42-0 43 -0 48-0 49-0 52+0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
52+0 50+0 51 +0 55+0 68+0 64+0 65+0 64+0 68+0 55 +0
49-0 51 +0 50+0 49-0 47-0 45 -0 44-0 43 -0 44-0 46-0
51 +0 51 +0 49-0 46-0 44-0 42 -0 42 -0 43 -0 45 -0 48 -0
53 +0 53 +0 50+0 48-0 44-0 41-0 42-0 44-0 47-0 50+0
61 +0 59+0 55+0 49-0 44-0 43 -0 42-0 46-0 51 +0 53+0 54+0 54+0 53+0 48-0 41-0 38-0 45-0 45-0 48-0 54+0
4.1 4.2 4.3 4.4
50+0 49-0 51 +0 55+0
48-0 50+0 50+0 49-0
50+0 50+0 50+0 47 -0
54+0 55+0 53+0 47 -0
59+0 58+0 53+0 52+0
54+0 39-0 41-0 41-0
1.1
57+0 62 +0 71 +0 54+0 53+0 52+0 50+0 44-0 53+0 60+0
181
6.1 Tables of Numerical Results
Table 6.3. Transitions with no change of spin LIS = 0; excitations rate coefficients (va) in the Born approximation. Parameters A and x The effective principal quantum number
LIn 0.5
1.0
1.5
2.0
no
2.5
3.0
3.5
4.0
4.5
5.0
Transition s - s, parameter A" 0.6 0.7 0.8 0.9 1.0
10+2 12 + 2 12 + 2 10 +2 80 + 1
10 + 2 11 +2 10+2 80 + I 51 + I
11 +2 11 +2 10+2 72+ I 41 + I
13 +2 12 + 2 94+ I 62 + I 32 + I
13 +2 11 +2 88 + I 54 + I 26 + I
14 +2 11 +2 81 + I 47 + I 22 + I
14+ 2 11 +2 75 + I 42 + 1 18 + I
14+2 10+2 70 + I 37 + 1 61 + I
14+2 10+2 65 + I 34+ 1 14 + I
14 +2 10+2 61 + I 31 + 1 12 + I
1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
29 + I 67+0 21 - 0 11 + I 35 + I 64 + I 91 + I 10+2 10+2 85 + 1
23 + I 65 +0 32 -0 11 + I 29 + I 52 + I 69 + I 74+ I 65 + I 45 + 1
17 + I 54+0 54+0 17 + I 37 + I 57 + I 68 + I 66+ I 53 + I 34 + 1
12 + I 50+0 80+0 23 + I 44 + I 60+ I 64+ I 56 + I 41 + I 23 + 1
10 + I 49 -0 10 + I 28 + I 48 + I 59 + I 57 + I 47 + I 32 + I 17 + 1
83 + 0 50+0 12 + I 32 + I 49+ I 55 + I 51 + I 39 + I 25 + 1 13 + 1
70+0 51 + 0 14 + I 35 + I 49 + I 51 + I 45 + I 34 + I 21 + 1 10 + 1
61 +0 53 +0 15 + I 36 + I 47 + I 47 + I 40 + I 29+ I 17 + 1 88 +0
54+0 54+0 16 + 0 36 + I 45 + I 44+ I 36 + I 25 + I 15 + 1 74+0
49-0 55 + 0 17 + I 36 + I 43 + I 40 + I 33 + I 23 + I 13 + I 63 +0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
30 + 1 80+0 19 -0 94+0 30 + 1 59 + 1 86 + 1 10 +2 10+2 88 + I
22 + 1 74+0 30 -0 84+0 23 + 1 44 + 1 61 + 1 67 + 1 61 + I 43 + I
15 + 1 56+0 45 -0 12 + 1 29+ 1 47 + 1 58 + 1 59 + 1 48 + I 32 + I
10 + 1 46 -0 60+0 16 + 1 33 + 1 47 + 1 52 + 1 47 + 1 35 + I 20 + I
78+0 41 - 0 70+0 19 + 1 35 + 1 44 + 1 44 + 1 37 + 1 26 + I 15 + I
60+0 38 - 0 77 +0 20 + 1 34 + 1 39 + 1 37 + 1 29+ 1 20+ I 10 + I
48 -0 35 - 0 80+0 20+ 1 31 + 1 35 + 1 31 + 1 24+ 1 15 + I 84+0
40- 0 33 -0 82+0 20+ 1 29+ 1 30 + 1 27 + 1 20+ 1 12 + I 66+0
34-0 32 -0 82+0 19 + 1 26+ 1 27 + 1 23 + I 17 + 1 10 + I 54+0
29- 0 30- 0 81 + 0 18 + 1 24 + 1 24+ 1 20+ 1 14 + 1 89+0 45 -0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
30 + I 84+0 19 - 0 87 +0 28 + I 57 + I 84+ I 10+2 10+2 90+ I
22 + I 76+0 30 - 0 76+0 21 + I 41 + I 58 + I 65 + I 59 + I 42 + I
14 + I 56+0 42-0 11 + I 26 + I 43 + I 55 + I 55 + I 46 + I 31 + I
97+0 44-0 53 +0 14 + I 29 + I 42 + I 47 + I 43 + I 32 + I 19 + I
69+0 38 - 0 60+0 16 + I 30 + I 38 + I 39 + I 33 + I 23 + I 13 + I
51 + 0 33 - 0 62+0 16 + I 28 + I 33 + I 31 + I 25 + I 17 + I 97+0
40-0 29-0 62+0 16 + I 25 + I 28 + I 26+ I 20+ I 13 + I 73+0
32 -0 26-0 60+0 15 + I 22 + I 24+ I 21 + I 16 + I 10 + I 56+0
26-0 24-0 58+0 14 + I 20+ I 21 + I 18 + I 13 + I 86+0 45 -0
22+0 22 -0 56+0 13 + I 18 + I 18 + I 15 + I II + I 71 +0 37 - 0
4.1 30+ I 22 + I 14 + I 93 +0 64+0 47 -0 4.2 85 +0 77+0 56+0 43 - 0 36- 0 30- 0 4.3 19 - 0 30-0 41- 0 51 + 0 55 +0 55 +0 4.4 84+0 72+0 10 + I 13 + I 14 + I 14 + I a This table can be applied to transitions between the configurations ns-n's
35 - 0 28 -0 22 -0 19 - 0 26- 0 23 -0 20 -0 19 - 0 53 +0 50+0 47 -0 44-0 13 + 1 12 + I 11 + I 10 + I levels of two different electronic
182
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.3. (continued) The effective principal quantum number no Lin
0.5 1.0 1.5 2.0 Transition s - s, parameter X
0.6 0.7 0.8 0.9 1.0
13 + 14 + 15 + 15 + 16 +
1 I 1 1 1
15 + 16 + 17 + 17 + 16 +
1 1 1 1 1
17 + 1 17 + 1 17 + 1 16+ 1 14+ 1
17 + 17 + 16 + 14 + 11 +
I 1 1 1 1
2.5
3.0
3.5
4.0
4.5
5.0
17 + I 16 + 1 14 + I 12 + I 90+0
16 + I 15 + 1 13 + 1 10 + 1 72+0
15 + I 13 + 1 11 + 1 87+0 58+0
14+ I 12 + 1 10 + 1 74+0 47-0
13 + I 11 + 1 88+0 63 +0 39-0
12 + I 10+ 1 78+0 54+0 32-0
1.1 15 + 1 13 + 1 99+0 74+0 57+0 44-0 35 -0 29-0 24-0 20-0 1.2 88+0 68+0 53 +0 48 -0 47 -0 48-0 49-0 50+0 50+0 50+0 1.3 26-0 39 -0 64+0 98+0 13 + 1 15 + 1 17+ 1 18 + 1 19 + 1 19 + 1
1.4 1.5 1.6 1.7 1.8 1.9 2.0
72+0 10+ 1 13 + 1 14 + 1 15 + 1 16 + 1 16 + 1
91 +0 14 + 1 17 + 1 18 + 1 19 + 1 19 + 1 18 + 1
14 + 20+ 22 + 22 + 21 + 19 + 16 +
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
16 + 1 99+0 26-0 65 +0 10 + 1 13 + 1 14 + 1 15 + 1 16 + 1 16 + 1
14 + 1 81 +0 40-0 82+0 13 + 1 17 + 1 19 + 1 20+ 1 19 + 1 18 + 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
16 + 1 10 + 1 26-0 63 +0 10+ 1 12 + 1 14 + 1 15 + 1 16 + 1 16 + 1
4.1 4.2 4.3 4.4
16 + I 10 + 1 26-0 62+0
I I I 1 1 I I
25 + 1 28 + I 26 + 1 22+ 1 18 + 1 14 + 1 10+ 1
28 + 1 29+ 1 25 + 1 20+ 1 16 + 1 12 + 1 82+0
30+ 1 28+ 1 23 + 1 18 + 1 13 + 1 10+ 1 66+0
30+ 1 27 + 1 21 + 1 16 + 1 11 + 1 83+0 53+0
29 + 1 25 + 1 19 + I 14+ 1 10 + 1 70+0 43 -0
28 + 1 23 + 1 17 + 1 12 + 1 90+0 60+0 36-0
11 + 1 63 +0 62+0 13 + 1 20+ 1 23 + 1 23 + 1 22+ 1 20+ 1 16 + 1
86+0 56+0 93+0 20+ 1 27 + I 27 + I 25 + 1 22 + 1 18 + 1 13 + 1
66+0 54+0 11 + 1 25 + 1 31 + 1 28 + 1 24+ 1 19 + 1 15 + 1 10+ 1
52+0 52+0 13 + 1 28 + 1 32 + 1 27 + 1 22 + 1 17 + 1 12 + 1 86+0
42-0 50+0 14+ 1 30+ 1 31 + 1 25+ 1 19+ 1 14+ 1 10+ 1 69+0
34-0 48 -0 15 + 1 29+ 1 29+ 1 23 + 1 17 + 1 12 + 1 87+0 56+0
28 -0 46-0 15 + 1 28+ 1 27 + 1 20+ 1 15 + 1 10+ 1 74+0 46-0
23 -0 45 -0 15 + 1 27 + 1 24+ 1 18 + 1 13 + 1 95 +0 63 +0 38 -0
15 + 1 86+0 41- 0 79+0 13 + 1 17 + 1 19 + 1 20+ 1 20+ 1 18 + 1
11 + 1 68+0 63 +0 13 + 1 20+ 1 23 + I 24+ 1 23 + 1 20+ 1 17 + 1
90+0 60+0 93 +0 20+1 28 + I 28 + 1 26+ 1 22 + 1 18 + 1 14 + 1
70+0 57+0 11 + 1 25 + 1 32+ 1 30+ 1 25 + 1 20+ 1 15 + 1 11 + 1
55 +0 54+0 13 + 1 28 + 1 33 + 1 28 + 1 23 + 1 17 + 1 13 + 1 88+0
44-0 51 +0 14+ 1 29+ 1 32 + 1 26+ 1 20+ 1 15 + 1 10+ 1 71 +0
36-0 48-0 14 + 1 29+ 1 30+ 1 23 + 1 17 + 1 13 + 1 90+0 57+0
30-0 46-0 14 + 1 27 + 1 27 + 1 21 + 1 15 + 1 11 + 1 76+0 47-0
25 -0 43 -0 14+ 1 26+ 1 25 + 1 19 + 1 14 + 1 98+0 64+0 39-0
15 + 1 88+0 41- 0 78+0
12 + 1 70+0 63+0 13 + 1
93 +0 62+0 93 +0 20+ 1
72+0 58+0 11 + 1 25 + 1
57+0 55 +0 12 + 1 28 + 1
46-0 52+0 13 + 1 28+ 1
37 -0 48-0 13 + 1 28+ 1
31-0 46-0 13 + 1 27 + 1
26-0 43 -0 13 + 1 25 + 1
1 1 1 1 1 1 1
20 + 25 + 25 + 23 + 20+ 17 + 13 +
Table 6.3. (continued) The effective principal.quantum number Lin
2.5
3.0
3.5
4.0
4.5
5.0
14 + 1 20 + 1 30 + 1 37 + 1 46+148+1 58 + 1 52 + 1 64 + 1 51 + 1 62+144+1 53 + 1 34 + 1 40+123+1 25+113+1 13 + 1 66 + 0*
25 + 1 40+ 1 46+ 1 46+ 1 41 + 1 33 + 1 23 + 1 14 + 1 79 + O· 41 - 0
28+ 1 41 + 1 44+ 1 41 + 1 34+ 1 26+ 1 17 + 1 10 + 1* 57 + 0* 33 -0
31 + 1 41 + 1 42 + 1 37 + 1 30+ 1 21 + 1 14 + 1 81 + 0* 44 - 0* 30-0
33 + 1 41 + 1 40+ 1 34+ 1 26+ 1 18 + 1 11 + 1* 66 + 0* 37 - 0* 28-0
35 +1 41 + 1 37 + 1 31 + 1 23 + 1 15 + 1 97 + 0* 55 + 0* 33 - 0* 28 -0
36+ 1 40+ 1 35 + 1 28 + 1 20+ 1 13 + 1* 84 + 0* 48 - 0* 30 - 0* 27 - 0*
0.5 1.0 1.5 2.0 Transition s - p, parameter A
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
89+ 95 + 91 + 77+ 57 +
1 1 1 1 1
no
1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
19 + 2 32 + 1 14 + 2 13 + 1 89 + 1 37 - 0* 44 + 1 52 + 0 15 + 1 29 + 1 21 - 0 45 + 1 34 - 0 56 + 1 14 + 1 61 + 1 25+158+1 34 + 1 49 + 1
66 + 0 34 - 0 32 - 0 43 - 0* 73 + 0 21 + 1 29 + 1 28 + 1 37 + 1 27 + 1 36 + 1 24 + 1 33 + 1 20 + 1 27 + 1 15 + 1 19+199+0 11 + 1 55 + 0
31 - 0 64 + 0* 22 + 1 22 + 1 19 + 1 16 + 1 12 + 1 88 + 0 54+0 32 - 0
33 - O· 86 + 0 18 + 1 17 + 1 14 + 1 12 + 1 89 + 0 60 + 0 37-0* 24 - 0
36 - 0* 10 + 1 15 + 1 13 + 1 11 + 1 90 + 0 65 + 0 43 - 0* 27-0* 20 - 0
38 - 0* 10 + 1 13 + 1 11 + 1 92 + 0 71 + 0 51 + O· 43 - O· 22-0* 18 - 0
40 - 0* 10 + 1 11 + 1 94 + 0 76 + 0 58 + 0 41 - O· 27 - 0* 19-0* 17 - 0
41 - O· 97 + 0 94 + 0 80 + 0 64 + 0 49 - O· 34 - O· 23 - 0* 17-0* 16 - 0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
13 +2 30 + 1 10 +2 14 + 1 73+146-0 41 + 1 32 - 0 16 + 1 22 + 1 37 - 0 39 + 1 75 -1 49 + 1 10+154+1 18 + 1 54 + 1 26+146+1
66+031-0 32-031-0 44-011+1 23+122+1 32 + 1 23 + 1 32 + 1 20 + 1 29 + 1 17 + 1 24+113+1 17 + 1 88 + 0 10+151+0
24-0 39 - O· 15 + 1 17 + 1 15 + 1 13 + 1 10 + 1 72+0 46-0 28- 0
23 - O· 46 - O· 13 + 1 12 + 1 11 + 1 91 +0 69+0 48-0 31 - O· 21- 0
23 - O· 52 + 0 10 + 1 97+0 82+0 65+0 49-0 33 - O· 22 - O· 17 - 0
23 - O· 53 +0 84+0 75 +0 63 +0 50+0 37 - O· 25 - O· 17 - O· 14 - 0
23 - O· 52+0 67+0 60+0 50+0 39 -0 29 - O· 20 - O· 14 - O· 13 -0
22 - 0* 48 -0 55+0 49-0 41- 0 32 - O· 23 - O· 16 - 0* 12 - O· 12 -0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
11 + 2 29 + 1 96 + 1 14 + 1 68 + 1 50 + 0 39 + 1 29 - 0 17 + 1 19 + 1 44 - 0 36+ 1 65-146+1 82 +0 51 + 1 15 + 1 51 + 1 23 + 1 45 + 1
66 + 32 38 21 + 30 + 30 + 27 + 22 + 16 + 10 +
0 0 0 1 1 1 1 1 0 0
22-0 32 -0· 12 + 1 15 + 1 14 + 1 11 + 1 91 +0 65+0 42 -0 26-0
20-0 36 - O· 11 + 1 11 + 1 96+0 79+0 61 +0 43 -0 28 - O· 19 - 0
19 - 0* 38 - 0 86+0 81 +0 69+0 55+0 42-0 29 - O· 20 - O· 15 - 0
18 - O· 38-0 66+0 61 +0 52+0 41- 0 31-0· 22 - O· 15 - 0* 12 - 0
17 - 0* 36-0 52+0 47 -0 40-0 32 -0 24-0· 17 - O· 12 - 0 11-0
16 - 0* 34-0 42-0 38-0 32-0 25 -0· 19-0· 14 - O· 10-0 10-0
4.1 4.2 4.3 4.4
10 +2 91 + 1 65 + 1 38 + 1
66+028-0 33 - 0 27 - 0 35 - 0 76 + 0 19 + 1 19 + 1
20-0 29-0· 10 + 1 14 + 1
18 - 0 31-0 97+0 10 + 1
16 - O· 32-0 76+0 72+0
15 - 0* 31- 0 57+0 53+0
14 - 0* 30-0 45 -0 41-0
13 - O· 27 -0 35 -0 32-0
29 + 1 14 + 1 52 +0 28 - 0
0 0 0 1 1 1 1 1 1 1
29 28 87 + 20 + 21 + 19 + 16 + 12 + 84 + 49 -
Table 6.3. (continued) The effective principal quantum number no L1n 0.5
1.0
1.5
2.0
2.5
3.0
3.5
4.0
4.5
5.0
Transition s - p, parameter X 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
71 + 0 63 +0 56 + 0 48 - 0 41 - 0
l.l 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
10+ 1 99+0 87+0 75 +0 64+0 54 + 0 44 - 0 35 - 0 26 - 0 18 - 0
10 + 1 92+0 76+0 62+0 51 +0 40-0 31 - 0 23 -0 16 - 0 10 - O·
10+ 1 84+0 66+0 52+0 40-0 30-0 22-0 15 - 0 10- O· 10-0
10 + 1 77+0 58+0 44-0 32-0 23 -0 16 - 0 10 - O· 10 -0' 10-0
97+0 70+0 51 + 0 37 -0 26-0 18 - 0 12 - 0 10 - O· 10 - O· 10 - 0
93 +0 64+0 45 -0 31 - 0 22 -0 14 - 0 10 - O· 10 -0' 10 - O· 10-0
89+0 59+0 40-0 27 -0 18 - 0 ll- 0 10 - O· 10 - O· 10 -0' 10-0
85 +0 54+0 35 - 0 23 -0 15 - 0 10 - O· 10 - O· 10 - O· 10- O· 10 - O·
61+031-0 55 + 0 20 - 0 48 - 0 11 - 0 40 - 0 81 + 0 29 - 0 31 + 1 12 - 0 18 + 1 26 + 1 11 + 1 14 + 1 82 + 0 87 + 0 63 + 0 67 + 0 50 + 0
12-0 13 - 0 11 + 1* 38 + 1 21 + 1 12 + 1 78 + 0 53 + 0 36 - 0 24 - 0
10- 0 44 - 0* 42 + 1 30 + 1 15 + 1 86+0 54+0 35 - 0 23 -0 14 - 0
15 - 0 96 + 0* 39 + 1 21 + 1 10 + 1 62+0 38-0 23 -0 15 - 0 II - 0
23 - O· 15 + 1 30 + 1 16 + 1 81 +0 46-0 27 - 0 17 - 0 II - 0* 10-0
30 - O· 19 + 1 23 + 1 12 + 1 62+0 35 - 0 20-0 12 - 0* 10 - O· II - 0
37 - O· 21 + 1 18 + 1 93 +0 48 -0 27 -0 15 - O· 10 - O· 10 - 0* 11 - o·
43 - O· 20 + 1 14 + 1 73 +0 38 -0 21-0 12 - O· 10 - O· 10 - O· 12 -0
47 - O· 17 + 1 II + 1 59+0 30-0 16 - 0* 10 - O· 10 - O· 10 - O· 12 - 0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
65 + 57 + 49 40 30 16 27 23 + 10 + 73 +
0 0 0 0 0 0 0 1 1 0
36 24 13 36 35 + 23 + 13 + 92 + 69 + 53 +
0 0 0 0 1 1 1 0 0 0
16 13 61 + 45 + 28 + 15 + 92 + 60 + 40 26 -
0 0 1 1 1 1 0 0 0 0
12 - 0 34-0 27 + 1 37 + 1 20+ 1 10 + 1 64+0 40-0 26 - 0 16 - 0
16 - 0 68 +0* 41 + 1 27 + 1 14 + 1 77+0 45 -0 27 -0 17 - 0 13 -0
22 - O· 10+1* 35 + 1 20+ 1 10 + 1 56+0 33 - 0 20-0 13 - 0* II - 0
29 - O· 13+1 27 + 1 15 + 1 78+0 42 -0 24-0 15 - 0* 10 - 0* 12 - 0
34 -0* 15 + 1 21 + 1 II + 1 60+0 33 -0 19 - O· 11 - 0* 10 - 0* 12 -0
38 - O· 15 + 1 16 + 1 90+0 47 -0 26 -0 14 - O· 10 - O· 10 - 0* 13 -0
41 - O· 15 + 1 13 + 1 72+0 37 - 0 20 - O· 11 - O· 10 - O· 10 - O· 13 - 0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
66 + 57 + 49 40 30 17 13 28 + 11 + 78 +
0 0 0 0 0 0 0 1 1 0
39 25 14 28 35 + 25 + 14 + 97 + 71 + 54 +
0 0 0 0 1 1 1 0 0 0
17 14 50 + 45 + 31 + 17 + 10 + 64 + 42 27 -
0 0 0 1 1 1 1 0 0 0
13 - 0 32 - 0 22 + 1 40 + 1 22 + 1 11 + 1 69+0 43 -0 27 -0 17 - 0
17 - 0 61 + O· 37 + 1 30+ 1 16 + 1 85 +0 49-0 30-0 18 - 0 14- 0
23 -0 92 +0' 36 + 1 22+ 1 II + 1 62+0 36-0 22 -0 14 - O· 12 - 0
28 - O· II + 1 28 + 1 16 + 1 87+0 47 -0 27 -0 16 - 0* 11 - 0* 13 - 0
33 - O· 13 + 1 22+ 1 12 + 1 67+0 36-0 21 - O· 12 - 0* 10 - O· 13 - 0
37 - O· 14 + 1 17 + 1 99+0 52+0 28 -0 16 - O· 10 - O· 10-0 14 -0
40 - O· 13 + 1 14 + 1 78+0 42 -0 23 - 0* 13 - O· 10 - 0* 10-0 14 - 0
32 12 + 23 + 13 +
36 -0' 13 + 1 18 + 1 10 + 1
38 - O· 13 + 1 14 + 1 83 +0
4.167+040-0 4.2 57 + 0 26 - 0 4.3 49 - 0 15 - 0 4.4 40 - 0 25 - 0
18-0 14 - 0 17 - 0 14 - 0 31 - 0 59 +0' 45 - 0 19 + 1 35 + 1 43 + 1 42 + 1 32 + 1
23 -0 28 - O· 86+0 11 + 1 35 + 1 29 + 1 23 + 1 17 + 1
O· 1 1 1
Table 6.3. (continued) The effective principal quantum number no LIn 0.5
2.5
3.0
3.5
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
93 + 1 12 +2 13 +2 14+2 13 +2
36-0 16 + 1 38+ I 64+ 1 89+ 1 10+2 11 +2 11 +2 97 + 1 74+ 1
73+0 28+ 1 55 + 1 79+ 1 96+ 1 10+2 96+ 1 82+ 1 63 + 1 43 + 1
11 + 38 + 66+ 86+ 94+ 91 + 80+ 63 + 45 + 28 +
27+2 19+2 11 +2 55 + 1 15 + 1
19+2 18+2 16+2 11 +2 74+ 1 30+ 1 89+0 86+0 36+ 1 79+ 1
10+2 76+ 1 45 + 1 22+ 1 97+0 84+0 26+ 1 61 + 1 84+ 1 92+ 1
50 + 1 29+ 1 14 + 1 84+0 10 + 1 30 + 1 60+ 1 70+ 1 68 + 1 58 + 1
1.0 1.5 2.0 Transition s - d, parameter A
1.1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
4.0
4.5
5.0
I I I 1 1 1 1 1 1 1
15 + 1 47+ 1 74+ I 88 + I 89+ 1 80+ 1 66+ 1 49+ 1 33 + 1 20+1
20+ I 55 + 1 79+ 1 87 + 1 83 + 1 71 + 1 56+ 1 39+ 1 25 + 1 15 + 1
24+ I 61.+ 1 81 + 1 . 84+ 1 77 + 1 63 + 1 47+ 1 32+ 1 20+ 1 12 + 1
26+ 1 14 + 1 86+0 91 +0 20+ 1 46+ 1 56+ 1 53 + 1 44+ 1 34+ 1
16 + 1 96+0 80+0 12 + 1 30+ 1 46+ 1 46+ 1 39+ 1 31 + 1 22+ 1
11 + 1 80+0 88+0 17 + 1 34+ 1 40+ 1 36+ 1 29+ 1 21 + 1 15 + 1
94+0 75+0 10+ 1 20+ 1 33 + 1 34+ 1 29+ 1 22 + 1 16+ 1 17 + I"
81 +0 76+0 11.+ 1 22+ 1 30+ 1 28+ 1 23 + 1 17 + 1 12 + 1 86+0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
49+2 26+2 10+2 25 + 1 66 -1 69+0 24+ 1 38 + 1 43 + 1 40+ 1
31- 0 36 + 1 91 + 1 14+2 16+2 16+2 13+2 93 + 1 51 + 1 19 + 1
10+2 12+2 11 +2 10+2 75 + 1 37 + 1 13+ 1 65 +0 19 + 1 55 + 1
85 + 1 68 + 1 47 + 1 27 + 1 13 + 1 75+0 12 + 1 39+ 1 68 + 1 81 + 1
43 + 1 29+ 1 16 + 1 93 +0 77+0 15 + 1 39+ 1 58 + 1 59 + 1 53 + 1
23 + 1 14+ 1 87+0 70+0 10 -i- 1 25 + 1 42+ 1 43 + 1 38 + 1 30+ 1
14 + 1 89+0 65+0 76+0 14 + 1 29+ 1 35 + 1 32 + 1 26+ 1 19 + 1
97+0 66+0 61 +0 89+0 17 + 1 27 + 1 27 + 1 23 + 1 18 + 1 12 + 1
73+0 56+0 61 +0 10 + 1 18 + 1 23 + 1 21 + 1 17 + 1 13 + 1 93+0
60+0 51 +0 63 +0 10 + 1 17 + 1 19 + 1 17 + 1 13 + 1 10 + 1 70+0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
23+2 14+2 63 + 1 17 + 1 91-1 35 -0 14 + 1 24+ 1 30+ 1 29+ 1
24-0 20+ 1 62+ 1 10+2 13+2 13 +2 11 +2 85 + 1 49+ 1 21 + 1
79 + 1 10+2 10+2 96+ 1 75 + 1 40+ 1 16 + 1 67+0 13 + 1 44+ 1
78 + 1 65 + 1 47 + 1 29+ 1 14 + 1 79+0 97+0 29+ 1 60+ 1 75 + 1
40+ 1 28 + 1 17 + 1 98+0 71 +0 11 + 1 31 + 1 51 + 1 55 + 1 50+ 1
21 + 1 13 + 1 86+0 64+0 84+0 18 + 1 35 + 1 39+ 1 35+ 1 28+ 1
13+ 1 84+0 60+0 62+0 10+ 1 22 + 1 30+ 1 28 + 1 23 + 1 17 + 1
87+0 60+0 51 +0 67+0 12 + 1 21 + 1 23 + 1 20+ 1 16 + 1 11 + 1
64+0 48-0 49-0 72+0 13 + 1 18 + 1 18 + 1 15 + 1 11 + 1 84+0
50+0 42-0 48-0 75+0 12 + 1 15 + 1 14 + 1 11 + 1 87+0 62+0
4.1 4.2 4.3 4.4
17 +2 10+2 50+ 1 14+ 1
28-0 14+ 1 51 + 1 90+ 1
69+ 90+ 98 + 92 +
74+ 63 + 47 + 29+
39 + 1 27 + 1 17 + 1 10+ 1
20+ 1 13 + 1 84+0 61 +0
12 + 1 80+0 57+0 56+0
81 +0 56+0 47 -0 57+0
58+0 44-0 42-0 59+0
45 -0 37 -0 40-0 60+0
1 1 1 1
1 1 1 1
186
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.3. (continued) The effective principal quantum number no LIn 0.5
2.5
3.0
3.5
4.0
4.5
5.0
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
14+ 1 20+ 1 21 + 1 19 + 1 16 + 1 13 + 1 11 + 1 88+0 67+0 49-0 36-0 29-0 42-0 11 + 1 30 + 1 36+ 1 25 + 1 17 + 1 11 + 1 79+0
15 + 1 21 + 1 20+ 1 17 + 1 14 + 1 11 + 1 91 +0 69+0 51 +0 36-0 27 -0 29-0 58+0 16 + 1 32 + 1 28+ 1 19 + 1 12 + 1 85+0 58+0
18 + 1 21 + 1 18 + 1 14 + 1 11 + 1 83+0 62+0 44-0 31-0 23 -0
15 + 1 14+ 1 13 + 1 11 + 1 85+0
12 + I 19 + 1 21 + 1 20+ 1 18 + 1 16+ 1 13 + 1 11 + 1 91 +0 70+0 51 +0 37-0 34-0 66+0 21 + 1 40+ 1 34+ 1 23 + 1 16 + 1 11 + 1
17 + 1 21 + 1 19 + 1 16 + 1 12 + 1 98+0 74+0 55+0 39-0 28 -0
16+ 1 15 + 1 14+ 1 12 + 1 10 + 1 77+0 44-0 82+0 24+ 1 27+ 1
19 + 1 18 + 1 17 + 1 16 + 1 14 + 1 12 + 1 10+ 1 81 +0 57+0 41- 0 68+0 25 + 1 37 + 1 31 + 1 24+ 1
10 + 1 17 + 1 20+ 1 20+ 1 20+ 1 18 + 1 16 + 1 14 + 1 12 + 1 10 + 1 80+0 59+0 42 -0 39 -0 90+0 29+ 1 41 + 1 32 + 1 23 + 1 16 + 1
23 -0 31 - 0 74+0 19 + 1 29+ 1 22+ 1 14 + 1 97+0 65 +0 10 - O·
21 -0 36-0 89+0 21 + 1 25 + 1 18 + 1 11 + 1 76+0 50+0 35 - 0
1.0 1.5 2.0 Transition s - d, parameter X
1.1
1.2 1.3
1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
15 + 1 15 + 1 15 + 1 13 + 1 70+0 19 + 1 17 + 1 16 + 1 15 + 1 14 + 1
64+0 19 + 1 19 + 1 18 + 1 17 + 1 16 + 1 15 + 1 13 + 1 11 + 1 90+0
24+ 1 21 + 1 18+ 1 15 + 1 12 + 1 93+0 58+0 51 +0 17 + 1 29+ 1
18 + 1 14 + 1 10 + 1 78+0 53 +0 50+0 13 + 1 36+ 1 37 + 1 29+ 1
12 + 1 86+0 60+0 46-0 61 +0 17 + 1 40 + 1 39+ 1 28 + 1 20 + 1
79+0 55+0 42-0 52+0 12 + 1 32 + 1 40+ 1 29+ 1 20+ 1 13 + 1
54+0 40-0 41- 0 76+0 19 + 1 36+ 1 31 + 1 21 + 1 14 + 1 96+0
41-0 35 -0 48-0 10+ 1 24+ 1 32+ 1 24+ 1 15 + 1 10+ 1 70+0
33 -0 34-0 57+0 13 + 1 25 + 1 26+ 1 18 + 1 12 + 1 79+0 53+0
28 -0 35 -0 66+0 14 + 1 24+ 1 21 + 1 14+ 1 93 +0 61 +0 42-0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
15 + 1 15 + 1 14+ 1 13 + 1 71 +0 21 + 1 18 + 1 16 + 1 15 + 1 14 + 1
40-0 19 + 1 21 + 1 19 + 1 18 + 1 17 + 1 15 + 1 13 + 1 11 + 1 92+0
28+ 1 23 + 1 19 + 1 16+ 1 13 + 1 10+ 1 64+0 48-0 14 + 1 29+ 1
22 + 1 16 + 1 12 + 1 88+0 60+0 49-0 10 + 1 31 + 1 40+ 1 31 + 1
14 + 1 10 + 1 70+0 51 +0 57+0 14 + 1 36 + 1 42+ 1 31 + 1 22+ 1
94+0 65+0 48-0 51 +0 10+ 1 26+ 1 41 + 1 33 + 1 22+ 1 15 + 1
65+0 47-0 43 -0 68+0 15 + 1 32+ 1 34+ 1 24+ 1 16 + 1 10 + 1
49-0 39-0 47+0 89+0 20+ 1 31 + 1 26+ 1 17 + 1 11 + 1 78+0
39-0 36-0 53+0 10+ 1 22+ 1 26+ 1 20+ 1 13 + 1 88+0 59+0
33 -0 36-0 59+0 12 + 1 21 + 1 22 + 1 15 + 1 10+ 1 68+0 46-0
4.1 4.2 4.3 4.4
15 + 1 15 + 1 14+ 1 12 + 1
39-0 17 + 1 21 + 1 20+ 1
30+ 1 25 + 1 20+ 1 17 + 1
23 + 1 17 + 1 13 + 1 94+0
15 + 1 10+ 1 76+0 54+0
10+ 1 71 +0 52+0 51 +0
72+0 51 + 0 45 -0 64+0
54+0 42-0 46-0 82+0
42-0 38-0 51 +0 99+0
36 -0 36-0 56+0 11 + 1
6.1 Tables of Numerical Results
187
Table 6.3. (continued) The effective principal quantum number Lin
1.5
2.0
2.5
no
3.0
3.5
4.0
4.5
5.0
Transition p - s, parameter A 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
10 + 1 16 + 1 18 + 1 16 + 1 12 + 1 84+0 45 -0 21 - 0 16 - 0 51 + 0
17 + 1 24+ 1 24+ 1 21 + 1 15 + 1 99+0 55 +0 29 -0 21 - 0 37 -0
21 + 1 28 + 1 27 + 1 22 + 1 15 + 1 99+0 55 + 0 30- 0 26-0 49 -0
25 + 1 31 + 1 28 + 1 22 + 1 15 + 1 95 +0 53 +0 31 - 0 27 -0 45 - O·
28 + 1 32 + 1 28 + 1 21 + 1 14+ 1 89+0 50+0· 31 - 0 28 - O· 48 - O·
30 + 1 33 + 1 28 + 1 21 + 1 14+ 1 84 +0' 48 - O· 30 -0 28 - O· 45 - O·
32 + 1 33 + 1 27 + 1 20 + 1 13 + 1 79+ O· 45 - O· 30-0 28 - O· 45 - O·
33 + 1 33 + 1 27 + 1 19 + 1 12 + 1 74+0· 43 - O· 29 - O· 28 - O· 43 - O·
1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 l.9 2.0
92+0 12 + 1 12 + 1 10+ 1 75 +0 48 - 0 27 -0 15 - 0 19 - 0 71 + 0
13 + 1 15 + 1 13 + 1 10 + I 76+0 51 + 0 31 - 0 20 -0 20-0 39-0
15 + 1 15 + 1 12 + 1 96+0 69+0 46 -0 29- 0 21 - 0 23 - 0 51 + 0
14 + 1 14 + 1 11 + 1 84+0 60+0 40 -0 27 - 0 20-0 22 - o· 39-0
13 + 1 12 + 1 99+0 74+0 53 +0 36 - 0 24-0 19 - 0 21 - O· 39 - O·
11 + 1 11 + 1 87 +0 65 +0 46-0 32 -0 22 -0 18 - 0 20 - O· 33 - O·
10 + 1 98 +0 77 +0 58+0 41- 0 29 - O· 20-0 17 - 0 19 - O· 31 - O·
94+0 86+0 68+0 51 + 0 37 - O· 26 - O' 19 - 0 16 - 0 17 - O· 28 - 0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
85+0 11 + 1 11 + 1 89+0 65+0 41 - 0 23 -0 14 - 0 22 -0 79+0
11 + 1 12 + 1 11 + 1 85 +0 61 +0 41 - 0 26 -0 18 - 0 19 - 0 39 -0
12 + 1 11 + 1 97 +0 73 +0 52+0 35 - 0 24- 0 18 - 0 23 -0 53 +0
10 + 1 99+0 80+0 60+0 43 -0 30- 0 21 - 0 17 - 0 19 - O· 36-0
89+0 83 +0 67+0 50+0 36-0 26-0 18 - 0 16 - 0 19 - O· 36-0
74+0 69+0 56+0 42 -0 31 - 0 22 -0 16 - 0 14 - 0 16 - O' 28 -0
62+0 58+0 47 - 0 36-0 27 -0 19 - O· 14 - 0 13 - 0 15 - O· 26-0
53 +0 49 -0 40-0 31 - 0 23 - O· 17 - O· 13 - 0 12 - 0 14 - O· 22 -0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
83 +0 10 + 1 10 + 1 85 + 0 61 +0 38 - 0 21 - 0 14 - 0 24-0 83 +0
10 + 1 11 + 1 10 + 1 77+0 56+0 38 - 0 24- 0 17 - 0 19 - 0 39 - 0
10 + 1 10 + 1 85 +0 64+0 46 -0 31 - 0 21 - 0 17 - 0 22 - 0 55 +0
89+0 83 +0 68+0 51 + 0 37 -0 26-0 19 - 0 16 - 0 18 - O· 35 - 0
72+0 67+0 55+0 41 - 0 30-0 21- 0 16 - 0 14 - 0 17 - O· 34-0
58+0 54+0 44 - 0 34-0 25 -0 18 - 0 14 - 0 12 - 0 15 - O· 25 -0
47 - 0 44 - 0 36-0 28 -0 21- 0 15 - 0 12 - 0 11 - 0 13 - O· 23 -0
39- 0 37 - 0 30- 0 24-0 18 - O· 13 - O' 11- 0 10 - 0 12 - O· 19 - 0
4.1 4.2 4.3 4.4
81 + 0 10 + 1 10 + 1 82+0
10 + 1 10 + 1 96+0 73 +0
10 + I 95 +0 79+0 59+0
82+0 75 +0 62+0 46 -0
64+0 59+0 49-0 37 -0
50+0 47 - 0 38 - 0 30 -0
40 38 31 24
33 -0 30- 0 25 -0 20-0
-0 - 0 - 0 -0
188
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.3. (continued) The effective principal quantum number no Lin
1.5
2.0
2.5 3.0 Transition p - s, parameter X
3.5
4.0
4.5
5.0
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
10 + 1 97 +0 81 +0 66+0 51 + 0 37 -0 25 -0 17 - 0 29-0 18 + 1
10 + 1 89+0 71 +0 54+0 40+0 28 -0 19 - 0 13 -0 21 - 0 93 +0
10 + 1 82+0 62+0 45 -0 32-0 22-0 14 - 0 11- 0 23 -0 10+ 1
10 + 1 75+0 54+0 38 - 0 26-0 17 - 0 ll- 0 10- 0 20-0 84 +0'
97+0 68+0 47 -0 32 -0 21 - 0 13 - 0 10- O· 10-0 19 - O· 81 + O·
93 +0 62+0 41 - 0 27 -0 18 - 0 11 - o· 10 - O· 10-0 18 - O· 71 + O·
89+0 57+0 37 -0 24-0 15 - 0 10 - O· 10 -0· 10- 0 17 - O· 66+0'
85 +0 52+0 33 -0 20-0 12 - 0 10 - O' 10 - O· 10 - O· 15 - O· 60+0'
1.1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
39 + 1 33 + 1 21 + 1 12 + 1 81 +0 51 + 0 32 -0 26-0 64+0 30+ 1
46 + 1 34 + 1 19 + 1 11 + 1 65 +0 40-0 26-0 22 -0 39 -0 14 + 1
45 + 1 31 + 1 17 + 1 91 +0 53 +0 32- 0 22 -0 22 -0 45 -0 17 + 1
39 + 1 27 + 1 14 + 1 76+0 43 -0 26- 0 18 - 0 19 - 0 38 - O· 12 + 1
33 + 1 23 + 1 12 + 1 63 +0 35 - 0 21 - 0 15 - 0 17 - 0 37 - O· 12 + I·
28 + 1 19 + 1 10 + 1 52+0 29-0 17 -0 13 -0 15 - 0 32 - O· 10 + 1·
24+ 1 16 + 1 85 +0 44-0 24-0 14 - O· 11- 0 14 - 0 30 - O· 93 +0'
20+ 1 13 + 1 71 +0 37 -0 20 - O· 12 - O· 10-0 12 - 0 27 - O· 80+0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 4.1 4.2 4.3 4.4
42 + 1 36+ 1 24+ 1 14 + 1 89+0 55+0 35 - 0 31 - 0 89+0 34+ 1 43 + 1 37 + 1 25 + 1 15 + 1 92+0 57+0 36-0 34-0 10 + 1 35 + 1 43 + 1 38 + 1 25 + 1 15 + 1
50+ 1 37 + 1 22 + 1 12 + 1 72+0 45 -0 30-0 27 -0 48 -0 16 + 1 52 + 1 39 + 1 23 + 1 13 + 1 76+0 47 -0 32 -0 29 -0 53 +0 18 + 1 53 + 1 39 + 1 24+ 1 13 + 1
49+ 1 34 + 1 19 + 1 10 + 1 59+0 36-0 26-0 28-0 59+0 22+ 1 50 + 1 35 + 1 20+ 1 10+ 1 63 +0 39-0 28 -0 32 -0 68+0 25 + 1 51 + 1 35 + 1 20+ 1 11 + 1
42 + 1 29 + 1 16 + 1 86+0 49-0 30-0 22-0 24-0 47 - O· 14 + 1 43 + 1 29 + 1 16 + 1 90+0 52+0 32 -0 24-0 27 -0 53 + O· 16 + 1 43 + 1 30+ 1 17 + 1 93 +0
35 + 1 24+ 1 13 + 1 71 +0 40-0 25 -0 19 - 0 23 -0 47 - O· 14 + 1 35 + 1 24+ 1 13 + 1 75+0 43 -0 27 -0 21 - 0 26-0 53 + O· 16 + 1 36 + 1 24+ 1 14 + 1 77+0
28 + 1 20+ 1 11 + 1 59+0 33 - 0 21- 0 16 - 0 20-0 40 -0' 11 + 1 29+ 1 20+ 1 11 + 1 62+0 36-0 23 -0 18 - 0 23 -0 44 - O· 12 + 1 29 + 1 20+ 1 11 + 1 64+0
23 + 1 16 + 1 92+0 49 -0 28 -0 17 - O· 14 - 0 18 -0 37 - O· 10 + 1 23 + 1 17 + 1 95+0 52+0 30 -0 19 - 0 16 - 0 21 - 0 42 - O· 11 + 1 24 + 1 17 + 1 97+0 54+0
19 + 1 14 + 1 77+0 41 - 0 23 - O· 15 - O· 12 - 0 16 - 0 33 - O· 90+0 19 + 1 14 + 1 80+0 44- 0 25 - O· 16 - O· 14 - 0 18 - 0 36 - O· 97+0 19 + 1 14 + 1 82+0 45 - 0
189
6.1 Tables of Numerical Results Table 6.3. (continued) The effective principal quantum number Lin
1.5
2.0
2.5
no
3.0
3.5
4.0
4.~
5.0
Transition p - p; parameter A ,,=0 0.5 0.6 0.7 0.8 0.9 1.0
14+2 18+2 20+2 20+2 18+2 13 +2
26+2 29+2 29+2 25+2 18+2 11 +2
34+2 36+2 33+2 26+2 17 +2 92+ 1
40+2 39+2 33 +2 24+2 15 +2 75 + 1
44+2 41 +2 33+2 23 +2 13 +2 62 + 1
47+2 42+2 32+2 21 +2 11 +2 53 + 1
49+2 42+2 31 +2 20+2 10+2 46+ 1
50+2 41 +2 30+2 18+2 97 + 1 40+ 1
1.1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
71 + 1 27 + 1 79+0 97+0 31 + 1 68 + 1 10+2 13+2 13+2 11 +2
50+ 1 17 + 1 12 + 1 32 + 1 77 + 1 12+2 15 +2 15 +2 12+2 83 + 1
37 + 1 15 + 1 19 + 1 56+ 1 11 +2 15 + 2 16+2 14+2 10+2 64+ 1
29+ 1 14+ 1 26+ 1 75 + 1 12+2 15 +2 15 +2 12+2 85 + 1 47 + 1
23 + 1 14 + 1 33 + 1 89 + 1 13 +2 15 +2 13 +2 10+2 69+ 1 37 + 1
20+ 1 14+ 1 39+ 1 97+ 1 13 +2 14+2 12 +2 92+ 1 57 + 1 29+ 1
17 + 1 15 + 1 43 + 1 10+2 13 +2 13 +2 11 +2 81 + 1 49+ 1 24+ 1
15 + 1 15 + 1 46+ 1 10+2 12+2 12+2 10+2 71 + 1 42+ 1 20+ 1
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
67+ 1 30+ 1 97+0 74+0 22+ 1 53 + 1 98+ 1 11 +2 12+2 11 +2
43 + 1 17 + 1 10+ 1 22+ 1 56+ 1 98+ 1 12+2 13+2 11 +2 74+ 1
30 + 1 13 + 1 14 + 1 36+ 1 77 + 1 11 +2 12+2 11 +2 88 + 1 55 + 1
21 + 1 11 + 1 17 + 1 46+ 1 87 + 1 11 +2 11 +2 94+ 1 66+ 1 38 + 1
16 + 1 10+ 1 19 + 1 51 + 1 88+ 1 10+2 97 + 1 77 + 1 52+ 1 29+ 1
13 + 1 97+0 20+ 1 53 + 1 84+ 1 92+ 1 83 + 1 64+ 1 41 + 1 22+ 1
11 + 1 91 +0 21 + 1 54+ 1 78+ 1 82+ 1 72+ 1 54+ 1 34+ 1 18 + 1
95+0 88+0 21 + 1 52+ 1 72+ 1 74+ 1 63 + 1 46+ 1 28+ 1 14+ 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
66+ 1 31 + 1 10 + 1 69+0 19+ 1 48+ 1 83 + 1 11 +2 12+2 11 +2
39+ 1 17 + 1 10+ 1 20+ 1 49+ 1 88+ 1 11 +2 12+2 10+2 70+ 1
26+ 1 12 + 1 12 + 1 30 + 1 65 + 1 98 + 1 11 +2 10+2 80+ 1 50+ 1
18 + 1 10+ 1 14+ 1 36+ 1 71 + 1 93 + 1 95 + 1 81 + 1 58 + 1 34+ 1
14 + 1 88+0 14 + 1 39+ 1 69+ 1 83 + 1 88 + 1 65 + 1 45 + 1 25 + 1
10+ 1 78+0 15 + 1 39+ 1 64+ 1 73,+ 1 67 + 1 52+ 1 34+ 1 19 + 1
88+0 71 +0 15 + 1 38+ 1 59+ 1 63 + 1 57 + 1 43 + 1 28+ 1 15 + 1
73+0 65+0 14+ 1 36+ 1 53 + 1 56+ 1 48+ 1 36+ 1 23 + 1 12 + 1
4.1 4.2 4.3 4.4
65 + 1 32+ 1 11 + 1 67+0
38+ 1 16+ 1 10+ 1 18 + 1
25 + 12 + 11 + 27 +
17 + 1 96+0 12 + 1 31 + 1
12 + 1 80+0 12 + 1 33 + 1
96+0 69+0 12 + 1 32+ 1
76+0 60+0 12 + 1 31 + 1
62+0 54+0 11 + 1 29+ 1
1 1 1 1
190
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.3. (continued) The effective principal quantum number no
An
1.5
2.0
2.5
3.0
3.5
4.0
4.5
5.0
Transition p - p; parameter X
K=O 0.5 0.6 0.7 0.8 0.9 1.0
12 + 14 + 15 + 16 + 17 + 17 +
1 1 1 I 1 I
16+ 1 17 + 1 17 + I 17 + I 16 + I 14+ I
17 + 18 + 17 + 16 + 14 + II +
1 I 1 I 1 I
18 + 1 17 + I 16 + I 14 + I II + I 85+0
17 + 1 16 + I 14 + 1 12 + I 96+0 67+0
17 + 1 15 + I 13 + 1 10 + I 80+0 53+0
16 + 1 14+ I II + I 94+0 68+0 43 -0
15 + 1 13 + I 10+ 1 82+0 58+0 35 -0
l.l
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
15 + I 10 + 1 45 -0 49-0 10+ 1 14+ 1 17 + 1 19 + 1 19 + 1 19 + 1
10 + I 59+0 55+0 12 + 1 20+ 1 23 + 1 24+ 1 23 + 1 20+ 1 17 + 1
73 +0 48 -0 88+0 20+ I 27 + 1 27 + 1 24+ 1 21 + 1 17 + 1 13 + 1
54-0 44-0 II + I 25 + I 29+ 1 26+ 1 22 + 1 18 + 1 14 + 1 10 + 1
41-0 44-0 14 + I 28 + I 29+ 1 25 + 1 20+ I 15 + 1 II + 1 78+0
32-0 45 -0 16 + 1 30+ I 28 + 1 22 + 1 17 + I 13 + I 94+0 61 +0
26-0 45-0 17 + I 29+ 1 26+ I 20+ 1 15 + 1 11 + 1 78+0 49-0
21 - 0 46-0 18 + 1 28 + 1 24+ 1 18 + 1 13 + 1 97+0 65+0 40-0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
17 + 1 12+ 1 61 +0 44-0 93+0 14+ 1 17 + 1 19 + 1 20+ 1 20+ 1
12 + 1 73+0 58+0 II + I 20+ 1 25 + 1 26+ 1 24+ 1 22+ 1 18 + 1
87+0 58+0 83 +0 19 + I 28 + I 29+ 1 27 + 1 23 + 1 18 + 1 14 + 1
64+0 51 + 0 10 + 1 24+ 1 32 + 1 29 + 1 25 + 1 19 + 1 15 + 1 10 + 1
49-0 7-0 12 + 1 27 + 1 32 + 1 27 + 1 22 + I 16 + 1 12 + 1 83 +0
38 -0 45 -0 13 + 1 28+ 1 30+ 1 25 + 1 19 + 1 14 + 1 10+ 1 65 +0
31 - 0 43 -0 13 + 1 28 + 1 28 + 1 22+ I 16 + 1 12 + 1 82+0 52+0
25 -0 41-0 14 + 1 27 + 1 26+ 1 20+ 1 14+ 1 10+ 1 69+0 42-0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
18 + 1 13 + 1 68+0 44-0 89+0 14 + 1 17 + I 19 + 1 20+ I 20+ I
13 + 1 79+0 61 +0 II + 1 20+ 1 25+ I 27 + 1 25 + 1 23 + 1 18 + I
94+0 63 +0 84+0 19 + 1 29 + 1 31 + 1 28 + I 24+ I 19 + I 14 + I
69+0 54+0 10 + 1 23 + I 32 + I 31 + I 26+ 1 20+ I 15 + I 11 + I
53 +0 49-0 11 + 1 26+ 1 33 + 1 29+ 1 23 + I 17 + 1 12 + I 86+0
41 - 0 45 -0 12 + 1 27 + I 31 + 1 26+ 1 20+ I 14 + 1 10 + I 67+0
33 -0 43 -0 12 + 1 27 + 1 29+ I 23 + I 17 + 1 12 + I 85+0 54+0
27-0 40-0 12 + 1 26+ 1 26+ 1 20+ 1 15 + I 10 + 1 71 +0 44-0
4.1 4.2 4.3 4.4
19 + 1 14 + 1 72+0 44-0
13 + I 82+0 62+0 II + 1
97+0 66+0 85 +0 18 + I
72+0 56+0 99+0 23 + I
55+0 50+0 II + 1 25 + I
43 -0 46-0 II + 1 26+ I
35 -0 43 -0 11 + 1 26+ 1
28 -0 40-0 12 + 1 25 + I
191
6.1 Tables of Numerical Results Table 6.3. (continued) The effective principal quantum number .dn
l.5
2.0
2.5
no
3.0
3.5
4.0
4.5
5.0
Transition p - p, parameter A
K=2 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 l.0
13 -0 63+0 15 + 1 25 + 1 36 + I 42 + 1 42 + 1 37 + 1 28 + 1 17 + 1
42-0 16 + 1 33 + 1 48 + 1 57 + I 56 + I 48 + 1 35 + 1 22 + 1 12 + I
77+0 27 + I 49+ 1 63 + 1 65 + 1 58 + 1 45 + 1 30 + 1 18 + 1 10 + 1
11 + 1 38 + I 61 + 1 71 + 1 68 + 1 56 + 1 40+ 1 26+ 1 15 + 1 95 +0
16 + I 47 + 1 69 + 1 75 + 1 67 + 1 52 + 1 36 + 1 22 + 1 13 + I 91 +0
21 + 1 56 + 1 75 + 1 76+ 1 64 + I 48 + I 32 + 1 20 + 1 12 + 1 90+0
25 + 1 63 + 1 79+ I 75 + 1 61 + I 45 + 1 29+ I 18 + 1 11 + I 89+0
30 + 1 69 + 1 81 + 1 74+ 1 58 + 1 41 + 1 27 + 1 16 + 1 10 + 1 88+0
1.1 l.2
l.6 l.7 l.8 l.9 2.0
78+0 36-0 34-0 82+0 18 + 1 28 + 1 33 + 1 32 + 1 26+ I 17 + 1
67+0 61 +0 11 + 1 24+ 1 37 + 1 41 + 1 37 + 1 28+ 1 18 + I 11 + I
73 +0 95 +0 19 + 1 36 + 1 43 + 1 40+ 1 31 + 1 22 + I 14 + 1 92+0
83 + 0 12 + 1 26+ 1 41 + 1 42 + 1 35 + 1 26+ 1 17 + 1 11 + I 82+0
92+0 15 + 1 30 + 1 41 + 1 37 + 1 29 + 1 21 + 1 14 + I 99+0 75 +0
99+0 16 + 1 31 + 1 38 + 1 33 + 1 25 + 1 18 + 1 12 + 1 87 +0 70+0
10 + 1 17 + 1 31 + 1 34 + 1 29+ 1 21 + 1 15 + 1 10 + 1 77 +0 66+0
10 + 1 18 + 1 29+ 1 31 + 1 25 + 1 19 + 1 13 + 1 94+0 70+0 63 +0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.8 3.0
83 +0 41 - 0 33 - 0 66+0 15 + 1 25 + 1 31 + 1 31 + 1 26+ 1 18 + 1
68+0 60+0 98+0 20 + 1 32 + 1 37 + 1 33 + 1 26+ 1 17 + 1 10 + 1
70+0 85 + 0 15 + 1 28 + I 36 + 1 34 + I 27 + 1 19 + 1 13 + 1 87+0
74+0 10 + 1 19 + 1 31 + 1 33 + 1 28 + 1 21 + 1 15 + 1 10 + 1 75 +0
77 +0 11 + 1 20 + I 29 + 1 28 + 1 23 + 1 17 + 1 12 + 1 86+0 67 +0
78+0 11 + I 20+ I 26 + 1 24+ 1 19 + 1 14 + 1 10 + 1 73 +0 61 +0
77+0 11 + 1 19 + 1 23 + 1 20 + 1 15 + 1 11 + 1 84+0 63 +0 56+0
76+0 11 + 1 17 + 1 19 + 1 17 + 1 13 + 1 98+0 72+0 56+0 52+0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
86+0 43 -0 32 -0 60+0 14 + 1 24+ 1 30 + 1 31 + 1 26 + 1 18 + 1
67 +0 60-0 93+0 18 + 1 30 + 1 35 + 1 32 + 1 25 + 1 16 + 1 10 + 1
68+0 81 + 0 14 + 1 25 + 1 33 + 1 31 + 1 25 + 1 18 + 1 12 + 1 84+0
70+0 94+0 16 + 1 26 + 1 30 + 1 25 + 1 19 + 1 14 + 1 97 +0 72+0
69+0 99+0 17 + 1 24+ 1 24+ 1 20+ 1 15 + 1 11 + 1 79+0 62+0
67+0 98+0 16 + 1 21 + 1 20 + 1 16 + 1 12 + 1 88+0 66+0 56+0
65 +0 95 +0 14 + 1 18 + 1 16 + 1 13 + 1 99+0 73 +0 56+0 50+0
61 +0 90+0 13 + 1 15 + 1 13 + 1 10 + 1 82+0 61 +0 49- 0 46 - 0
4.1 4.2 4.3 4.4
87 +0 44 -0 32 -0 58+0
67 +0 59+0 90+0 17 + 1
66+0 78+0 13 + 1 23 + 1
67 +0 88 +0 15 + 1 24 + 1
65 + 0 90+0 15 + 1 22 + 1
61 +0 88+0 14 + 1 18 + 1
58+0 83 +0 12 + 1 15 + 1
54+0 77 +0 11 + 1 13 + 1
1.3
1.4 1.5
192
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.3. (continued) The effective principal quantum number
no 3.5
4.0
4.5
5.0
12 + 1 19 + 1 21 + 1 19 + 1 16 + 1 13 + 1 10 + 1 78+0 56+0 47 -0
14 + 1 20 + 1 21 + 1 18 + 1 14 + 1 11 + 1 85+0 61 +0 46 -0 42 -0
16 + 1 21 + 1 20+ 1 16 + 1 12 + 1 96+0 70+0 50+0 38 -0 40-0
17 + 1 21 + 1 19 + 1 15 + 1 11 + 1 82+0 58+0 41 - 0 33 - 0 38 - 0
18 + 1 21 + 1 17 + 1 13 + 1 98+0 70+0 49-0 34-0 29 -0 37 - 0
56+0 10+ 1 25 + 1 40+ 1 39 + 1 30 + 1 21 + 1 14+ 1 10 + 1 76+0
62+0 13 + 1 31 + 1 42 + 1 35 + 1 24+ 1 16 + 1 11 + 1 81 + 0 67+0
67+0 15 + 1 33 + 1 39 + 1 30 + 1 20 + 1 13 + 1 91 +0 67+0 62+0
71 +0 16 + 1 33 + 1 35 + 1 25 + 1 16 + 1 10 + 1 74+0 57+0 58+0
73 +0 17 + 1 31 + 1 30 + 1 20 + 1 13 + 1 89+0 62+0 50+0 48 -0
73 +0 16 + 1 28 + 1 25 + 1 17 + 1 11 + 1 74+0 52+0 44-0 52+0
71 +0 82+0 15 + 1 30 + I 40+ 1 37 + 1 29 + 1 21 + 1 15 + 1 10 + 1
74+0 11 + 1 24+ 1 41 + I 43 + 1 34 + 1 24+ 1 16 + 1 11 + 1 86+0
80+0 14 + 1 29+ 1 43 + I 39 + 1 28 + I 19 + 1 13 + 1 93+0 77+0
85+0 16 + 1 31 + 1 40+ 1 33 + 1 23 + 1 15 + 1 10 + 1 78+0 71 + 0
86+0 16 + 1 30+ 1 35 + 1 27 + 1 18 + 1 12 + 1 86+0 67 +0 67+0
86+0 16 + 1 28 + 1 30 + 1 22 + 1 15 + 1 10+ 1 71 +0 58+0 62+0
84+0 16 + 1 26+ 1 26+ 1 18 + 1 12 + 1 84+0 60+0 51 + 0 58+0
11 + 1 71 +0 67+0 13 + 1 23 + 1 30+ 1 30 + I 27 + 1 22 + 1 17 + 1
78+0 87 +0 15 + 1 30 + 1 40+ 1 39 + 1 31 + 1 23 + 1 16 + 1 10 + 1
83 +0 12 + 1 24+ 1 41 + 1 45 + 1 36 + 1 25 + 1 17 + 1 12 + 1 91 +0
89+0 15 + 1 29 + 1 43 + 1 41 + 1 30 + 1 20+ 1 14 + 1 10 + 1 83 +0
93 +0 16 + 1 30 + 1 40+ 1 34 + 1 24+ 1 16 + 1 11 + 1 84+0 76+0
94+0 16 + 1 29 + 1 35 + 1 28 + 1 19 + 1 13 + 1 92+0 72+0 72 +0
92+0 16 + 1 27 + 1 30 + 1 23 + 1 16 + 1 10 + 1 77+0 63 +0 66+0
89+0 15 + 1 24+ 1 26+ 1 19 + 1 13 + 1 90+0 65 +0 56+0 62+0
11 + 1 74+0 67+0 12 + I
82+0 90+0 16 + I 30+ 1
88+0 12 + 1 24+ 1 41 + 1
94+0 15 + 1 28 + 1 43 + 1
98+0 16 + 1 30 + 1 40+ 1
98+0 16 + 1 29+ 1 35 + 1
96+0 16 + 1 26+ 1 30 + 1
92+0 15 + 1 24+ 1 25 + 1
Lin
1.5 2.0 2.5 3.0 Transition p - p, parameter X
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
63+0 11 + 1 14 + 1 17 + 1 18 + 1 19 + 1 18 + 1 17 + I 15 + 1 12 + 1
84+0 14 + 1 18 + 1 20+ 1 20+ 1 18 + 1 16 + 1 13 + 1 10 + 1 71 + 0
10 + 1 17 + 1 20+ 1 20+ 1 18 + 1 16 + 1 13 + 1 10+ 1 73+0 54+0
1.1
1.4 1.5 1.6 1.7 1.8 1.9 2.0
88+0 52+0 66+0 15 + 1 24+ 1 28 + 1 27 + 1 24+ 1 20+ 1 15 + 1
54+0 71 +0 16 + 1 31 + 1 37 + 1 33 + 1 26+ 1 19 + 1 13 + 1 94+0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
10 + 1 65+0 66+0 13 + 1 24+ 1 29 + I 29+ 1 26+ 1 22 + 1 17 + 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 4.1 4.2 4.3 4.4
K=2
1.2 1.3
Table 6.3. (continued) The effective principal quantum number no An
1.5
2.0 2.5 3.0 Transition p - d, parameter A
4.0
4.5
5.0
1 I 1 1 1 1 1 1 I· I·
59 + 1 82 + 1 86+ 1 81 + 1 69 + 1 54+ 1 38 + 1 24 + 1· 13 + 1· 74+0·
65 + 1 82 + 1 82 + 1 74+ 1 60+ 1 45 + 1 30 + 1· 18 + 1· 10 + I· 61 +0
68 + I 82 + 1 78 + 1 67 + 1 53 + 1 38 + 1· 25 + 1· 15 + I· 84+0· 54+0
3.5
K=I
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
15 +2 16 + 2 15 + 2 12 +2 97 + 1
30 + 1 60+ 1 86 + 1 10+2 11 +2 10+2 96+ 1 76 + 1 53 + 1 32 + 1
43 + 73 + 91 + 99+ 96 + 85 + 68 + 49+ 31 + 16 +
1 1 1 1 1 I 1 1 1 I·
53 + 79+ 90 + 89 + 81 + 66+ 49 + 32 + 19 + 10 +
1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
19+2 15 + 2 10+2 64+ 1 29 + 1 66 +0· 38 -0 34+ 1 56 + 1 72 + 1
59 + 1 29+ 1 11 + I· 65+0 29+ 1 68 + 1 79+ 1 83 + 1 80+ 1 69+ 1
17 + 1· 79+0· 64+0 23 + 1 52 + 1 53 + 1 49 + 1 43 + 1 34+ 1 24+ 1
83 + O· 57+0 11 + 1 41 + 1 42 + 1 39 + 1 34+ 1 28 + 1 20 + 1 12 + 1·
60+0 65 +0· 19 + 1 34 + 1 32 + 1 28 + 1 23 + 1 17 + 1 12 + 1· 73 +0·
54+0 78 + O· 25 + 1 28 + 1 25 + 1 21 + 1 17 + 1 12 + 1· 83 + O· 51 + O·
54+0 93 +0· 24+ 1 23 + 1 20+ 1 17 + 1 13 + 1· 93 +0· 60+0· 39 - O·
55 +0 10 + 1 21 + 1 19 + 1 17 + 1 13 + 1 10 + I· 73 +0· 48 - O~ 33 -0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
10+2 98 + 1 79+ 1 54+ 1 30 + 1 97+0 26-0 20+ 1 41 + 1 54 + 1
48 + 1 27 + 1 12 + 1 61 +0 10 + 1 50+ 1 65 + 1 68 + 1 67 + 1 61 + 1
15 + 1 79+0 50+0 87 + O· 39 + 1 42 + 1 39 + 1 35 + 1 29+ 1 21 + 1
71 + 45 57 + 21 + 31 + 30 + 27 + 22 + 17 + 11 +
O· 0 O· 1 1 1 1 1 1 1·
46 -0 41 - 0 78 +0· 23 + 1 23 + 1 21 + 1 17 + 1 13 + 1 98 + O· 62 + O·
36-0 42 -0 10 + 1 18 + 1 17 + 1 15 + 1 12 + 1 97 +0· 67 +0· 43 - O·
33 - 0 45 -0 11 + 1 14 + 1 13 + 1 11 + 1 94+0· 69 +0· 47 - O· 32 - O·
31 - 0 48 -0 11 + 1 12 + 1 10 + 1 93 +0 73 +0· 53 + O· 36 - O· 26 -0·
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
84+ 1 81 + 1 68 + 1 50 + 1 30 + 1 11 + 1 29-0 10 + 1 35 + 1 47 + 1
44+ 1 27 + 1 13 + 1 63 +0 73 +0 42 + 1 58 + 1 62+ 1 61 + 1 57 + 1
14+ 1 79+0· 47 - 0 65+0 32 + 1 37 + 1 35 + 1 31 + 1 26+ 1 19 + 1
66+0· 41- 0 44 - O· 13 + 1 27 + 1 26 + 1 24 + 1 20+ 1 15 + 1 10 + 1
40 -0· 33 - 0 54+0 17 + 1 19 + 1 17 + 1 15 + 1 12 + 1 87 +0· 57 + O·
30-0 32 -0 66+0 14 + 1 14 + 1 13 + 1 10 + 1 84+0· 59+0· 39 - O·
26-0 33 - O· 75 +0 11 + 1 11 + 1 96+0 78+0 59 +9· 41 - O· 28 - O·
23 -0 33 - 0 75 +0 92+0 86+0 74+0 60+0· 45 - O· 31 - O· 22 - O·
4.1 4.2 4.3 4.4
74+ 73 + 63 + 48 +
42 + 1 26+ 1 13 + 1 65+0
13 + 1 78 + O· 46-0 56+0
63 +0· 38 - 0 39-0 10 + 1
37 -0 30 -0 45 -0 14 + 1
27 -0 28 -0 52+0 12 + 1
22 -0 27 -0 58+0 99+0
20-0 26-0 58+0 78+0
1 1 1 1
Table 6.3. (continued) The effective principal quantum number no An
1.5 2.0 2.5 3.0 Transition p - d, parameter X K
3.5
4.0
4.5
5.0
= I
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
65+0 57+0 49 -0 41 - 0 33 - 0
10 + 1 94+0 79+0 66+0 55 + 0 45 -0 36 -0 28 -0 21 - 0 15 - 0
10 + 1 84+0 67+0 53 + 0 42 -0 33 - 0 25 -0 19 - 0 13 - 0 10 - O·
10 + 1 76+0 58+0 44 -0 33 - 0 25 -0 18 - 0 12 - 0 10 - O· 10 - O·
96+0 69+0 50+0 37 -0 27 -0 19 - 0 13 -0 10 - O· 10 - O· 10 - O·
92+0 63 +0 44 - 0 31 - 0 22 -0 15 - 0 10 - O· 10 - O· 10 - O· 10-0
88+0 57+0 38 -0 26 -0 18 - 0 12 - o· 10 - O· 10 - O· 10 - O· 10 -0
1.6 1.7 1.8 1.9 2.0
56+0 48 - 0 41 - 0 33 - 0 24-0 11 - O· 44-0 30+ 1 15 + 1 95 +0
25 - 0 16 - 0 10 - O· 18 - 0 26+ 1 32 + 1 16 + 1 10 + 1 67 - 0 48 -0
10 - O· 10 - O· 19 - 0 21 + 1 32 + 1 16 + 1 87+0 54+0 35 - 0 23 - 0
10 - O· 11 - 0 76+0 36 + 1 19 + 1 95 +0 55 +0 34- 0 22 - O· 13 - O·
10-0 23 - O· 18 + 1 24+ 1 12 + 1 63 +0 37 -0 22 -0 13 - O· 10 - O·
10-0 40- 0 24 + 1· 16 + 1 84+0 45 -0 26-0 15 -0· 10 - O· 10 - O·
11 - 0 59+0· 21 + 1 12 + 1 61 +0 33 - 0 19 - O· 11 - O· 10 - O· 10 - O·
14 - 0 77 +0 17 + 1 92 +0 46-0 25 -0 14 - O· 10 - O· 10 - O· 10-0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
73 +0 58+0 47 -0 36-0 27 -0 14 - 0 12 -0 37 + 1 22 + 1 12 + 1
34-0 22 -0 13 - 0 12 - 0 76+0 43 + 1 25 + 1 13 + 1 81 +0 55 +0
15 - 0 10 - O· 13 - 0 76+ O· 43 + 1 23 + 1 11 + 1 68+0 42 -0 27 -0
10 - O· 10-0 37 - O· 29+ 1 26+ 1 13 + 1 72+0 43 -0 26-0 16 - O·
10 - 0 16 - 0 82 +0· 30 + 1 17 + 1 87+0 48 -0 28 -0 17 - O· 10 - O·
10-0 25 - 0 13 + 1 21 + 1 11 + 1 60+0 33 - 0 19 - O· 11 - O· 10 - O·
10-0 36-0 17 + 1 15 + 1 83 +0 44-0 24 - O· 14 - O· 10 - O· 10 - O·
12 -0 48 -0 16 + 1 11 + 1 62 +0 33 -0 18 - O· 10 - O· 10 - O· 10 - O·
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
82+0 63 +0 49-0 38 - 0 28 -0 16 - 0 10-0 20+ 1 28 + 1 14 + 1
38 - 0 25 -0 15 - 0 12 - 0 47 -0 45 + 1 30 + 1 15 + 1 90+0 59+0
18 - 0 11 - O· 12 - 0 53+0 44+ 1 28 + 1 13 + 1 76+0 47 -0 30-0
10 - O· 10-0 30 - O· 20+ 1 30 + 1 15 + 1 82+0 48 -0 29-0 18 - 0
10 - O· 14 - 0 61 +0 29 + 1 19 + 1 10 + 1 55 +0 32 -0 19 - O· 11 - O·
10-0 21 - 0 10 + 1 23 + 1 13 + 1 70+0 38 - 0 22 - O· 13 - O· 10 - O·
10- 0 30 - O· 13 + 1 17 + 1 96+0 51 +0 28-0 16 - O· 10 - O· 10 - O·
11 - 0 38 -0 14 + 1 13 + 1 71 +0 38 -0 21 - O· 12 - O· 10 - O· 10 - O·
4.1 4.2 4.3 4.4
88+0 66+0 51 +0 39-0
41 - 0 27-0 17 - 0 12 -0
19 - 0 12 - O· 12 - 0 44-0
11 - O· 10-0 26-0 16 + 1
10 - O· 14 - 0 52+0 27 + 1
10-0 20 -0 85+0 24+ 1
10-0 27 -0 11 + 1 18 + 1
10-0 34-0 13 + 1 14 + 1
1.1
1.2 1.3
1.4 1.5
6.1 Tables of Numerical Results
195
Table 6.3. (continued) The effective principal quantum number no
.dn
1.5
2.0
2.5
3.0
3.5
4.0
4.5
5.0
27 - 1 19 - 0 63+0 14 + 1 25 + 1 38 + 1 49+ 1 56 + 1 55 + 1 47 + 1 35 + 1 22+ 1 12 + 1 69+0 65 +0 10 + 1 20+ 1 31 + 1 39 + 1 39 + 1 33 + 1 23 + 1 14 + 1 84+0 65 +0 85 +0 15 + 1 24+ 1 33 + 1 36 + 1
66 - 1 42 -0 12 + 1 25 + 1 40 + 1 53 + 1 59 + 1 58 + 1 49 + 1 36 + 1 23 + 1 14 + 1 86+0 77 +0 II + 1 21 + 1 32 + 1 39 + 1 39 + 1 32 + 1 23 + 1 14 + 1 96+0 76+0 92+0 15 + 1 24+ 1 32 + 1 34 + 1 29 + 1
ll- 0 72+0 19 + 1 36 + 1 51 + 1 61 + 1 62 + 1 54+ 1 41 + 1 28 + 1 17 + 1 10 + 1 83 +0 10 + 1 17 + 1 29 + 1 38 + 1 38 + 1 32 + 1 24+ 1 16 + 1 11 + 1 83 +0 85 +0 12 + 1 20+ 1 28 + 1 31 + 1 28 + 1 22 + 1
18 - 0 10 + 1 27 + 1 46+ 1 60+ 1 65 + 1 59 + 1 48 + 1 34 + 1 22 + 1 13 + 1 95 +0 92+0 13 + 1 23 + 1 34 + 1 37 + 1 33 + 1 26 + 1 18 + 1 12 + 1 92+0 81 + 0 10 + 1 15 + 1 23 + 1 28 + 1 27 + 1 22+ 1 16 + 1
26-0 14 + 1 34+ 1 54+ 1 65 + 1 65 + 1 56 + 1 42 + 1 29 + 1 18 + 1 11 + 1 91 +0 10 + 1 16 + 1 27 + 1 34+ 1 34 + 1 28 + 1 21 + 1 15 + 1 10 + 1 80+0 81 + 0 10 + 1 16 + 1 23 + 1 25 + 1 22 + 1 17 + 1 13 + 1
36- 0 19 + 1 42 + 1 61 + 1 68 + 1 63 + 1 51 + 1 37 + 1 25 + 1 15 + 1 10+ 1 92+0 11 + 1 19 + 1 29 + 1 33 + 1 30 + 1 24+ 1 17 + 1 12 + 1 88+0 74+0 83 +0 II + 1 17 + 1 22+ 1 22 + 1 19 + 1 15 + 1 10 + 1
Transition p - d, parameter A
K=3 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
31 + 1 34+ 1 33 + 1 28 + 1 21 + 1 11 + 1 40-0 13 - 0 22 -0 62+0 13 + 1 20+ 1 24+ 1 25 + 1 21 + 1 14 + 1 65 +0 21 - 0 15 - 0 37 -0
19 + 1 29+ 1 40+ 1 48 + 1 51 + 1 48 + 1 38 + 1 25 + 1 13 + 1 59+0 38 - 0 61 + 0 13 + 1 23 + 1 33 + 1 38 + 1 36 + 1 27 + 1 17 + 1 86+0 46-0 48-0 92+0 17 + 1 28 + 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
99+0 16 + 1 21 + 1 23 + 1 21 + 1 15 + 1 78+0 28 -0 14 - 0 29-0
34+ 1 34 + 1 28+ 1 18 + 1 99+0 52+0 45 -0 79+0 15 + 1 26+ 1
32 + 1 23 + 1 15 + 1 91 +0 66+0 78+0 13 + 1 22 + 1 30 + 1 34 + 1
22 + 1 14 + 1 98+0 75 +0 84+0 12 + 1 21 + 1 28 + 1 31 + 1 27 + 1
15 + 1 10+ 1 80+0 78+0 10 + 1 16 + 1 24+ 1 27 + 1 26+ 1 20+ 1
11 + 1 88 +0 76+0 87 +0 12 + 1 19 + 1 24+ 1 24 + 1 20+ 1 15 + 1
95 +0 71 +0 71 +0 89+0 13 + 1 19 + 1 21 + 1 19 + 1 15 + 1 11 + 1
78+0 68 + 1 69+0 93 +0 14 + 1 19 + 1 19 + 1 16 + 1 15 + 1 10+ 1
4.1 4.2 4.3 4.4
83 +0 14+ 1 20+ 1 22+ 1
33 + 34+ 28 + 19 +
31 + 1 23 + 1 15 + 1 94+0
21 + 1 14 + 1 98+0 75 +0
15 + 1 10 + 1 79+0 74+0
11 + 1 86+0 75 +0 85 +0
87+0 66+0 62+0 76+0
79+0 69+0 63 +0 73 +0
1 1 1 1
196
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.3. (continued) Lin
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 l.l
1.2 1.3
1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0 4.1 4.2 4.3 4.4
The effective principal quantum number 1.5 2.0 2.5 3.0 Transition p - d, parameter X ,,=3 19 -0 30-0 59+0 88+0 15 + I 10 + I 15 + I 21 + I 20+ I 26+ I 16+ I 24+ I 29+ I 19+ I 27 + I 31 + I 22+ I 29+ I 30 + I 25 + I 30+ I 27 + I 27+ I 28 + I 23 + I 19 + I 28+ I 25 + I 18 + I 21 + I 28+ I 20+ I 14 + I 24+ 1 25 + I 14 + I II + I 25 + I 18 + 1 12 + I 10 + 1 26+ 1 II + I 11 + I 20+ I 24+ 1 82+0 18 + 1 33 + 1 16 + I II + 1 29+ 1 44+ I 68+0 19 + I 38 + I 46+ I 84+0 26+ 1 41 + I 42 + I 14+ 1 31 + I 40+ I 34+ I 18 + 1 22+ 1 26+ 1 28 + 1 29+ 1 28+ I 21 + 1 10 + I 72+0 12 + I 17 + I 22+ I 26+ 1 29+ I 30+ I 29+ 1 23 + I 13 + I 75+0 II + 1 17 + 1 22 + I 27 + 1 29+ 1
34+ I 34+ I 31 + I 24+ I 16+ I 10+ I 10+ I 17 + 1 25 + I 32+ I 36+ I 37+ I 34+ I 27 + I 18 + I II + 1 10+ I 16+ I 24+ I 32+ I 37+ 38+ 35 + 28+
I I I I
34+ I 27 + I 20+ I 14 + I 12 + I 17 + I 27 + I 38 + I 44+ I 44+ I 38+ I 31 + I 22 + I 16 + I 13 + I 16 + I 26+ I 37 + I 45 + I 45 + I 41 + I 33 + I 24+ I 17 + I
no 3.5
4.0
4.5
5.0
41-0 11 + I 19 + I 26+ I 30+ I 31 + I 30+ I 27 + I 23 + I 18 + I
54+0 14 + I 23 + I 29+ I 32+ I 31 + I 28 + I 23 + I 19 + I 14+ I
66+0 17 + I 26+ I 31 + I 32+ I 29+ I 25 + I 20+ I 15 + I 12 + I
79+0 20+ I 29+ I 32 + I 31 + I 27 + I 22 + I 17 + I 13 + I 10 + I
14 + I 11 + I II + I 17 + 1 29+ I 44+ 1 40+ I 44+ I 35 + I 27 + 1
11 + 10 + 12 + 22+ 37 + 48 + 46+ 38 + 29+ 21 +
I I 1 I I 1 1 1 I 1
97+0 99+0 14+ I 26+ 1 41 + I 47 + I 41 + 1 31 + I 23 + I 17 + 1
86+0 10+ 1 16 + I 28 + I 42+ 1 43 + I 35 + I 26+ 1 19 + I 14 + I
26+ I 19 + I 15 + I 14+ I 18 + I 30+ 1 43 + I 49+ I 47 + I 39+ I 30+ I 22+ I 17 + I 15 + I 18 + 1 28 + I 42+ 1 50+ I 49+ I 42+ I
20+ I 15 + I 13 + 1 16 + I 26+ I 40+ 1 50+ I 49+ I 41 + I 31 + I 23 + 1 17 + I 15 + I 17 + I 24+ 1 37 + I 49+ I 51 + I 43 + I 34+ 1
16 + I 13 + I 14+ I 20+ I 32+ I 45 + I 49+ I 43 + I 33 + I 25 + I 18 + 1 15 + 1 15 + I 19 + I 30+ I 42+ I 49+ 1 45+ 1 35 + I 26+ 1
11 + I 11 + I 15 + I 24+ I 35 + I 42+ I 37 + I 29 + 1 22 + I 16+ 1 13 + I 13 + 1 15 + I 23 + 1 35 + I 43 + I 41 + I 31 + 1 24+ I 18 + 1
32+ I 24+ I 18 + I 16 + 1
25 + 19 + 16 + 17 +
20+ 1 16+ 1 16 + 1 20+ 1
13 + 1 12 + I 14 + 1 22 + I 34+ I 45 + 1 44+ I 35 + 1 26+ I 20+ 1 15 + 1 13 + I 15 + 1 21 + I 32 + 1 45 + 1 45 + 1 37 + 1 27+ 1 21 + 1 16 + 1 13 + 1 14+ I 20+ 1
1 I 1 1
15 + 14 + 15 + 21 +
1 1 1 1
6.1 Tables of Numerical Results
197
Table 6.3. (continued)
An
The effective principal quantum number no 2.5 3.0 3.5 4.0 Transition d - s, parameter A
4.5
5.0
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
24-0 71 +0 10+ 1 10 + 1 83 +0 56+0 34-0 21- 0 17 -0 11 - O·
54+0 15 + 1 20+ 1 19 + 1 14 + 1 96+0 59+0 38 -0 35 -0 49-0
90+0 23 + 1 28+ 1 25 + 1 18 + 1 12 + 1 75+0 51 +0 47 -0 57+0
12 + 1 30+ 1 35 + 1 30+ 1 21 + 1 13 + 1 86+0 59+0 56+0 78+0
16 + 1 36 + 1 40+ 1 33 + 1 23 + 1 14+ 1 92+0 65+0 62+0 78+0
20+ 1 42+ 1 44+ 1 35 + 1 24+ 1 15 + 1 96+0 68+0 66+0 89+0
1.1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
44-0 67+0 74+0 65+0 49-0 34-0 24-0 19 - 0 18 - 0 18 -0
85 +0 12 + 1 13 + 1 11 + 1 80+0 56+0 41- 0 35 -0 38-0 53 +0
11 + 1 17 + 1 17 + 1 13 + 1 97+0 68+0 50+0 43 -0 47 -0 62+0
13 + 1 19 + 1 18 + 1 14+ 1 10+ 1 73 +0 55+0 48 -0 53+0 74+0
14+ 1 20+ 1 18 + 1 14 + 1 10+ 1 74+0 56+0 49-0 54+0
14 + 1 20+ 1 18 + 1 14+ 1 10+ 1 73+0 55+0 49-0 55+0 73 +0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
45 -0 59+0 61 +0 52+0 40-0 29-0 22 -0 18 -0 18 - 0 18 -0
81 +0 10+ 1 10+ 1 86+0 64+0 47 -0 37 -0 34-0 39-0 54+0
10 + 1 13 + 1 12 + 1 10 + 1 75 +0 55+0 44-0 40-0 46-0 59+0
11 + 1 13 + 1 13 + 1 10 + 1 76+0 57+0 46-0 44-0 50+0 69+0
11 + 1 13 + 1 12 + 1 99+0 74+0 56+0 45 -0 43 -0 49 -0 64+0
10+ 1 12 + 1 11 + 1 93+0 70+0 53+0 44-0 42-0 48-0 63+0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
44-0 55+0 55+0 47-0 36-0 27 -0 21-0 18 - 0 17 -0 17 -0
77+0 95+0 92+0 76+0 57+0 43 -0 35 -;- 0 33 -0 39-0 53 +0
94+0 11 + 1 10 + 1 86+0 65+0 50+0 41- 0 39-0 44-0 57+0
97+0 11 + 1 10+ 1 86+0 65+0 50+0 42-0 41- 0 48-0 65 +0
93+0 11 + 1 10 + 1 81 +0 62+0 48 -0 40-0 39-0 45 -0 5~+0
87+0 10+ 1 92+0 74+0 57+0 45 -0 38-0 37 -0 43 -0 57+0
4.1 4.2 4.3 4.4
43 -0 52+0 52+0 44-0
75+0 90+0 86+0 70+0
89+0 10+ 1 98+0 79+0
90+0 10 + 1 96+0 77+0
84+0 96+0 88+0 71 +0
76+0 86+0 79+0 64+0
198
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.3. (continued)
An
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
The effective principal quantum number 2.5 3.0 3.5 Transition d - s, parameter X ,,=2 11 + 1 13 + 1 14 + 1 18 + 1 20 + 1 21 + 1 21 + 1 21 + 1 20+ 1 19 + 1 18 + 1 16 + 1 15 + 1 14 + 1 12 + 1 11 + 1 10 + 1 90+0 84+0 74+0 65+0 64+0 61 +0 56+0 68+0 76+0 73 +0 27 -0· 14 + 1 11 + 1
no 4.0
4.5
5.0
16 + 1 21 + 1 19 + 1 15 + 1 11 + 1 78+0 57+0 51 +0 70+0 13 + 1
17 + 1 21 + 1 18 + 1 13 + 1 97+0 67+0 49-0 45 -0 64+0 10+ 1
18 + 1 21 + 1 17 + 1 12 + 1 86+0 59+0 43 -0 41-0 59+0 11 + 1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
23 + 1 34+ 1 34+ 1 27 + 1 20+ 1 14 + 1 10+ 1 93+0 10+ 1 10+ 1
27 + 1 39 + 1 37 + 1 28 + 1 19 + 1 13 + 1 10+ 1 10+ 1 13 + 1 21 + 1
28 + 1 41 + 1 36 + 1 26+ 1 18 + 1 12 + 1 99+0 98+0 12 + 1 19 + 1
27 + 1 39+ 1 34+ 1 23 + 1 15 + 1 11 + 1 90+0 91 +0 12 + 1 20+ 1
25 + 1 36+ 1 30+ 1 21 + 1 13 + 1 98+0 79+0 82+0 11 + 1
23 + 1 32+ 1 27 + 1 18 + 1 12 + 1 85+0 70+0 73+0 10+ 1 16 + 1
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
28 + 1 35 + 1 34+ 1 27 + 1 20+ 1 14 + 1 11 + 1 10+ 1 11 + 1 12 + 1
33 + 41 + 38 + 28 + 20+ 15 + 12 + 12 + 16 + 24+
34+ 1 42 + 1 37 + 1 27 + 1 19 + 1 14 + 1 11 + 1 12 + 1 15 + 1 22 + 1
32+ 1 39 + 1 34+ 1 24+ 1 17 + 1 12 + 1 10+ 1 11 + 1 15 + 1 23 + 1
29+ 1 35 + 1 30+ 1 21 + 1 15 + 1 11 + 1 95+0 10+ 1 13 + 1 20+ 1
26+ 1 31 + 1 26+ 1 18 + 1 13 + 1 97+0 84+0 91 +0 12 + 1 18 + 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
30+ 1 35 + 1 33 + 1 27 + 1 20+ 1 15 + 1 12 + 1 11 + 1 12 + 1 13 + 1
36+ 1 42 + 1 38 + 1 29+ 1 21 + 1 15 + 1 13 + 1 13 + 1 18 + 1 26+ 1
37 + 43 + 37 + 27 + 19 + 15 + 12 + 13 + 17 + 24+
1 1 1 1 1 1 1 1 1 1
34+ 1 40+ 1 34+ 1 24+ 1 17 + 1 13 + 1 11 + 1 12 + 1 17 + 1 25 + 1
31 + 1 35 + 1 30+ 1 21 + 1 15 + 1 11 + 1 10+ 1 11 + 1 15 + 1 21 + 1
27+ 1 31 + 1 26+ 1 18 + 1 13 + 1 10 + 1 93+0 10+ 1 13 + 1 20+ 1
4.1 4.2 4.3 4.4
30+ 1 35 + 1 33 + 1 26+ 1
37 + 42+ 38 + 29 +
38 + 43 + 37 + 27 +
1 1 1 1
35 + 1 40+ 1 34+ 1 25 + 1
32 + 35 + 29+ 22 +
28+ 1 30+ 1 25 + 1 19 + 1
1.1
1 1 1 1 1 1 1 1 1 1
1 1 1 1
1 1 1 1
6.1 Tables of Numerical Results
199
Table 6.3. (continued) The effective principal quantum number no LIn
2.5
3.0
3.5
4.0
4.5
5.0
Transition d - p, parameter A K=1 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
19 + 1 24 + 1 21 + 1 15 + 1 94+0 52+0 32-0 35 - 0 77+0 18 + 1
31 + 1 37 + 1 32 + 1 23 + 1 15 + 1 87+0 50+0 38 - 0 50+0' 12 + 1
41 + 1 46 + 1 38 + 1 27 + 1 17 + 1 99 +0 58+0 47 - 0 63 + 0" 15 + 1
48 + 1 51 + 1 41 + 1 29 + 1 18 + 1 10 + I' 63 +0 49- 0 60+0' 13 + 1
53 + 1 55 + 1 43 + 1 29 + 1 18 + 1 10 + l' 65+0 52 +0 63 +0" 13 + 1
58 + 1 57 + 1 43 + 1 29 + 1 18+ 1 10 + I" 66+0 52 + 0 62 +0' 11 + 1
1.1
1.4 1.5 1.6 1.7 1.8 1.9 2.0
16 + 1 14 + 1 99+0 63 +0 39-0 28 -0 31- 0 57 +0 13 + 1 17 + 1
20+ 1 17 + 1 12 + 1 87+0 59 - 0 40-0 31 - 0 33 - 0 51 +0 12 + 1
23 + 1 18 + 1 13 + 1 92+0 62+0 43 - 0 35 - 0 39 - 0 64+0 15 + 1
21 + 1 17 + 1 12 + 1 89+0 62+0 43 -0 35 - 0 35 - 0 50+0 10 + 1
20+ 1 16 + 1 11 + 1 85 +0 59 + 0" 42 -0 34-0 35 - 0 50+0 10 + 1
18 + 1 14 + 1 11 + 1 79+0 56 + O' 40-0 32 - 0 33 - 0 44 - 0" 81 + 0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
13 + 1 11 + 1 75 +0 47 -0 31 - 0 26 -0 36 - 0 75 +0 14 + 1 17 + 1
14 + 1 12 + 1 89+0 63 +0 44-0 32-0 28-0 32-0 52+0 11 + 1
15 + 1 12 + 1 89+0 63 +0 44- 0 33 - 0 30-0 37 - 0 65 +0 14 + 1
13 + 1 10 + 1 81 + 0 58+0 42 -0 32 - 0 28 -0 30 -0 45 -0 92+0
12 + 1 96+0 73 +0 53 +0 39 -0 30 -0 26 -0 29 -0 44-0 86+0
10 + 1 84+0 65 +0 48 -0 36 - 0 27 - 0 24 -0 26 -0 36 -0 65 +0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
12 + 1 10 + 1 67+0 42 -0 28 -0 26-0 40 -0 86+0 14 + 1 17 + 1
12 + 1 10 + 1 75 +0 53 + 0 38 - 0 29-0 26-0 31 - 0 52+0 10 + 1
12 + 1 10 + 1 73 + 0 52 +0 38 - 0 29 - 0 28 - 0 36 -0 66+0 13 + 1
10 + 1 85 +0 64+0 47 -0 35 - 0 27 - 0 25 - 0 28 -0 42 -0 84+0
91 +0 74+0 56+0 42 -0 31 - 0 25 -0 23 - 0 27 -0 41 - 0 77+0
77+0 63 +0 49-0 37 -0 28 -0 22 - 0 20 - 0 23 - 0 32 -0 57 +0
4.1 4.2 4.3 4.4
12 + 1 95 +0 63 +0 39 - 0
11 + 1 92+0 68+0 49-0
11 + 1 88+0 65 +0 47 - 0
91 + 0 74+0 56+0 41 - 0
77 +0 63 +0 48 -0 36-0
64+0 52+0 41 - 0 31 - 0
1.2 1.3
200
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.3. (continued) The effective principal quantum number 2.5 3.0 3.5 Transition d - p, parameter l ,,=1 10 + 1 10 + 1 99+0 88+0 79+0 71 +0 49-0 67+0 57+0 48-0 40-0 33 -0 32-0 27 -0 21- 0 21-0 17 - 0 14-0 19-0 I3 -0 ll-O 42-0 19 - 0 18 -0 16+ 1 57 = 0 55+0 44+ 1 26+ 1 25 + 1
no 4.0
4.5
5.0
95+0 64+0 43 -0 28 -0 18 - 0 ll-O 10 -0 14 -0 42 -0 18 + 1
90+0 59+0 38 -0 24-0 15 -0 10 -0 10-0 12 -0 38 -0 15 + 1
86+0 53 +0 33 -0 20-0 12 - 0 10-0 10-0 10-0 32-0 12 + 1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
40+ 1 27 + 1 15 + 1 88+0 54+0 44-0 65+0 16+ 1 41 + 1 46+ 1
41 + 1 25 + 1 I3 + 1 74+0 45 -0 31- 0 30-0 49-0 12 + 1 40+ 1
36+ 1 21 + 1 II + 1 61 +0 36-0 26-0 27 -0 48-0 12 + 1 39+ 1
31 + 1 17 + 1 93+0 50+0 30-0 21-0 21-0 34-0 84+0 26+ 1
26+ 1 15 + 1 78+0 42 -0 25 -0 17 -0 18 - 0 31-0 75 +0 23 + 1
22 + 1 12 + 1 66+0 35 -0 20-0 14-0 15 -0 i5 -0 60+0 17 + 1
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
42+ 1 28 + 1 16 + 1 98+0 65 +0 63+0 II + 1 27 + 1 47 + 1 45 + 1
42+ 1 26+ 1 14 + 1 85+0 53+0 40-0 42-0 70+0 16 + 1 45 + 1
36+ 1 22+ 1 12 + 1 70+0 44-0 34-0 39-0 70+0 18 + 1 45 + 1
31 + 1 18 + 1 10 + 1 57+0 36-0 27-0 29-0 47-0 II + 1 29+ 1
26+ 1 15 + 1 85+0 47 -0 29-0 23 -0 25 -0 43 -0 10 + 1 26+ 1
21 + 1 12 + 1 71 +0 40-0 24-0 19 -0 21-0 34-0 76+0 19 + 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
42+ 1 29+ 1 17 + 1 10+ 1 72+0 77+0 14+ 1 33 + 1 47 + 1 45 + 1
42+ 1 27 + 1 15 + 1 91 +0 58+0 46-0 50 + 1 84+0 19 + 1 48+ 1
36+ 1 22+ 1 12 + 1 74+0 48-0 39-0 47 -0 86+ 1 21 + 1 47 + 1
30+ 1 18 + 1 10+ 1 61 +0 39-0 31-0 34-0 56+0 12 + 1 31 + 1
25 + 1 15 + 1 88+0 51 +0 33 -0 26-0 30-0 51 +0 II + 1 27 + 1
21 + 1 I3 + 1 73+0 42-0 27-0 22 -0 24-0 40-0 87+0 20+ 1
4.1 4.2 4.3 4.4
42+ 1 29+ 1 17 + 1 10+ 1
42+ 1 27 + 1 16 + 1 94+0
36+ 1 22+ 1 I3 + 1 77+0
30+ 1 19 + 1 10+ 1 64+0
25 + 1 15 + 1 90+0 53 +0
21 + 1 I3 + 1 75+0 44-0
An
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1
6.1 Tables of Numerical Results Table 6.3. (continued) The effective principal quantum number no
An
2.5 3.0 3.5 Transition d - p, parameter A
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
20 - 1 II - 0 29-0 53 +0 73 +0 80+0 70+0 51 + 0 32 -0 20-0
55 - 1 30 - 0 74+0 12 + 1 15 + 1 15 + 1 12 + I 88 +0 55 +0 37 -0
1.1
1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0
15 - 0 17 - 0 26-0 40-0 53+0 58+0 51 + 0 39-0 27 -0 20-0
2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
4.0
4.5
5.0
10 - 0 55 +0 12 + 1 20+ 1 23 + 1 21 + 1 16 + 1 11 + 1 71 + 0 51 + 0
16 - 0 85 +0 19 + 1 27 + 1 29 + 1 25 + 1 18 + 1 12 + 1 80+0 62+0
24- 0 12 + 1 25 + 1 34 + 1 34 + 1 27 + 1 19 + 1 12 + 1 87 +0 70+0
33 - 0 15 + 1 31 + 1 39 + 1 37 + 1 29 + 1 20+ 1 13 + 1 90+0 76+0
32 - 0 41 - 0 62+0 91 +0 II + 1 II + 1 93 +0 69+0 49 -0 38 - 0
49 -0 67 +0 10 + 1 14 + 1 16 + 1 15 + 1 11 + 1 85 + 0 62+0 52+0
65 +0 92+0 14 + 1 18 + 1 19 + 1 16 + 1 12 + 1 93 +0 70+0 61 +0
78 +0 11 + I 16 + 1 21 + 1 20+ 1 17 + 1 12 + 1 94+0 73 +0 66+0
89+0 13 + 1 19 + 1 22 + 1 21 + 1 17 + 1 12 + 1 92+0 73 +0 67 +0
17 -0 20-0 27 -0 38 - 0 48 -0 51 + 0 45 -0 34- 0 25 -0 19 - 0
36 -0 44-0 60+0 82+0 97 +0 96+0 81 + 0 62+0 46-0 38 - 0
53 +0 67 +0 93 +0 12 + 1 13 + 1 12 + 1 10 + 1 76+0 58+0 51 + 0
66+0 87 +0 11 + 1 15 + 1 15 + 1 13 + 1 10 + 1 82 +0 64+0 58+0
74+0 96+0 13 + 1 15 + 1 15 + 1 13 + 1 10 + 1 81 + 0 65+0 62+0
76+0 10 + 1 13 + 1 16 + 1 15 + 1 12 + 1 99+0 76+0 63 +0 59+0
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
18 - 0 28 -0 28 -0 38 -0 46-0 48 -0 42 - 0 32 -0 24-0 19 -0
37 - 0 44 -0 59+0 77 +0 90+0 88 +0 75 +0 58 +0 45 -0 37 - 0
52+0 65 +0 87+0 11 + 1 12 + 1 11 + 1 92+0 71 + 0 56+0 50+0
64+0 83 +0 11 + 1 13 + 1 13 + 1 12 + 1 98 +0 76+0 62+0 56+0
69+0 84+0 11 + 1 13 + 1 13 + 1 II + 1 93 +0 74+0 62+0 61 +0
65 +0 92+0 11 + 1 13 + 1 13 + 1 II + 1 85 +0 69+0 58+0 50+0
4.1 4.2 4.3 4.4
18 - 0 21- 0 28 -0 37 -0
37 - 0 44-0 58+0 75 +0
52+0 63 +0 83 +0 10 + 1
64+0 83 +0 II + 1 12 + 1
68+0 75 +0 98+0 12 + 1
57 +0 82+0 98+0 II + 1
K=3
201
202
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.3. (continued) The effective principal quantum number no
LIn
2.5
3.0
3.5 Transition d - p, parameter X 1(=3
4.0
4.5
5.0
O.l 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
21 - 0 68+0 12 + 1 19 + 1 24+ 1 27 + 1 26+ 1 21 + 1 14 + 1 10 + 1
32 -0 97 +0 17 + 1 24 + 1 29 + 1 29 + 1 26 + 1 20+ 1 15 + 1 11 + 1
43 -0 12 + 1 21 + 1 28 + 1 31 + 1 29 + 1 24 + 1 19 + 1 14 + 1 12 + 1
56+0 15 + 1 25 + 1 31 + 1 31 + 1 28 + 1 22 + 1 17 + 1 13 + 1 12 + 1
69+0 18 + 1 28 + 1 32 + 1 31 + 1 26+ 1 20+ 1 15 + 1 12 + 1 12 + 1
82 +0 21 + 1 30 + 1 32 + 1 29 + 1 23 + 1 18 + 1 13 + 1 11 + 1 11 + 1
1.1 1.2
1.6 1.7 1.8 1.9 2.0
86+0 10 + 1 15 + 1 23 + 1 30 + 1 32 + 1 28 + 1 21 + 1 15 + 1 11 + 1
11 + 15 + 24+ 33 + 39 + 38 + 32 + 24+ 18 + 15 +
1 1 1 1 1 1 1 1 1 1
13 + 20 + 31 + 42 + 45 + 40 + 32 + 24 + 19 + 17 +
1 1 1 1 1 1 1 1 1 1
15 + 24 + 37 + 47 + 46+ 39 + 30 + 22 + 18 + 17 +
1 1 1 1 1 1 1 1 1 1
2.l 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 3.0
10 + 12 + 17 + 24+ 30 + 32 + 28 + 21 + 15 + 12 +
1 1 1 1 1 1 1 1 1 1
15 + 19 + 27 + 36 + 41 + 39 + 33 + 25 + 20 + 17 +
1 1 1 1 1 1 1 1 1 1
21 + 29 + 40 + 48 + 48 + 41 + 32 + 25 + 20+ 20 +
1 1 1 1 1 1 1 1 1 1
16 + 27 + 41 + 46+ 41 + 32 + 24+ 18 + 16 + 16 + 20+ 30 + 41 + 46+ 41 + 33 + 25 + 20+ 18 + 18 +
1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1
11 + 13 + 18 + 25 + 31 + 31 + 27 + 21 + 15 + 12 +
1 1 1 1 1 1 1 1 1 1
17 + 21 + 28 + 37 + 41 + 40+ 33 + 26 + 20 + 18 +
1 1 1 1 1 1 1 1 1 1
1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1
1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1
3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 4.0
18 + 25 + 35 + 44+ 47 + 42 + 34 + 26 + 21 + 19 + 21 + 27 + 37 + 46 + 48 + 43 + 35 + 27 + 22 + 20 +
16 + 26 + 40+ 48 + 45 + 36 + 27 + 20+ 17 + 17 + 21 + 30 + 41 + 48 + 45 + 37 + 29+ 23 + 19 + 20+
23 + 31 + 41 + 49 + 48 + 42 + 33 + 26 + 22 + 21 +
1 1 1 1 1 1 1 1 1 1
24+ 31 + 42 + 48 + 46 + 39 + 30 + 24+ 21 + 22 +
1 1 1 1 1 1 1 1 1 1
22 + 33 + 44 + 47 + 43 + 34+ 27 + 22 + 20+ 19 +
1 1 1 1 1 1 1 1 1 1
4.l 4.2 4.3 4.4
12 + 14 + 19 + 26 +
1 1 1 1
18 + 22 + 29 + 37 +
1 1 1 1
22 + 29 + 38 + 46 +
1 1 1 1
25 + 33 + 43 + 49+
1 1 1 1
26 + 31 + 39+ 47 +
1 1 1 1
22 + 31 + 43 + 49 +
1 1 1 1
1.3
1.4 1.5
6.1 Tables of Numerical Results
203
A summary of formulas defining the angular factors QK for the actual cases most frequently met is given in Sect. 6.2. The functions cPK(u) and GK«(3) are approximated by means of the following formulas: for K = 1:
cPI(u)
= C(_U_) 1/21n(16 + u) , u+l
G I «(3)
for
K
(6.1.9)
u+q>
= A J ~«(3 + 3) In( 16 + 1/(3) . +X
(6.1.10)
= C (_u_) 1/2 _ _ ,
(6.1.11 )
¥- 1 :
cPK(u)
u+l GK «(3)
= A J~«(3 + 3) +X
u+q> .
(6.1.12)
The transition under consideration is characterized by the assignment of the effective principal quantum numbers of the lower level no and of the upper level nj no
= VZ2RY/IEol, nj = Vz2Ry/IE I I
The quantities Eo and EI are the ionization energies corresponding to a specified state of the atomic core; z is the spectroscopic symbol of an ion. For a neutral atom, z = 1, for a singly charged ion, Z = 2, and so on. The parameters C, q> and A, X for transitions s -+ S, S -+ p, S -+ d, p -+ s, p -+ p, p -+ d, d -+ s, d -+ P are given in Tables 6.2 and 6.3 as functions of no and LIn = nj - no' The spacing with respect to no and LIn adopted in the tables ensures the possibility of linear interpolation almost everywhere. The tables give the order and the mantissa of the number; for example, 24 - 1, 47 - 0, 59+0, 42+ 1, and 12+2 denote respectively 0.024, 0.47, 0.59, 4.2, and 12. The range of approximation for cross sections is 1 :S u :S 128. The cases where the errors of approximation exceed 10 percent are indicated in Table 6.2 by asterisks. These errors, however, do not exceed a factor of 2. The rate coefficients are approximated in the range 1/32 :S (3 :S 4. The asterisks in Tables 6.3 indicate the cases in which errors of approximation are greater than 25 percent. 6.1.4 Normalized Cross Sections for Specific Atoms and Ions (Tables 6.4--8) (i) LIS = 0 For transitions with no change of spin (LIS = 0) the cross sections (J and rate coefficients (v(J) are fitted by
(J' = naij [EI] 3/2 Q~(aoad CcP'(u) z4 Eo 2/0 + 1 u + q> ,
(6.1.13)
204
6. Tables and Formulas for the Estimation of Effective Cross Sections u = (8 - AE)/z'l-Ry ,
(vn) =
1O-8~ [EI] 3/2 Q~(aoad z3 Eo 210 + 1
P=
Ry/T,
z2
AE/Z2
p=
• AG'(P)ex (_ P) P+ X P P ,
cm3 s- 1
(6.1.14)
Ry.
Here, z is the charge of the parent ion (spectroscopic symbol of ion, Z = 1 for a neutral atom, Z = 2 for a singly charged ion, and so on), and Q~(aoad is the angular factor. In fact, in all tables only the states with s core electrons (besides closed shells) are considered. In this case
Lp
Gfo~o p p
= 0,
= 1,
Q'
=m
for excitation from the shells of equivalent electrons 1'0, and Q' = 1 for one electron outside closed electron shells. Since Q' are independent of K we give the values, summed over K, of n and (vn). The formulas for tP'(u) and G'(P) are given by (5.1.12, 13 and 16). (ii) AS = 1 In the case of intercombination transitions n" = naij
z4
[EI]3/2 Q~(aoat>CtP"(u) Eo
210 + 1
(6.1.15)
u + cp ,
u = (8 - AE)/z2 Ry,
(vn") =
1O-8~ [EI]3 /2Q~(aoad.AG"(P) exp(-pp) [cm3 S-I], z3
P=
z2 Ry/T,
Eo
210
+I
P+ X
(6.1.16)
p = AE/z2 Ry.
In the tables for intercombination transitions, as in those for AS = 0 only the states with s core electrons (besides closed shells) are considered. In this case
L
p = 0,
"LnSo" lTL;Sp
= 1,
Q
= mA 2 = m
2S1 + 1 2(2Sp + 1)
(6. l.l 7)
for excitation from the shells of m equivalent electrons. Since Q" are independent of K we give summed over K values of n" and (vn"). The formulas for tP"(u) and G"(P) are given by (5.1.12, 13 and 16). The energy dependence of exchange cross sections varies from one transition to another, and the errors of fitting are rather large. For this reason only the rate coefficients are tabulated in most cases. The set of parameters C, cp,D is adjusted for the range 0.02 < u < 16, and the set A,X,D, for 0.25 < P < 16.
6.1 Tables of Numerical Results
205
Table 6.4. Normalized Born and Coulomb-Born excitation cross sections. Transitions with no change of spin (LIS = 0) Atom
HI
He I
C 3.46 70.32 2.33 38.11 1.81 2.06 31.58 2.07 0.03
0.67 4.27 0.68 3.64 1.13 0.69 3.49 1.29 0.61
D 0.00 0.00 0.00 0.00 0.30 0.00 0.00 0.20 0.40
R 0.04 0.03 0.01 0.05 0.01 0.01 0.05 0.Q1 0.01
A 7.52 24.12 5.72 18.59 2.03 5.24 16.77 2.40 0.06
X 12.13 0.34 2.94 0.28 0.68 2.53 0.32 0.65 0.87
D 9.90 0.50 1.40 0.00 0.20 1.00 0.00 0.10 0.00
R 0.03 0.02 0.02 0.02 0.02 0.02 0.Q1 0.02 0.02
2s-3s 2s-3p 2s-3d 2s-4s 2s-4p 2s-4d 2s-4f 2p-3s 2p-3p 2p-3d 2p-4s 2p-4p 2p-4d 2p-4f
18.27 139.93 57.52 8.34 59.82 16.73 8.94 10.51 60.96 1014.92 4.89 27.75 313.54 38.55
0.26 0.60 0.18 0.22 0.60 0.12 0.13 0.02 0.41 1.59 0.Q1 0.24 1.05 0.35
0.00 0.90 0.00 0.00 0.90 0.00 0.00 0.90 0.00 0.20 0.90 0.00 0.00 0.00
0.02 0.53 0.02 0.02 0.58 0.01 0.03 0.57 0.06 0.06 0.44 0.02 0.11 0.08
20.15 15.20 89.18 13.57 7.72 46.84 21.24 8.73 42.94 147.18 5.80 42.45 122.06 41.11
1.64 0.53 1.14 0.74 0.68 10.17 4.10 0.26 1.75 0.67 0.54 0.84 0.80 1.74
2.10 9.90 0.60 0.00 9.90 6.70 2.60 0.00 3.90 6.70 0.00 0.20 2.70 2.30
0.02 0.16 0.02 0.02 0.12 0.02 0.02 0.08 0.02 0.02 0.17 0.02 0.02 0.02
3s-4s 3s-4p 3s-4d 3s-4f 3p-4s 3p-4p 3p-4d 3p-4f 3d-4s 3d-4p 3d-4d 3d-4f 11S-2 1S 11S-ip 11S-3 1S 11S_3 1P 11S-3 1D 11S-4 1S 11S-4 1p 11S-41D 11S-41F
55.53 0.16 359.31 0.26 114.84 0.11 56.65 0.03 61.83 -0.01 197.65 0.27 1644.09 0.51 394.47 0.13 0.05 6.43 52.52 0.02 251.01 0.17 5485.46 0.73 1.26 1.85 8.22 26.71 1.43 1.32 21.53 7.78 2.90 0.36 1.34 1.32 21.77 8.99 0.44 2.91 0.00 1.48
0.00 0.90 0.00 0.00 1.00 0.00 0.60 0.00 0.10 0.70 0.50 0.70 0.00 0.20 0.00 0.20 0.20 0.00 0.10 0.20 0.30
0.07 0.25 0.12 0.01 0.44 0.07 0.16 0.10 0.05 0.25 0.04 0.14 0.Q1 0.02 0.01 0.03 0.02 0.01 0.02 0.02 0.02
40.45 44.43 111.48 121.39 25.01 88.72 228.43 332.30 10.84 49.05 84.22 502.57 4.13 8.09 3.43 7.55 0.33 3.25 7.35 0.42 0.00
3.07 0.57 4.54 0.99 0.63 2.46 0.74 4.44 1.29 0.50 1.83 0.38 1.61 0.25 1.23 0.25 0.52 1.25 0.27 0.54 0.97
7.70 9.90 8.70 0.00 2.90 9.90 9.90 9.90 0.70 0.30 9.90 9.90 0.40 0.10 0.00 0.00 0.00 0.00 0.00 0.00 0.20
0.02 0.22 0.02 0.02 0.02 0.02 0.13 0.02 0.Q1 0.02 0.02 0.31 0.02 0.02 0.02 0.01 0.02 0.Q1 0.01 0.02 0.02
1.00 0.00
0.15 0.02
72.85 17.95
1.32 1.32
9.90 1.30
0.07 0.02
Transition Is-2s Is-2p Is-3s ls-3p Is-3d ls--4s Is-4p Is-4d Is-4f
2 1S-21p is-3 1S
287.51 14.84
qJ
0.00 0.28
206
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.4. (continued) Atom Transition He I
Li I
LiII
D
R
0.46 0.79 0.79 0.53 12.25 2.77
7.20 0.10 0.00 7.60 9.90 1.50
0.02 0.02 0.00 D.03 0.02 0.02
5.55 42.80 147.66 3.59 42.42 121.92 40.64
0.73 1.75 0.67 0.67 0.84 0.81 1.74
9.60 3.90 6.60 3.90 0.20 2.70 2.30
0.04 0.02 0.02 0.03 0.02 0.02 0.02
0.10 0.00 0.00 0.00 0.00 0.00 0.00 0.00
0.07 53.34 0.03 15.61 0.65 8.05 0.01 48.95 0.01 10.51 0.53 5.23 0.01 34.76 0.04 5.97
1.13 0.94 0.22 0.71 0.85 0.16 0.93 1.51
8.60 0.50 0.00 0.00 0.00 0.10 0.00 0.40
0.03 0.02 0.13 0.01 0.01 0.09 0.02 0.02
0.34 0.43 1.81 0.34 0.24 1.21
0.90 0.00 0.10 0.90 0.00 0.00
0.31 0.04 0.05 0.42 0.03 0.11
9.16 41.32 137.32 3.45 40.94 112.13 30.57
0.80 1.60 0.66 0.93 0.72 0.77 1.70
9.90 3.30 5.70 7.80 0.00 2.70 2.30
0.07 0.02 0.02 0.06 0.01 0.02 0.02
242.74 9.92 6.02 24.23 129.92 57.91 917.36 1261.32 75.59 2994.65
1.14 0.26 0.12 0.37 1.30 0.42 1.79 0.13 0.06 0.10
0.10 0.20 0.10 0.00 0.00 0.00 0.10 0.90 0.00 0.20
0.06 58.31 0.04 14.43 0.06 20.23 0.02 36.32 0.30 26.90 0.04 46.49 0.05 148.53 0.15 232.48 0.04 115.65 0.231495.79
0.86 0.66 7.03 0.70 0.86 1.22 0.63 0.93 2.17 2.48
5.20 0.00 3.40 0.00 6.00 2.10 5.40 9.90 2.10 9.10
0.02 0.01 0.02 0.01 0.03 0.02 0.02 0.07 0.02 0.02
1.87 43.32 1.37 31.48 0.79
0.78 7.77 0.80 7.63 3.46
0.00 0.20 0.00 0.20 0.40
0.06 0.02 0.08 0.02 0.02
1.30 0.21 1.41 0.22 0.51
0.00 0.20 0.00 0.10 0.80
0.01 0.02 0.01 0.02 0.02
({J
D
R
62.58 45.04 7.12 34.69 18.89 5.27
3.01 0.23 0.25 2.21 0.18 0.17
0.20 0.00 0.00 0.50 0.00 0.00
0.11 5.35 0.01 70.67 0.01 12.06 0.09 3.39 0.01 43.96 0.03 12.09
ip-3 l S 21P-3 1P 21p-3 1D 21p-4 IS 2lp-4lp iP-4 ID iP-4 IF
44.98 60.81 1010.04 16.10 27.69 313.07 38.15
0.97 0.41 1.59 1.73 0.24 1.05 0.36
0.60 0.00 0.20 0.00 0.00 0.00 0.00
0.21 0.06 0.06 0.09 0.02 0.11 0.08
23S_23P 23S-3 3S 23S_3 3P 23S-3 3D 23S-43S 23S-43P 23 S-4 3 D 23S-43F
255.67 11.64 11.93 31.92 5.91 10.22 18.13 2.72
0.83 0.31 0.60 0.30 0.28 1.02 0.27 0.23
23P_3 3 S 23 p_3 3 p 23p_3 3 D 23 P-4 3 S 23 P-4 3 P 23 P-4 3 D 23 P-4 3 F
60.27 55.97 865.03 16.22 25.80 309.41
2 1S-3 1P is-3 ID 2 IS-4 IS 2 1S-4lp 2 IS-4ID is-4 IF
2s-2p 2s-3s 2s-3p 2s-3d 2p-3s 2p-3p 2p-3d 3s-3p ·3s-3d 3p-3d lis-is I Is-ip 11S-3 1S 11S-3 1P 11S-3 1D
C
A
5.62 11.31 4.64 9.38 0.39
X
207
6.1 Tables of Numerical Results Table 6.4. (continued) Atom Transition
C
cp
D
R
A
X
D
R
2 l s-ip is-3 IS 2 1S-3 1P is-3 ID ip-3 l S 21P-3 1P 21p-3 1D
309.65 14.84 93.49 50.10 32.36 59.47 892.85
0.03 0.19 1.66 0.32 2.31 0.21 1.12
0.70 0.00 0.60 0.00 0.00 0.00 0.00
0.15 211.50 0.02 27.82 8.41 0.15 0.03 61.23 0.07 4.48 0.01 93.50 0.16292.64
1.33 1.02 0.53 1.18 0.54 1.21 0.62
3.10 0.20 9.10 1.10 5.20 0.70 2.60
0.02 0.02 0.02 0.02 0.02 0.02 0.02
23S-23p 23S-33S 23S-3 3p 23S-3 3D 23P_3 3S 23p_3 3p 23p-3 3D
249.92 13.55 57.24 41.93 43.37 54.68 780.14
0.03 0.23 1.87 0.41 2.15 0.22 1.21
0.80 0.00 0.70 0.00 0.10 0.00 0.00
0.18 164.06 0.01 23.92 0.15 4.15 0.02 48.10 0.17 5.70 0.01 87.89 0.16268.62
1.11 1.12 0.45 1.12 0.60 1.09 0.51
2.60 0.40 9.90 1.10 6.20 0.50 1.90
0.02 0.02 0.02 0.02 0.03 0.02 0.02
Be I
2S-2P
151.61
2.11
0.00
222.45 12.24 29.67 35.05 70.98 54.88 790.48 1517.48 68.55
0.02 0.26 4.26 0.44 1.72 0.21 1.20 0.03 0.03
0.90 0.00 0.00 0.10 0.00 0.00 0.00 0.80 0.10
0.92 1.11 0.30 1.08 0.65 1.10 0.51 1.51 1.11
0.90 2.20 0.40 3.00 1.10 4.80 0.50 1.90 6.60 0.30
0.02
2s-2p 2s-3s 2s-3p 2s-3d 2p--3s 2p--3p 2p--3d 3s-3p 3s-3d
58.21 141.37 21.28 3.48 38.34 13.17 89.02 273.34 615.05 129.97
0.40
Be II
0.09 0.24 0.01 0.03 0.02 0.10 0.01 0.16 0.15 0.02
0.02 0.02 0.02 0.02 0.03 0.02 0.02 0.02 0.02
CI
2p2 3p-2p3s 3p 18.47 2p21D-2p3s Ip 20.37 2p2 IS-2p3s IP 30.78 2 1s-ip 209.19
2.92 2.36 2.09
0.50 0.50 0.20
0.08 0.10 0.08
4.14 4.97 9.70
0.41 0.43 0.46
2.00 2.00 1.50
0.03 0.03 0.02
0.04
0.70
0.25 193.41
0.53
0.40
0.02
223.10 303.97 27.94 10.46 19.82 1392.49 254.78 70.07 85.49
0.03 1.37 0.34 0.33 0.11 1.44 0.92 0.38 0.45
0.70 0.10 0.00 0.00 0.60 0.30 0.00 0.00 0.00
0.23 0.06 0.01 0.04 0.09 0.05 0.11 0.10 0.07
71.46 1286.57
0.05 0.25
0.00 0.80
209.07 67.57 42.88 14.91 31.17 159.32 59.15 53.67 55.35 676.14 0.03 109.74 0.14215.54
0.54 0.76 0.72 0.65 0.74 0.68 0.97 1.39 1.36 1.62 2.24 0.88
0.40 4.80 0.00 0.00 0.00 9.10 6.40 2.70 3.10 9.90 2.20 9.90
0.02 0.02 0.01 0.02 0.02 0.02 0.03 0.02 0.01 0.04 0.02 0.06
Lill
OV F VI Na I
is-2IP 3s-3p 3s-3d 3s-4s 3s-4p 3p--3d 3p-4s 3p-4p 3p-4p 3d-4p 4s-3d 4s-4p
Na VIII
is-ip
244.83
0.02
0.70
0.20 225.78
0.62
0.60
0.02
MgI
3 1S-3 1P 3 IS-4 I S
214.17 5.29
2.32 0.54
0.00 0.10
0.06 62.81 0.03 6.87
0.45 -0.61
1.60 0.00
0.020.01
208
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.4. (continued) Atom Transition MgI
C
qJ
D
R
A
X
D
R
26.04 25.34 281.84 1140.87 84.65
0.44 0.79 0.84 1.06 0.18
0.00 0.00 0.00 0.50 0.00
om
3 1S-4lp 3 I P-4 I S 3 1P-3 1D 3 1P-4lp
45.35 27.74 68.56 130.28 127.20
0.85 0.55 1.02 0.68 1.18
0.00 0.00 6.50 9.90 0.70
0.01 0.02 0.02 0.01 0.02
33 P-4 3 S 33 P-43 P 33 p-3 3 D
103.99 298.92 706.60
1.56 2.62 2.22
0.10 0.00 0.10
0.18 23.65 0.51 68.46 0.05 141.69
0.73 0.15 0.53
4.30 0.60 3.30
0.03 0.03 0.02
406.66 15.14 51.07 208.84 1604.38 48.25
0.49 0.21 0.32 0.74 0.79 0.00
0.00 0.00 0.00 0.00 0.00 0.00
0.22 198.56 0.02 25.99 0.03 63.40 0.21 66.65 0.17475.20 0.01 104.53
0.87 1.33 1.20 0.76 0.81 0.99
2.70 0.70 1.10 3.70 4.30 0.00
0.02 0.02 0.02 0.02 0.02 0.00
3 1S-3 1D
0.13 0.10 0.07 0.02
Mg II
3s-3p 3s-4s 3s-3d 3p-4s 3p-3d 4s-3d
Mg IX
2S-2P
253.98
0.02
0.70
0.19 235.97
0.63
0.60
0.02
MgX
2s-2p 2s-3s 2s-3p 2s-3d 2p-3s 2p-3p 2p-3d
319.36 16.14 119.68 49.81 23.35 56.80 745.42
om 0.16 2.26 0.10 1.69 0.15 0.68
0.70 0.00 0.00 0.60 0.00 0.00 0.00
0.14278.24 0.02 34.07 0.11 22.37 0.06 68.92 0.17 5.40 0.01 119.17 0.29439.66
0.90 0.96 0.38 0.65 0.39 0.95 0.40
1.30 0.00 2.70 0.10 2.30 0.00 0.60
0.02 0.01 0.02 0.01 0.02 0.01 0.02
Al I
3p-4s
77.72
1.68
0.20
0.13
18.76
0.66
3.50
0.02
329.94
0.81
0.00
0.19 157.76
0.57
1.50
0.02
390.91 12.79 40.96 23.27 294.73 1522.11 80.13 33.26 1586.55 858.63
1.02 0.30 0.22 0.13 0.95 0.98 0.36 0.02 0.14 0.53
0.30 0.00 0.00 0.50 0.00 0.50 0.00 0.00 0.90 0.00
0.08 0.02 0.01 0.08 0.13 0.06 0.13 0.06 0.16 0.11
73.65 16.82 70.01 35.02 61.19 171.45 59.54 45.52 281.97 196.56
0.83 0.92 0.79 0.70 0.99 0.64 1.50 3.70 0.90 1.34
6.80 0.50 0.00 0.00 7.30 9.90 3.10 5.00 9.90 9.90
0.02 0.02 0.00 0.01 0.03 0.05 0.02 0.02 0.07 0.03
AlII
3 1S-3 1P
KI
4s-4p 4s-5s 4s-3d 4s-5p 4p-5s 4p-3d 4p-5p 5s-3d 5s-5p 3d-5p
Ca I
4 1S-3 1D 4 1S-4lp 3 1O-4 l p 43 p-3 3 D
12.19 302.55 304.09 283.09
0.16 1.82 0.19 0.59
0.00 0.10 0.20 0.00
0.02 0.06 0.10 0.09
25.12 68.44 116.87 69.84
0.99 0.62 1.95 1.40
0.00 3.50 9.10 9.40
0.02 0.02 0.02 0.02
Ca II
4s-3d 4s-4p 4s-5s 3d-4p 3d-5s 4p-5s
10.89 596.95 20.11 369.95 1.75 294.60
0.03 0.03 0.17 0.02 0.06 0.68
0.00 0.90 0.00 0.80 0.40 0.00
0.03 24.65 0.27 178.03 om 33.95 0.15 236.50 2.88 0.03 0.22 85.36
1.05 0.99 1.54 1.23 0.73 0.82
0.00 3.70 1.00 3.00 0.00 4.60
0.00 0.02 0.02 0.02 0.01 0.02
Table 6.4. (continued) Atom Transition
C
cp
D
R
A
X
D
R
Cu I
4s--4p
167.62
1.71
0.00
0.08
58.81
0.51
1.60
0.02
Zn I
4 1S--41P 4 1S-5 1S 4 1S--4 1D 4 1S_5 1P 41P_5 1S 41p--41D 41p_5 1p
163.76 3.66 15.12 30.46 240.58 1082.46 66.48
2.58 0.77 0.67 1.22 0.83 1.73 0.24
0.00 0.00 0.00 0.00 0.00 0.20 0.00
0.06 0.04 0.00 0.13 0.10 0.04 0.03
56.38 4.67 23.90 27.88 62.92 152.82 88.16
0.38 0.62 0.79 0.48 1.02 0.63 1.24
0.90 0.00 0.00 0.00 6.00 6.40 1.00
0.02 0.00 0.Ql 0.02 0.02 0.02 0.02
4 3P_5 3S 43p_5 3p 43P--4 3D
88.10 753.48 470.12
1.62 5.43 2.25
0.00 0.00 0.10
0.10 22.88 0.47 85.75 0.07 114.73
0.71 0.08 0.44
3.50 1.00 2.10
0.02 0.02 0.02
315.14 10.72 35.49 13.28 4.17 177.20 1253.98 243.28 71.52
0.62 0.24 0.39 0.19 0.38 0.80 0.96 0.69 0.15
0.00 0.00 0.20 0.30 0.00 0.00 0.00 0.00 0.60
0.21 0.02 0.02 0.05 0.05 0.20 0.17 0.67 0.03
156.02 20.05 38.25 24.07 6.70 57.89 388.52 133.56 69.26
0.78 0.84 1.05 0.83 1.41 0.74 0.70 0.26 1.19
2.20 0.00 1.10 0.00 0.90 3.40 3.30 0.20 1.70
0.02 0.02 0.02 0.00 0.02 0.02 0.02 0.03 0.02
Zn II
4s--4p 4s-5s 4s--4d 4s-5p 4s--4f 4p-5s 4p--4d 4p-5p 4p--4f
Ga I
4p-5s 4p-5p 4p--4d 4p-6s 5s-5p 5s--4d 5s--6s 4 1S--4 1p 4 1S-5 1S 4 1S--4 1D 41P_5 1S 41p--41D 43P_5 3S 4 3P--4 3D
78.66 22.83 479.96 21.00 700.64 57.69 21.33
1.83 0.00 2.64 1.47 0.69 0.11 0.24
0.00 1.00 0.00 0.30 0.50 0.00 0.00
0.09 0.04 0.05 0.12 0.11 0.04 0.06
20.93 30.47 123.45 8.21 105.03 96.59 23.53
0.66 0.70 0.42 0.54 0.88 0.99 1.52
3.00 0.20 1.70 1.50 9.90 0.30 1.90
0.02 0.02 0.02 0.03 0.02 0.02 0.02
299.06 7.91 40.57 230.70 1285.02 124.23 986.67
0.94 0.26 0.48 0.63 0.74 1.23 1.20
0.00 0.00 0.00 0.00 0.00 0.00 0.00
0.18 138.94 0.04 16.22 0.02 48.84 0.23 90.02 0.17417.23 0.15 33.28 0.15 336.24
0.54 0.93 1.07 0.76 0.83 0.67 0.52
1.40 0.00 0.90 3.00 4.00 3.50 2.00
0.02 0.Ql 0.02 0.02 0.02 0.02 0.02
5s-5p 5s--4d 5s--6s 5s--6p 5s-5d 5p--4d 5p-6s 5p-6p 5p-5d 4d--6s 4d--6p 4d-5d
421.39 39.60 13.38 29.20 8.52 1330.95 338.26 85.10 42.03 22.90 395.52 194.77
1.03 0.19 0.30 0.12 0.11 0.66 0.92 0.34 0.03 0.02 0.55 0.03
0.30 0.00 0.00 0.60 0.00 0.60 0.00 0.00 0.80 0.00 0.00 0.90
0.08 0.01 0.02 0.11 0.01 0.07 0.11 0.13 0.37 0.04 0.15 0.17
0.83 0.82 1.03 0.60 5.07 0.71 1.01 1.52 0.41 2.89 1.20 0.79
7.00 0.00 0.70 0.00 2.30 9.90 7.70 3.20 0.00 2.90 7.60 3.40
0.02 0.00 0.02 0.00 0.01 0.06 0.03 0.02 0.04 0.02 0.03 0.02
Ga II
RbI
76.70 70.04 17.21 38.59 27.98 174.03 68.96 62.76 42.62 37.65 103.37 83.95
210
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.4. (continued) Atom Transition Sr I
SI8-4 1D SiS-Sip SIS-6 IS SIS-6 l p 4 10-S1P 41D-(j IS 4 1D-(jl P S3P-43D S3P-63S S3P-63P 4 3D-(j3S 43D-(j3p
A
D
R
0.93 0.63 1.01 3.58 1.81 0.82 0.46
0.00 4.10 0.80 1.90 9.90 0.00 1.60
0.01 0.02 0.02 0.01 0.03 0.01 0.02
0.13 112.4S 0.24 33.94 62.69 0.03 11.S9 12.21
1.32 0.79 1.38 0.86 0.31
9.90 6.60 1.70 0.00 0.40
0.03 0.03 0.02 0.00 0.01
cp
D
R
21.03 338.S3
0.16 1.66
0.00 0.20
8.23 SS2.67 6.46 31.88
0.20 0.29 0.10 0.73
0.00 0.00 0.00 0.00
0.02 41.28 0.07 70.01 11.6S 0.01 21.27 0.08 181.86 0.02 11.79 0.32 13.04
448.12 181.20
0.00 0.89
1.00 O.SO
6.11
0.09
0.00
C
X
Sr II
Ss-4d Ss-Sp Ss-6s Ss-Sd Ss-6p Ss-4f Sp-6s Sp-Sd Sp-6p Sp-4f 4d-Sp 4d-6s 4d-Sd 4d-Sd 4d-Sd 4d-6p 4d-4f
18.13 726.97 21.9S 33.20 2S.6S 20.16 S03.13 2168.30 128.12 281.14 489.30 2.98 108.S2 SO.72 SO.72 22.17 978.39
0.03 0.S1 O.1S 0.16 0.11 0.16 0.03 0.69 0.11 0.12 0.03 0.06 0.13 0.01 0.01 0.07 1.02
0.00 0.00 0.00 0.50 0.30 0.00 0.90 0.00 0.10 0.30 0.80 0.40 0.10 0.70 0.70 0.40 0.00
0.01 39.07 0.22 288.11 0.01 36.83 O.OS 29.87 0.04 43.48 0.03 38.S2 0.32 199.26 0.19 SS8.87 0.02 183.3S 0.04 308.03 0.19277.21 0.04 4.S6 0.02 162.86 0.8S 82.76 0.8S 82.76 O.OS 3S.77 0.18280.00
0.99 0.90 1.61 1.32 0.77 0.86 0.93 0.88 1.70 1.88 1.21 0.96 1.36 0.81 0.81 0.74 0.66
0.00 3.70 1.10 2.20 0.00 0.00 4.30 S.70 1.60 2.70 3.S0 0.40 1.00 0.00 0.00 0.00 3.40
0.01 0.02 0.02 0.02 0.01 0.02 0.02 0.02 0.02 0.02 0.02 0.01 0.02 0.23. 0.23 0.00 0.02
Ag I
Ss-Sp Ss-6s Ss-6p Ss-Sd Sp-6s Sp-6p Sp-Sd 6s-6p 6s-Sd
189.97 6.10 20.24 13.98 162.11 48.7S 820.00 986.91 77.S6
1.82 0.47 0.62 0.56 1.06 0.38 1.89 0.39 0.08
0.00 0.00 0.00 0.10 0.00 0.10 0.10 0.70 0.00
0.07 0.03 0.12 0.02 0.10 0.04 O.OS 0.13 0.06
62.12 9.29 26.49 19.52 42.21 43.26 140.91 lS6.80 119.28
0.50 0.73 0.6S 0.67 0.87 1.21 0.61 0.86 1.84
1.70 0.00 0.00 0.00 4.80 1.80 4.80 9.90 1.60
0.02 0.00 0.03 0.01 0.03 0.02 0.02 0.04 0.02
Cd I
SiS-Sip S IS-6 IS SiS-SiD S IS-6 l p Slp-6 IS Sip_SiD Slp-6 l p
194.S9 4.44 17.94 29.17 269.74 1162.16 76.03
2.81 0.66 0.69 1.20 0.87 I.S4 0.19
0.00 0.10 0.00 0.00 0.00 0.30 0.00
O.OS 0.02 0.01 0.12 0.09 0.06 0.03
S7.54 S.78 26.70 26.20 66.26 lS4.64 114.68
0.42 0.63 0.74 0.46 1.01 0.63 1.12
1.30 0.00 0.00 0.00 6.30 7.10 0.60
0.01 0.01 0.01 0.01 0.02 0.02 0.02
6.1 Tables of Numerical Results Table 6.4. (continued) Atom Transition
C
D
R
0.71 0.17 0.45
3.90 0.50 2.40
0.02 0.03 0.02
0.67 0.85 0.42
4.90 0.50 2.40
0.03 0.02 0.03
0.18 162.58 0.02 17.44
0.54 1.08
1.50 0.30
0.02 0.02
0.00
0.16 42.80
0.68
3.70
0.02
1.03 0.13 0.29 0.12 0.19 0.15 0.00 0.92 0.33 0.87 0.21 0.03 0.02 0.03 1.12
0.30 0.00 0.00 0.60 0.30 0.00 1.00 0.00 0.00 0.60 0.00 0.00 0.90 0.90 0.30
0,07 0.02 0.02 0.11 0.02 0.02 0.15 0.14 0.13 0.16 0.04 0.02 0.35 0.11 0.09
80.69 55.13 18.03 41.66 6.68 15.99 191.12 72.16 66.24 57.17 170.92 20.70 21.00 63.48 169.13
0.85 0.87 1.11 0.55 0.66 2.13 1.19 1.03 1.57 0.74 1.60 0.90 0.77 0.90 0.80
7.90 0.00 0.90 0.00 0.00 0.90 9.90 8.20 3.40 9.90 1.70 0.00 2.40 3.20 9.20
0.02 0.00 0.02 0,0} 0.01 0.02 0.04 0.03 0.02 0.03 0.02 0.01 0.02 0.02 0.02
D
R
53p_53D
109.64 233.46 587.17
1.71 2.37 2.33
0.00 0.00 0.10
Inl
5p-6s 5p-6p 5p-5d
66.44 25.49 340.34
1.18 0.30 2.38
0.60 0.40 0.30
0.14 25.88 0.50 61.24 0.06 130.10 0.17 13.28 0.03 30.80 0.08 71.91
In II
5 1S-5 1P 5 1S-6 I S 53P-63S
362.32 9.61
0.90 0.28
0.00 0.00
162.86
1.16
482.05 29.52 14.48 33.30 4.59 6.84 812.31 370.22 90.97 466.25 136.19 10.35 39.98 128.76 1253.22
Cd I
53P-63S 53p~p
211
A
X
Cs I
6s-6p 6s-5d 6s-7s 6s-7p 6s-6d 6s-4f 6p-5d 6p-7s 6p-7p 6p-6d 6p-4f 5<1-7s 5d-7p 5d-6d 5d-4f
Ba I
6 1S-5 1D 6 1S-6 l p
6.24 319.72
0.11 1.32
0.00 0.20
0.04 11.63 0.07 69.95
0.86 0.72
0.00 4.70
0.01 0.02
5 1D-6 l p 5 10-7 1S 53 D-63P 530-73S 63P-73S
194.93
0.57
0.00
0.09 60.67 0.81
1.31 3.84
6.80 6.70
0.02 0.02
191.96
0.37
0.00
124.76
0.78
0.50
0.09 67.23 1.24 0.27 25.11
1.63 2.31 0.84
8.00 3.00 6.60
0.02 0.02 0.03
18.71 836.47 24.63 41.98 597.78 2.60 102.46 439.45 2135.33
0.01 0.03 0.14 0.17 0.04 0,07 0.13 0.54 0.70
0.00 0.90 0.00 0.40 0.80 0.30 0.10 0.00 0.00
0.04 42.83 0.27 355.84 0,0} 41.03 0,07 38.18 0.21 308.59 4.53 0.03 0,0} 158.29 0.24 134.20 0.20538.64
1.08 1.02 1.60 1.42 1.16 0.78 1.41 0.88 0.86
0.00 4.30 1.10 2.40 3.80 0.00 1.00 4.90 5.70
0.00 0.02 0.02 0.02 0.02 0.01 0.02 0.02 0.02
Ba II
6s-5d 6s-6p 6s-7s 6s-6d 5d-6p 5d-7s 5d-6d 6p-7s 6p-6d
Hg I
6 1S-6 l p 6 18-7 1S 6 1P-7 1S
195.00 10.02 309.30
2.95 0.29 1.01
0.40 0.00 0.00
0.08 44.18 0.02 14.91 0.08 68.78
0.39 0.82 0.96
1.80 0.20 6.50
0.02 0.02 0.02
63P-73S
168.16
1.70
0.10
0.14 36.45
0.69
4.20
0.02
212
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.5. Excitation of multiply charged ions. Normalized Coulomb-Bom-exchange cross sections for hydrogenlike ion Ne X. Parameters C, lp, D and A, X, D given below can be used for arty hydrogenlike ions with z > 3. Transition
C
ls-2s ls-2p Is-3s Is-3p Is-3d ls-4s Is-4p Is-4d Is-4f 2s-3s 2s-3p 2s-3d 2s-4s 2s-4p 2s-4d 2s-4f 2p-3s 2p-3p 2p-3d 2p-4s 2p-4p 2p-4d 2p-4f 3s-4s 3s-4p 3s-4d 3s-4f 3p-4s 3p-4p 3p-4d 3p-4f 3d-4s 3d-4p 3d-4d 3d-4f
3.42 65.74 2.25 34.74 1.33 1.97 28.24 1.46 0.02 17.64 168.98 55.08 8.12 71.75 16.06 8.70 11.25 57.98 789.52 4.23 26.75 261.84 32.88 52.74 405.74 122.48 57.08 70.33 190.45 1274.21 396.20 6.47 50.47 250.15 4204.00
lp
D
R
0.94 4.63 1.02 4.07 0.89 1.05 3.86 0.84 0.14 0.17 1.87 0.07 0.23 1.87 0.07 0.03 0.65 0.10 0.72 0.03 0.09 0.64 0.02 0.06 1.15 0.02 0.05 0.79 0.05 0.00 0.04 0.02 0.00 0.04 0.02
0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.10 0.00 0.00 0.70 0.00 0.00 0.70 0.80 0.00 0.20 0.00 0.90 0.30 0.00 0.90 0.00 0.00 0.80 0.30 0.00 0.10 1.00 0.60 0.50 0.90 0.10 0.90
0.02 0.08 0.03 0.12 0.38 0.04 0.14 0.40 0.39 0.01 0.13 0.08 0.01 0.13 0.09 0.09 0.63 0.01 0.29 0.66 0.02 0.29 0.21 0.03 0.17 0.22 0.14 0.56 0.03 0.45 0.15 0.11 0.30 0.03 0.35
A 5.90 23.92 4.20 16.34 2.65 3.79 14.60 3.55 0.29 32.45 34.82 64.69 15.15 19.11 24.72 14.46 5.90 122.67 431.23 4.10 66.44 200.66 39.02 105.23 49.19 80.69 85.15 10.50 364.70 453.05 393.76 10.54 42.37 531.28 2319.00
X 0.82 0.20 0.89 0.28 5.52 0.91 0.31 8.45 4.56 1.08 0.41 0.75 0.84 0.39 0.68 0.74 0.23 0.98 0.39 0.34 2.20 0.29 0.67 0.91 0.72 2.81 1.77 0.72 0.87 0.72 2.22 0.73 0.41 0.99 0.62
D
R
0.00 0.00 0.00 0.00 4.40 0.00 0.00 6.00 0.00 0.30 2.70 0.50 0.00 1.80 0.00 0.00 0.40 0.00 0.70 0.00 0.90 0.00 0.40 0.00 9.90 7.50 1.60 9.40 0.00 4.10 3.70 0.00 0.30 0.00 1.80
0.00 0.01 0.01 0.02 0.09 0.01 0.03 0.08 0.01 0.02 0.02 0.01 0.02 0.02 0.01 0.01 0.02 0.01 0.02 0.10 0.02 0.02 0.02 0.01 0.02 0.02 0.02 0.02 0.01 0.02 0.02 0.01 0.01 0.00 0.02
Table 6.6. Excitation of multiply charged ions. Normalized Coulomb-Born-exchange
cross sections for heliumlike ion Na x. Transitions with no change of spin (6S = 0) Parameters C, lp, D and A, X, D can be used for any heliumlike ion with z > 3 Transition 11 S-21 S 11 S-21 P 11 S-3 1 S
C 3.31 62.45 2.25
qJ
1.43 5.56 1.64
D 0.10 0.50 0.20
R 0.02 0.04 0.01
A
X
D
R
3.77 10.57 2.38
0.60 0.31 0.56
0.10 1.70 0.10
0.02 0.01 0.02
6.1 Tables of Numerical Results Table 6.6. (continued) Transition
C
qJ
D
R
R
41.37 1.70 2.01 36.13 1.96 0.02
6.90 3.76 1.78 7.33 3.99 1.69
0.50 0.70 0.20 0.50 0.70 0.00
0.04 0.07 0.Ql 0.06 0.08 0.33
6.37 0.31 2.05 5.46 0.35 0.02
X 0.32 0.44 0.54 0.32 0.43 0.55
D
IIS-3 IP IIS-3 ID IIS-4 IS IIS-4IP IIS-4ID IIS-4IF
1.80 3.20 0.10 1.80 3.10 0.00
0.Ql 0.02 0.02 0.02 0.02 0.08
zIS-2lp 21S-3 1S 2 1S-3 1P 2 1S-3 1D zIS-4 IS 2 1S-41P 2 1S-41D zIS-4IF 21P-3 1S 21P-3 1P 21p-3 1D 21P-4 1S 21p-41p 21p-41D zIP-4 IF
409.42 17.37 166.30 55.29 8.14 70.82 17.46 8.20 21.23 58.14 836.51 8.47 27.18 291.36 38.25
0.03 0.20 2.46 0.20 0.28 2.16 0.32 0.00 2.84 0.18 0.89 2.56 0.24 0.95 0.51
0.50 0.00 0.00 0.50 0.00 0.20 0.40 1.00 0.00 0.00 0.00 0.00 0.00 0.00 0.30
0.10 0.02 0.09 0.07 0.03 0.12 0.04 0.08 0.04 0.02 0.23 0.08 0.02 0.19 0.07
290.52 29.40 23.32 47.55 12.86 11.51 15.60 6.44 2.59 103.91 373.36 1.54 48.39 155.65 23.51
1.99 1.63 0.50 1.08 1.76 0.55 1.03 1.83 0.38 0.87 0.48 0.36 0.79 0.48 0.95
4.80 1.10 4.70 1.80 1.40 4.50 1.50 4.20 4.30 0.10 1.30 2.60 0.00 0.90 2.30
0.02 0.02 0.02 0.02 0.02 0.03 0.02 0.01 0.02 0.02 0.02 0.02 0.02 0.02 0.02
3 1S-4 1S 3 1S-41P 31S-41D 3 1S-41F 31P-4 1S 3 1P-41P 3 1P-41D 31P-41F 3 1D-4 1S 3 1D-41p 3 1D-41D 3 1D-41F
5l.98 387.56 116.56 56.59 99.72 190.96 1463.19 380.73 6.80 50.17 247.32 4214.
0.06 1.41 0.03 0.10 1.41 0.06 0.56 0.90 0.13 0.02 0.05 0.02
0.00 0.00 0.80 0.10 0.00 0.10 0.00 0.30 0.20 0.90 0.00 0.90
0.04 0.11 0.22 0.16 0.27 0.04 0.31 0.19 0.27 0.32 0.02 0.35
102.46 41.23 68.13 64.90 10.43 354.90 427.74 341.30 5.48 25.18 505.88 2237.
0.89 0.65 2.91 2.85 0.61 0.92 0.74 2.51 2.54 0.90 0.93 0.64
0.00 9.90 8.90 4.40 9.90 0.10 4.50 5.10 5.80 3.20 0.00 2.00
0.01 0.02 0.02 0.02 0.05 0.02 0.02 0.01 0.02 0.02 0.Ql 0.02
23S_23P 23S-3 3S 23S_3 3P 23S-3 3D 23S-43S 23S_43P 23S-43D 23S-43F 23P_3 3S
361.31 16.59 146.76 51.27 7.82 68.41 16.82 7.36 16.66
0.Ql 0.19 2.41 0.09 0.26 2.43 0.10 0.05 1.27
0.70 0.00 0.00 0.70 0.00 0.00 0.70 0.80 0.00
0.10 0.02 0.08 0.09 0.01 0.08 0.10 0.11 0.37
270.49 29.62 22.56 54.73 13.75 14.29 22.59 10.68 4.91
1.48 1.22 0.46 0.82 1.12 0.39 0.56 0.81 0.27
3.10 0.50 3.90 0.80 0.40 2.30 0.00 0.30 1.40
0.Ql 0.02 0.02 0.01 0.02 0.03 0.Ql 0.02 0.01
A
213
214
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.6. (continued) Transition 23p_3 3p 23p_3 3D 23P-43S 23p_4 3p 23p_43D 23p-43F 33S-43S 33S_43P 33S-43D 33S-43F 33P-43S 33p_43p 33p_4 3D 33p_4 3F 33D-43S 33D_4 3p 33D-43D 33D-43F
C
D
qJ
A
R
X
D
R
0.00 0.02 0.03 0.01 0.02 0.02 0.01 0.02 0.02 0.02 0.03 0.02 0.02 0.02 0.02 0.02 0.00 0.02
56.23 772.12 5.64 26.31 269.86 30.56
0.13 0.79 0.73 0.11 0.75 0.03
0.10 0.00 0.00 0.30 0.00 0.90
0.02 0.27 0.54 0.02 0.26 0.22
114.22 390.74 3.40 58.49 181.43 33.07
0.92 0.42 0.21 1.04 0.37 0.58
0.00 0.90 0.10 0.00 0.30 0.40
50.54 350.20 106.33 56.00 98.32 187.59 1351.28 391.17 7.65 53.06 250.60 4199.
0.06 1.41 0.02 0.06 1.15 0.05 0.55 0.04 0.01 0.00 0.04 0.02
0.00 0.00 0.80 0.30 0.00 0.10 0.00 0.60 0.70 0.90 0.10 0.90
0.04 0.13 0.22 0.14 0.37 0.03 0.34 0.15 0.20 0.35 0.03 0.35
100.15 37.00 66.88 76.69 11.50 356.10 403.69 371.17 9.49 37.24 522.72 2302.
0.90 0.64 2.72 2.15 0.65 0.86 0.72 2.26 1.44 0.50 0.97 0.61
0.00 9.90 7.70 2.40 9.90 0.00 4.30 4.00 1.40 0.90 0.00 1.80
Table 6.7. Normalized cross sections for intercombination transitions (AS = 1) Atom
Transition
He I
lIs-is IIS-2IP IIS-3 IS IIS-3 IP IIS-3 ID IIS-4 IS IIS-4IP IIS-4ID IIS-4IF 23S-2 1S
23 S-ip 23S-3 1S 23S-3 1P 23S-23D
is-23p is-3 3S
is-3 3p is-3 3 D 23p-2 1 p 23P-3 1S
C
qJ
D
R
22.66
0.69
2.60
0.31
27.63
0.37
3.70
0.38
28.54
0.34
3.90
0.38
X
D
R
1.10 9.92 1.91 12.18 0.75 2.14 12.94 0.98 0.Q3
2.25 1.88 3.68 2.37 0.73 4.06 2.52 0.74 0.93
0.20 0.20 0.20 0.20 0.00 0.20 0.20 0.00 0.00
0.03 0.04 0.Q3 0.04 0.07 0.Q3 0.04 0.07 0.14
9.38 22.20 13.66 15.76 88.17 13.13 4.93 19.10 108.73 19.58 17.22
1.77 1.78 3.89 2.16 4.80 1.69 2.59 4.26 5.50 1.04 3.70
0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00
0.04 0.02 0.02 0.02 0.01 0.04 0.04 0.03 0.01 0.05 0.02
A
6.1 Tables of Numerical Results
215
Table 6.7. (continued) Atom
Lill
Transition 23p_3 1p 23p_3 1D 21P_3 3S 21p_3 3p 21p_3 3D 11S-23S 11S-23P 11S-3 3S 11S_3 3P 11S-3 3D 23S-2 1S 23S-21P 23S-3 1S 23S_3 1P 23S-3 1D is-23p 2 1S-3 3S is-3 3p is-3 3D 23p_2 1p 23P-3 1S 23p_3 1p 23p_3 1D 21P-3 3S 21p_3 3p 21p_3 3D
Mg IX
2 1S-23P is-23p 2 1S-23P 2 1S_23P is-23p 2 1S-23P 3 1S-3 3P 31S-43S 3 1S_43P 31S-3 3D 33p_3 1p 33P-4 1S 33p_3 1D 33p_4 1p 2 1S_23P
AlII
3 1S-3 3P
Be I BII CIII OV F VI Na VIII MgI
C
D
R
1l.43
l.20
l.20
0.42
1l.64
l.23
1.40
0.48
X
D
R
36.07 166.02 14.15 40.87 159.60
3.89 5.17 3.22 4.57 4.81
0.10 0.00 0.00 0.10 0.00
0.05 0.04 0.01 0.06 0.03
0.04 7.20 0.04 6.35 l.53
0.87 0.45 0.85 0.40 0.90
9.90 0.00 9.90 0.00 0.00
0.33 0.05 0.34 0.06 0.02
12.95 25.83 8.42 9.80 52.71 14.93 6.10 6.54 50.03 41.35 9.70 22.67 107.21 14.98 19.92 123.15
3.64 3.60 5.78 3.20 4.79 3.27 4.59 2.50 4.77 l.87 3.28 l.64 3.63 4.25 l.69 3.94
0.00 0.00 0.10 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00
0.04 0.03 0.08 0.04 0.03 0.03 0.04 0.02 0.02 0.02 0.03 0.05 0.01 0.02 0.05 0.01
10.55 14.67 10.16 6.83 7.55 7.05
0.80 l.76 2.37 2.05 2.09 2.15
0.00 0.00 0.00 0.00 0.00 0.00
0.04 0.01 0.04 0.02 0.02 0.02
15.38 2.36 11.54 64.55 38.63 5.74 185.98 37.61
0.95 0.92 1.31 2.36 l.66 l.59 4.44 3.46
0.00 0.00 0.00 0.00 0.00 0.00 0.10 0.10
0.05 0.08 0.02 0.02 0.03 0.04 0.06 0.05
7.01
2.21
0.00
0.02
35.75
3.87
0.00
0.02
A
216
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.7. (continued) Atom Ca I
Zn I
Ga II
Sr I
Cd I
In II
Ba I
Transition 4 1S_43P 4 1S-3 3D 4 3p-4 1p 43p-3 1D 4 1S_43P 4 1S-5 3S 4 1S_53P 4 1S-43D 43p-4 1p 43P-5 1S 43p-41D 43p-5 1D 4 1S_43P 4 1S-53S 4 1S-43D 43p-4 1p 43P-5 1S 43p-41D 51S_5 3P 5 1S-43D 51S-63S 51S_63P 53p-41D 53P-5 1P 53P-6 1S 53p-6 1p 43D-5 1P 51S-5 3P 51S-63S 51S_63P 51S-5 3D 53P-5 1P 53P-6 1S 53p-5 1D 53P-6 1P 51S-53P 51S-63S 53P-5 1P 53P-6 1S 6 1S-5 3D 6 1S_63P 6 1S-73S
C
D
R
X
D
R
20.73 34.57 37.l9 31.84
1.54 2.12 1.78 1.42
0.00 0.00 0.00 0.00
0.04 0.02 0.00 0.Q1
13.08 1.64 10.63 36.60 32.85 8.37 222.55 35.37
0.68 0.73 1.04 1.90 1.40 3.75 6.75 3.27
0.00 0.00 0.00 0.00 0.00 0.10 0.10 0.10
0.06 0.03 0.02 0.02 0.04 0.08 0.06 0.04
37.95 7.66 62.19 72.04 16.86 127.73
3.53 4.37 4.24 3.02 4.45 2.81
0.00 0.00 0.00 0.00 0.00 0.00
0.02 0.04 0.03 0.Q1 0.Q1 0.Q1
25.27 43.30 8.71 23.66 36.50 39.25 8.87 29.75 22.87
1.99 2.38 3.08 3.l3 1.47 2.07 2.14 2.89 1.40
0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00
0.03 0.Q1 0.03 0.02 0.02 0.Q1 0.05 0.02 0.07
15.11 2.l3 11.86 45.80 35.l7 8.47 241.55 33.72
0.80 0.91 1.27 2.32 1.49 3.70 7.05 3.41
0.00 0.00 0.00 0.00 0.00 0.l0 0.l0 0.10
0.08 0.09 0.02 0.02 0.03 0.06 0.08 0.05
40.08 6.08 89.74 20.63
4.32 4.49 4.11 5.93
0.00 0.00 0.00 0.00
0.03 0.04 0.Q1 0.02
12.56 22.01 5.62
1.30 1.71 2.48
0.00 0.00 0.00
0.04 0.03 0.03
A
6.1 Tables of Numerical Results
217
Table 6.7. (continued) Atom
Hg I
A
X
D
R
53 D-6 1P 53 D-7 1 S 5 1D_63 p
16.62 6.85 11.02
1.12 1.90 0.65
0.00 0.00 0.00
0.08 0.05 0.13
61 S_63 p 6 1 S-73 S 63 p-6 1P 63 P-7 1 S 6 1P_7 3 S
19.83 3.84 37.16 12.30 21.52 13.63
1.17 1.34 1.61 4.18 4.36 3.94
0.00 0.00 0.00 0.10 0.00 0.00
0.08 0.12 0.01 0.06 0.04 0.01
Transition
C
D
R
73 S-is
Table 6.S. Excitation of multipy charged ions. Normalized exchange cross section for heliumlike ion Na X. Intercombination transitions (LIS = 1). Parameters C, q>, D and A, X, D can be used for any heliumlike ion with z > 3. Transition
C
q>
D
R
A
X
D
R
IS-2S IS-2P IS-3S IS-3P IS-3D IS-4S IS-4P IS-4D IS-4F 2S-3S 2S-3P 2S-3D 2S-4S 2S-4P 2S-4D 2S-4F 2P-3S 2P-3P 2P-3D 2P-4S 2P-4P 2P-4D 2P-4F 3S-4S 3S-4S 3S-4P 3S-4D 3S-4F 3P-4S
2.45 4.61 2.27 4.50 0.36 2.30 4.35 0.46 0.01
1.31 0.81 1.52 0.84 0.52 1.37 0.90 0.57 0.36
1.00 0.50 1.00 0.60 0.30 1.10 0.60 0.30 0.10
0.09 0.11 0.08 0.10 0.21 0.08 0.10 0.21 0.35
1.59 10.64 1.49 9.57 2.29 1.53 9.13 2.83 0.17 2.10 5.42 16.26 1.92 4.90 11.33 8.76 4.02 26.37 65.05 3.65 23.65 54.02 22.88 2.01 2.01 4.54 8.38 20.05 3.87
0.69 1.12 0.69 1.09 1.60 0.70 1.08 1.57 2.14 3.33 3.46 3.47 3.35 3.44 3.23 4.51 3.06 3.64 4.42 3.05 3.65 4.25 5.53 6.90 6.90 7.02 7.17 6.76 6.44
0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00
0.02 0.03 0.02 0.03 0.02 0.02 0.03 0.02 0.02 0.03 0.03 0.03 0.04 0.03 0.03 0.03 0.03 0.03 0.02 0.03 0.03 0.03 0.02 0.02 0.02 0.02 0.02 0.02 0.03
218
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.8. (continued) Transition 3P-4P 3P-4D 3P-4F 3D-4S 3D-4P 3D-4D 3D-4F
C
D
qJ
R
A
17.28 32.97 58.74 6.48 24.22 50.84 121.00
X
6.79 8.34 7.55 6.77 7.53 7.86 8.86
D 0.00 0.00 0.00 0.00 0.00 0.00 0.00
R
0.02 0.01 0.02 0.02 0.02 0.02 0.02
6.1.5 Transitions between Closely Spaced Levels (Tables 6.9-10)
In the case of transitions between closely spaced levels under the conditions AE ~ Eo, Eland AE ~ Iff, the dependence of multipole and exchange cross sections calculated by means of the first-order methods on AE is almost absent. For the optically allowed transitions (AI = 1) a weak logarithmic dependence exists. The calculations for multiply-charged ions have been made using the Coulomb-Born approximation for transitions with no change of spin (AS = 0) and using the orthogonalized functions method for intercombination transitions. The data of Tables 6.9 and 6.10 were obtained for a set of values of AE and can be applied to arbitrary multiply-charged ions with z > 3. For quadrupole and intercombination transitions the value of AE is not important. For dipole transitions one has to interpolate data for particular values of AE. The fitting formulas and the range of analytic approximation are quite the same as in Sect. 6.1.4. 6.1.6 Ionization Cross Sections (Table 6.11 and 6.12)
The ionization cross sections have been calculated in accordance with (3.1.38) in the partial wave representation. In cases of ions the Coulomb-Born approximation has been used:
O'i(aO)
= QiO'(lO),
(vO'i(ao»)
u
= Qi(VO'i(lO»)
= (Iff - EO)/z2
P= z2
DE
Ry/T,
= z2
Ry ,
.
(6.1.18) (6.1.19)
Ry,
p = EO/z2 Ry.
The fitting formulas and the angular factors Qi are given by (5.1.21-25). For the total cross section of ionization from a shell 1'0,
Qi=m,
(6.1.20)
where m is a number of equivalent electrons. The set of parameters C, cp,D is adjusted for the range 0.0625 < u < 64, and the set A,X,D, for 0.125 < P < 8.
Table 6.9. Transitions between the closely spaced levels with no change of spin (LIS Coulomb-Born-exchange cross sections for multiply charged ions Transition
1:l.E/z2
C
cp
R
D
A
[cm- I ]
= 0)
The
X
D
R
0.96 1.72 2.06 2.16 1.96 1.72 1.52 1.42 1.66 2.10 2.24 2.19 1.89 1.55 1.47 1.68 2.11 2.24 2.15 1.84 1.55 1.46
1.60 4.00 4.80 4.30 3.20 2.30 1.70 1.40 4.10 5.20 4.60 3.70 2.60 1.70 1.40 4.10 5.20 4.60 3.60 2.50 1.70 1.40
0.02 0.02 0.02 0.01 0.02 0.02 0.02 0.02 0.02 0.02 0.02 0.01 0.02 0.02 0.02 0.Q2 0.02 0.02 0.01 0.02 0.Q2 0.02
1.15 1.14 1.69 0.85 0.84 0.87 0.87 0.85 0.93
0.70 0.70 1.20 0.00 0.00 0.00 0.00 0.00 0.10
0.02 0.02 0.02 0.Q2 0.02 0.Q1 0.02 0.02 0.02
Dipole transitions 2s-2p 2s-2p 2s-2p 2s-2p 2s-2p 2s-2p 2s-2p 2s-2p 3s-3p 3s-3p 3s-3p 3s-3p 3s-3p 3s-3p 3s-3p 3p-3d 3p-3d 3p-3d 3p-3d 3p-3d 3p-3d 3p-3d
1480. 740. 370. 185. 93. 46. 23. 12. 856. 428. 214. 107. 54. 27. 13. 856. 428. 214. 107. 54. 27. 13.
2p-2p 2p-2p 3s-3d 3s-3d 3s-3d 3p-3p 3p-3p 3d-3d 3d-3d
100. 10. 1000. 100. 10. 100. 10. 100. 10.
321. 389. 433. 491. 531. 589. 647. 704. 1849. 2163. 2439. 2762. 3092. 3436. 3677. 2356. 2738. 3080. 3482. 3892. 4319. 4617. 13.53 13.51 51.26 51.64 51.53 91.07 91.17 75.06 75.09
0.Q1 0.01 0.02 0.Q1 0.01 0.01 0.01 0.00 0.Q1 0.03 0.02 0.Q1 0.Q1 0.01 0.01 0.01 0.03 0.02 0.Q1 0.01 0.01 0.Q1
0.70 0.15 0.08 0.70 0.50 0.09 0.50 0.06 0.08 0.40 0.06 0.40 0.40 0.05 0.40 0.04 0.12 0.70 0.50 0.10 0.40 0.10 0.08 0.40 0.40 0.06 0.05 0.40 0.30 0.07 0.70 0.11 0.50 0.10 0.40 0.10 0.40 0.08 0.40 0.06 0.40 0.05 0.07 0.30 Quadrupole transitions 0.00 0.30 0.03 0.00 0.04 0.30 0.Q1 0.20 0.05 0.00 0.20 0.04 0.00 0.20 0.04 0.00 0.10 0.03 0.00 0.10 0.03 0.00 0.03 0.10 0.00 0.10 0.03
265. 269. 315. 406. 524. 650. 773. 883. 1232. 1492. 2024. 2671. 3403. 4173. 4890. 1588. 1904. 2565. 3387. 4304. 5242. 6132. 20.46 20.37 86.06 96.24 95.54 178.25 178.31 144.24 143.78
Table 6.10. Intercombination transitions between the closely spaced levels (LIS = I). The summed over K exchange rate coefficients for multiply charged ions Transition 2s-2s 2s-2p 2p-2p 3s-3s 3s-3p 3s-3d 3p-3p 3p-3d
1:l.E/z2 200. 747. 200. 20. 210. 252. 20. 42.
[cm- I ]
A 6.00 7.84 62.32 6.08 9.00 15.36 41.08 47.72
X 3.07 2.83 3.51 6.62 7.80 8.35 7.15 8.59
D
R
0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00
0.03 0.02 0.03 0.02 0.02 0.01 0.02 0.01
220
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.11. Ionization cross sections for atoms and ions in Coulomb-Born approximation Atom Level A D R C D R cp X Is 2s 2p 3s 3p 3d 4s 4p 4d 4f 5s 5p 5d 5f 5g
9.581 32.6 86.9 66.9 175.0 294.0 106.0 283.0 483.0 680.0 145.0 396.0 674.0 956.0 1296.0
2.37 0.13 0.33 0.03 0.11 0.08 0.00 0.01 0.00 -0.01 -0.01 -0.02 -0.03 -0.03 -0.03
0.60 0.00 -0.60 -0.50 -0.80 -0.80 -0.70 -0.80 -0.80 -0.80 -0.80 -0.80 -0.80 -0.80 -0.80
0.07 0.11 0.08 0.11 0.10 0.12 0.13 0.11 0.12 0.21 0.16 0.12 0.13 0.19 0.28
7.371 198.5 430.0 746.3 1961.0 3462.0 2084.0 5919.0 10416.0 17566.0 4445.0 13595.0 24815.0 35980.0 57240.0
0.12 -0.70 0.01 21.45 5.10 0.05 5.25 1.00 0.02 15.23 1.60 0.03 9.00 0.60 0.02 7.11 0.20 0.01 19.66 1.00 0.02 15.61 0.50 0.02 14.02 0.30 0.02 14.32 0.10 0.00 0.80 0.02 26.75 25.52 0.50 0.02 25.57 0.40 0.02 22.74 0.20 0.01 23.95 0.00 0.01
lIS 23S 23p 21S
5.986 19.67 88.1 25.3 88.0
4.50 0.21 0.44 0.16 0.34
3.50 0.20 -0.60 0.10 -0.60
0.05 0.11 0.07 0.12 0.08
1.583 86.14 366.8 128.4 426.8
0.16 -0.10 0.02 17.47 5.60 0.06 5.65 1.50 0.03 18.37 5.10 0.06 5.42 1.10 0.02
Is
2s 2p 3s 3p 3d
9.570 32.45 85.1 66.2 176.0 287.0
2.41 0.22 0.40 0.07 0.09 0.11
1.10 0.00 -0.60 -0.50 -0.70 -0.80
0.07 0.12 0.05 0.12 0.09 0.03
4.500 89.60 295.6 406.4 1388.0 2548.0
0.25 -0.10 0.04 13.12 7.20 0.06 3.81 1.10 0.02 1.60 0.03 8.30 6.37 0.60 0.02 5.65 0.30 O.oI
Li I
2s 2p 3s 3p 3d
13.80 88.7 34.1 179.0 294.0
0.24 0.40 0.08 0.13 0.08
0.00 -0.60 -0.70 -0.80 -0.80
0.06 0.08 0.03 0.12 0.12
77.41 389.9 386.5 1913.0 3458.0
16.35 5.45 9.60 9.65 7.12
4.10 1.30 0.70 0.80 0.20
0.04 0.02 0.02 0.02 0.01
Li II
lIS 23S 21S 23p 21p
8.046 25.00 29.41 85.3 85.7
2.68 0.30 1.33 0.49 0.41
4.00 0.20 -0.80 -0.60 -0.60
0.07 0.11 0.09 0.07 0.05
1.872 44.27 60.58 259.3 294.2
0.20 7.56 9.83 3.89 3.95
0.30 6.00 6.80 1.40 1.20
0.02 0.07 0.07 0.03 0.02
Bel
2 1S 2~P 21p
BI
2p
8.56 64.51 88.5 53.08
0.73 1.05 0.56 1.70
0.60 0.10 -0.50 0.60
0.08 0.09 0.08 0.08
11.87 77.73 285.4 36.56
0.17 -0.80 0.09 0.13 -0.80 O.oI 7.85 3.30 0.04 0.29 -0.30 0.04
CI
2s 2p3p 2plD 2p l S
4.529 36.88 41.11 47.58
3.25 2.60 2.30 1.88
1.10 1.70 1.30 0.90
0.05 0.10 0.08 0.07
HI
He I
ip He II
2.349 12.47 16.79 25.70
0.18 -0.40 0.01 0.36 0.50 0.02 0.36 0.30 0.02 0.30 -0.10 0.02
6.1 Tables of Numerical Results
221
Table 6.11. (continued) Atom
cn CIll
C IV CV
NI 01
on o III o IV OV
o VI FI Ne I Na I
MgI
MgIX
Level 2p 2 1S 23 p 21p 2s 2p lIS 23 S 23 p 2p 28 2p 2s 2p 2s 2p 2s 2p 21S 23 p 21p 2S 2p 2p 38 3p 3d 31S 33 p 31P
is 23 p
ip MgX
2s 2p
Mg XI ArI KI
lIS
Ca I
3p 48 1 4 S 43 p 33 D 3 1D
C
A
D
R
ffJ
D
R
67.48
1.01
0.00
0.11
74.04
0.23 -0.60 0.04
21.63 76.3 84.6 25.86 84.4
0.31 0.40 0.34 0.23 0.42
0.50 -0.10 -0.30 0.30 -0.60
0.10 0.09 0.09 0.11 0.08
31.72 165.9 239.8 53.42 302.0
0.17 -0.80 0.05 11.48 8.20 0.05 6.21 3.00 0.04 9.73 6.70 0.07 4.89 1.60 0.03
9.203 29.04 83.4 26.43 2.644 24.92 8.321 50.62 13.67 66.66 19.41 75.1
1.42 0.19 0.40 3.78 3.66 3.64 2.56 1.88 0.92 0.74 0.40 0.41
3.80 0.20 -0.60 3.00 8.00 2.70 1.50 0.80 0.80 0.20 0.70 0.00
0.05 0.11 0.07 0.10 0.04 0.06 0.12 0.08 0.11 0.11 0.11 0.10
3.519 0.21 -0.10 0.02 76.64 12.60 7.00 0.06 4.89 312.3 1.50 0.03 0.25 0.70 0.02 5.18 0.485 -0.11 -0.10 0.01 0.19 5.45 0.30 0.01 0.45 2.540 1.10 0.03 0.54 0.90 0.03 21.90 0.23 -0.50 0.04 11.63 0.11 -0.80 0.03 80.48 24.52 0.13 -0.80 0.02 9.42 7.40 0.05 143.3
23.95 79.1 83.9 28.03 17.07 13.17 13.06 85.2 296.0
0.26 0.31 0.33 0.19 5.88 5.82 0.42 0.26 0.09
0.50 -0.20 -0.40 0.30 5.00 6.50 -0.60 -0.70 -0.80
0.11 0.08 0.09 0.10 0.06 0.03 0.02 0.11 0.11
37.80 226.1 273.7 66.22 1.98 1.39 83.04 553.7 3362.0
5.43 7.11 5.95 11.34 0.10 0.09 8.29 5.03 6.89
9.21 68.4 77.3
0.68 0.57 0.32
-0.40 -0.40 -0.70
0.03 0.08 0.10
39.92 209.8 464.8
9.37 6.26 4.99
27.47 80.4 83.1 29.94 83.7
0.20 0.32 0.35 0.17 0.29
0.40 -0.40 -0.50 0.30 -0.50
0.10 0.08 0.08 0.10 0.07
57.88 272.0 304.3 80.34 331.4
9.80 5.79 5.79 12.65 5.37
9.477 3Q.62 16.36
1.23 1.95 0.36
3.20 1.70 -0.60
0.06 0.41 0.05
0.71 0.53 0.39 0.39
-0.40 -0.50 0.60 0.40
0.11 0.14 0.14 0.15
12.31 88.3 174.1 188.4
4.417 18.03 92.98 34.93 285.1 200.9 234.6
X
4.40 3.50 2.40 6.90 0.40 0.30 1.50 0.50 0.20
0.08 0.04 0.03 0.07 0.01 0.01 0.02 0.02 0.02
2.90 0.03 2.60 0.03 0.60 0.02 6.50 2.20 2.00 6.80 1.60
0.07 0.03 0.03 0.06 0.03
0.23 -0.20 0.02 0.73 0.70 0.06 6.23 1.10 0.02 2.40 0.03 5.37 4.35 1.40 0.03 0.12 -0.80 0.02 0.13 -0.80 0.03
222
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.11. (continued) Atom
Cu I Krl Rb I
Sr I
Sr II Ag I Xe I Cs I
Ba I
Ba II
Hg I
Level
C
41p
99.4
0.42
-0.60
0.09
405.2
4s 4p 5s 5p 4d SiS 53 p 43D 41D Sip
10.27 39.98 16.32 95.7 306.0 13.22 99.7 236.3 39.77 117.9 25.0 325.5 11.28 46.68 19.2 125.3 297.0
0.75 2.47 0.42 0.23 0.30 0.59 0.54 0.46 1.59 0.36 0.18 0.22 0.71 1.87 0.38 0.22 0.23
-0.30 1.70 -0.60 -0.70 -0.80 -0.50 -0.50 0.70 1.40 0.20 0.20 0.60 0.60 1.60 0.10 0.10 0.40
0.04 0.31 0.05 0.05 0.13 0.04 0.11 0.14 0.09 0.13 0.03 0.16 0.04 0.18 0.05 0.08 0.16
37.25 16.19 77.12 624.6 1926.0 56.38 331.0 393.7 36.03 585.7 144.2 785.6 40.13 35.78 122.0 869.6 1128.0
13.17 5.40 0.04 0.60 1.00 0.05 5.69 1.30 0.02 6.07 0.80 0.02 7.56 1.30 0.03 8.94 2.90 0.03 7.97 3.20 0.04 6.67 5.40 0.07 0.20 -0.60 0.03 9.49 2.50 0.04 5.44 0.90 0.02 8.18 4.90 0.05 18.90 8.30 0.04 0.34 -0.30 0.03 6.53 1.00 0.02 6.49 0.80 0.02 4.20 0.05 1l.l0
14.52 153.3 163.3 96.6 27.3 352.1 127.0
0.51 0.45 0.38 0.43 0.14 0.21 0.16
0.20 2.70 2.60 0.20 0.20 0.60 0.00
0.05 0.09 0.09 l.l0 0.02 0.16 0.04
73.18 100.5 118.8 399.1 171.0 883.3 1018.0
6.39 1.40 0.02 0.22 -0.40 0.01 0.20 -0.50 0.01 4.96 1.20 0.03 5.58 0.80 0.02 6.90 3.80 0.05 5.52 0.40 0.02
9.67 89.2 114.9
0.24 0.22 0.85
2.60 1.80 0.10
0.12 0.13 0.12
18.60 129.9 413.2
12.23 8.50 0.16 0.18 -0.80 0.12 12.41 4.90 0.05
5s 4d 5s 5p 6s 6p 5d 6 1S 53 D SiD 63 p 6s 5d 6p 6 1S 63 p 6 1P
D
qJ
A
R
Table 6.12. Rate coefficients of dielectronic recombination in Coulomb-Born-exchange approximation. Parameters and Xd.
He II BeN
C VI
o VIII NeX Mg XII SiXN
S XVI
IXo (XI H-like ions Is - 2p Is - 2p Is - 2p Is - 2p Is - 2p Is - 2p Is - 2p Is - 2p
31.18 36.69 31.34 25.78 21.06 17.20 14.08 11.56
0.74 0.73 0.71 0.69 0.67 0.66 0.64 0.63
A.I
X
6.91
D
R
2.10 0.03
6.1 Tables of Numerical Results
223
Table 6.12. (continued) Xz+1
IXo
(XI
A.i
CaXX Fe XVI
Is Is He-like lIS lIS lIS lIS lIS lIS lIS lIS lIS lIS lIS lIS lIS lIS lIS lIS lIS -
2p 2p ions 21p
7.828 4.420
0.61 0.60
17.43 22.21 0.024 18.21 0.078 14.37 0.170 11.16 0.309 8.659 0.495 6.738 0.714 4.144 1.151 2.138 1.500
1.13 0.85 0.90 0.79 0.85 0.75 0.82 0.72 0.80 0.69 0.78 0.68 0.75 0.66 0.71 0.64 0.65
10.81 6.405 3.706 2.400 1.690 1.182 .9387 .6229 .5012
0.07 0.04 0.02 0.02 0.01 0.01 0.01 0.01 0.01
21.07 11.62 7.010 5.665 4.663 1.003
0.10 0.06 0.04 0.03 0.03 0.01
Li II CV CV o VII o VII NeIX Ne IX Mg XI Mg XI Si XIII Si XIII S XV SXV CaXIX Ca XIX Fe XXV Fe XXV Be II C IV o VI Ne VIII MgX Si XII S XIV Ca XVIII Fe XXIV CIII
ov
Ne VII Na VIII Mg IX Fe XXIII
ip 23 p
ip 23p
ip 23p
ip 23 p
ip 23p
ip 23 p
ip 23 p
ip
23 p Li-like ions 2s - 2p 2s - 2p 2s 2p 2s - 2p 2s - 2p 2s 2p 2s - 2p 2s - 2p 2s - 2p Be-like ions 21p 2 1S
is - ip 21S - ip is ip 21S - ip ip 2 1S
Xd
6.1.7 Dielectronic Recombination Rate Coefficients (Table 6.12) The methods of calculations of the rate coefficients for the dielectronic recombination process,
Xz+\(IXo) + e
--+
Xz(lX\nl)
--+
Xz(lXonl)
+ fut),
224
6. Tables and Formulas for the Estimation of Effective Cross Sections
are described in Sect. 5.2. The simplified model (5.2.12) with its modification (5.2.29) for s - p transitions was used. The excitation cross section for the transition IXo - 0(1 of an ion XZ+I has been calculated in the Coulomb-Born approximation with exchange whenever it has been substantial. The rate coefficient for dielectronic recombination connected with the transition IXo - IXI is expressed in the form
f3
=
(z
+ 1)2Ry T
.
(6.1.21) Parameters Ad and Xd for the most important actual cases are given in Table 6.12 and the angular factors Qd for these cases are given by
Qd(nolO', nol:;'-lnI1d = m, Qd(noltnllf', nol:-lnllf'+I)
=N
(1- 2(21~+ 1»)·
(6.1.22)
In the case of heliumlike ions the total rate coefficient for dielectronic recombination is the sum of contributions from excitation of both singlet and triplet P levels.
6.2 Formulas Defining the Angular Factors 6.2.1
Rules for the Addition of Cross Sections
In various applications, cross sections are required for transitions between separate levels, between two groups of closely spaced levels, for transitions from a given level to a group of levels, and for transitions from the whole group of levels to a given level. For example, one may be interested in transitions between separate fine structure components LoSoJo - LISIJI of two terms or in the transition between the terms LoSo - LISI as a whole. The cross section for transition from a given level a of the group A to the group B of levels b is, clearly, a(Aa, B)
= L a(Aa, Bb) ,
(6.2.1 )
b
where a(Aa, Bb) is the cross section for the transition a-b. If every level a of the group A is populated proportionally to its statistical weight, then the cross section for the transition A - Bb is defined by a(A, Bb)
=
1 g(A) ~g(a)a(Aa, Bb),
(6.2.2)
and the cross section for the transition A - B, by 1 a(A, B) = g(A) ~g(a)a(Aa, Bb) .
(6.2.3)
6.2 Formulas Defining the Angular Factors
225
La
Here g(a) is the statistical weight of level a, and g(A) = g(a) is the statistical weight of the group of levels A. The tabulated cross sections are given by formulas (6.1.1,2) where the dependence of effective cross sections on angular momenta is determined by the factors Q~ and Q~. Therefore the summation of the cross sections over the finestructure components of terms and over the terms belonging to a single electronic configuration is equivalent to the summation of these angular factors. The next subsections give a summary of formulas defining the factors Q~ and Q~ for the cases which can be met when using the tables of cross sections given in Sect. 6.1. 6.2.2
LS-Coupling; Q" for transitions between levels LSI
In this and the following subsections we give general formulas for Q-factors in the LS-coupling. The derivation for transitions not involving the shells of equivalent electrons was given in Sect. 2.3. We consider also some most important particular cases. Q~P) means Q~ or Q~. To simplify the notation, we denote by y the whole set of quantum numbers defining the term, specifying if necessary the spin S P and orbital angular momentum L p of the atomic core, the orbital momentum of an electron I, the total spin S, and the total orbital momentum of an atom L. The unnecessary quantum numbers will be omitted in formulas. The multipole order " in general can vary between "min
= 1/0 -
Id,
"max
= 10 + II
,
and Q~ is not zero only if " = "min, "min + 2, ... ,10 + II ,
For transitions between LS.! levels Q-factor can be written as follows, compare (2.3.3-5) 2/0 + 1
Q~p)(LoSoJo, LI SIJd = 2Jo + 1 FvB~lCv(J)C(P)(q), C'(q)
= 2b(q),
C/(q)
= ~[qf ,
Bq1u(J) = BqlC(SL)MqlCv(SLJ)
(6.2.4)
(6.2.5) (6.2.6)
The factor M according to (2.2.23) is equal to
(6.2.7)
BqlC(SL) == BqiSoLo, SILd does not depend on J, but depends on the type of transition. It is discussed in the next subsection.
226
6. Tables and Formulas for the Estimation of Effective Cross Sections
The sum over fine-structure components J) is independent of J o:
Q£p)(LoSoJo. L)S)
= Q£p)(LoSo• L)S) (6.2.8)
= ~ " B2 (SL) C(p) (q) [LoSoF Lq' qK • QK averaged over Jo of the initial levels is Q£p)(LoSo. L)S)JI)
[J ]2
= [L)~)F Q£p)(LoSo• L)SI) •
(6.2.9)
i.e .• it is proportional to the upper level statistical weight.
6.2.3 LS-Coupling; Q" for transitions between Terms LS Q-factors for transition LoSo-LIS) are defined by (6.2.8). On substitution of C(p) we obtain I 2[/0]2 2 QK(LoSo• L) S) = [LoSoF BOK (SoLo. S)L) •
(6.2.10)
2[/of " 2 2 QK(LoSo. L) SI) = [LoSoF Lq' BqK (SoLo. SI LI) [q] . /I
a) Transitions not involving the shells of equivalent electrons ao = [LpSp]loLoSo. BqK(SL)
a) = [LpSp]I)L)SI.
(6.2.11)
= MOqq(SpsS)MoKK(LpIL)[SpLp] .
Therefore Q~(LoSo. L)S)
= QK(L o• L I ) • Ao. Q~(LoSo. LISI ) = QK(L o• L I ) • A2 •
Ao = !5(So. SI) • A2
= (2S1 + l)j2(2Sp + 1)
(6.2.12)
where
22
QK(Lo. L I) = [LpSp] MOKK(LpIL) = [loLo]
2{LoLl }2 II 10Lp K
(6.2.13 )
The sum over L) and average over Lo are independent on Lo:
QK(Lo. LplI)
= QK(Lplo. LplI) =
(6.2.14)
1•
QK(Lplo. LI) = [Ld 2j[Lpld 2 .
(6.2.15)
Similar sums take place for spin factors 1
2[S ]2 p
2
l: [So] Ao = ~
l:Ao = l:A2 = 1. ~
~
1
--2
2[Sp]
l: [So] 2A2 = So
A2 . (6.2.16)
6.2 Formulas Defining the Angular Factors
227
b) Transitions from the shell of equivalent electrons ao = I[J'LoSo, BqK(SL)
=
al
1[J'-I[LpSp]IILISI ,
= v'mG£o~o . MOqq(SpsS)MoKK(LplL)[SpLp] , p p
(6.2.17)
where G£Ip ~Ip is the fractional parentage coefficient (Sect. 6.2.5). Q-factors are defined by (6.2.12) with (6.2.18) We see that QK(Lo, LI) depends in fact on So through G. The sums over LI and LpSp are QK(aO,
l~-I [LpSp]ld = m (G£~~~)2
QK(l~Lo, I~-Ild
= QK(l~,
I~-Ill)
,.
(6.2.19)
= m.
(6.2.20)
c) Transitions between shells of equivalent electrons ao = 1~lrLoSo,
=
al
1~-llr+1 [LpSp]LISI
N
= 410 +2
We assume here for simplicity that l~ is the closed shell. Here, LpSp are momenta of the shell Ir+l. For such transition one can use (6.2.18) for the transition I~-m - /f-m-I/ o, M = 2(2/1 + 1). (6.2.21 ) and corresponding substitutions into (6.2.19,20). We note also that for any value of n ::; 4/0 + 2 r-llm+l) = n(M - m) QK ( Inlm 0 I' 0 1M·
(6.2.22)
We used here for the total statistical weight the expression g(lm)
=
(41 + 2)! m!(M -m)!
(6.2.23)
d) Transitions inside the shell of equivalent electrons ao = rSoLo, BqK(SL)
al
=
ImSIL I ,
= (lmSoLolwqKll/mSILd
= L: v'mG£os£ . Moqq(SpsS)MoKK(LplL)[SpLp]. SpLp
p p
(6.2.24)
228
6. Tables and Formulas for the Estimation of Effective Cross Sections
Table 6.13. Reduced matrix elements (p3LoSollU 2l1 p3LISJ)
(p2LoSolIU2l1p2 LISJ) 3p
IS IS
0 0
3p ID
ID 2p 2D
0
- 1
2/-.13
4S
2/-.13
0
..jff3
0
4S
2p
2D
0 0 0
0 0
--.13
-.13
0 0
Thus we obtain
Q"'( ao, a\ )
=
2[1]2 (l mSoLo II U "II ImS\Ld 2 [SoLoF
Q~ (ao, a\) = ~Q~ (ao, ad + [:0[~~~2(lmSoLollV\"lllmS\Ld
(6.2.25)
where
(l mSoLoIIU"1I1mS\Ld =
G£o~o G£I~I
E
p p
p P
[Lp]
fllP7P~}, OL\K
LpSp LoSo (ImSoLollvq"lllmS\L\) = "L.J GLpSp .
LpSp
x
GLlsl LpSp
[L P SP ]
{:P:P~} . f7P7P~}. SoS\q
10L\K
(6.2.26)
The reduced matrix elements (aoIIU"llad and (aollV q"lIad were defined and partly tabulated in [6.1]. More detailed tables are given in [6.3]. For K = 0
(lmSoLoIlUOlllmS\Ld = b(Lo, Ldm[Lo]/[l]
(6.2.27)
Therefore, transitions with a change of L are possible only with K ~ 2 or due to exchange. At AL = 0, AS # 0 also exchange is necessary; at AL = AS = 0 there is no transition. In the Table 6.13 reduced elements for K = 2 are given for m = 2,3; for m > M/2 one can use relation: (6.2.28)
6.2.4 j/ Coupling
Below we shall give formulas for two cases: (i) both initial and final levels are described by jl coupling; (ii) the initial term LoSo is described by LS coupling, and the final term K is described by j I coupling.
6.2 Formulas Defining the Angular Factors
229
(i) For transitions between the fine structure components
Jo = Ko ±
!,
J, = K, ±
!,
we have
Q" (KoJo, K, J, ) = (2Ko + 1)(2J,
1}2 Q" (Ko, K,) .
KoJo K, ~
+ 1) { J,
(6.2.29)
Summation over J, gives
Q,,(KoJo, K,)
= Q" (Ko, K,) .
(6.2.30)
Equation (6.2.29), being averaged over Jo, yields
2J, + 1 Q" (Ko, K,J,) = 2(2K, + 1) Q" (Ko, K,) .
(6.2.31 )
The j I-coupling scheme cannot be used for a shell with equivalent electrons. Therefore only the case of transitions which do not involve groups of equivalent electrons should be considered. For transitions between the terms Yo = [LpSpj]/oKo, y, = [LpSpj]/,K, as a whole the factor Q" is
Q,,(yo, y,) = ( 2/ 0 + 1)(2K,
/o
+ 1) { K,
KOj}2 I,
(6.2.32)
K
Summing (6.2.32) over K, gives
Q" ([LpSpj] 10Ko, [LpSpj] Id
= Qd/o,
Id
= 1,
(6.2.33)
and averaging over Ko provides
Q (I "
IK )_ 0,
,
,
-
2K, + 1 (2j+ 1)(2/, + 1)
(6.2.34)
(ii) For transitions from the level LoSoJo described by LS coupling to the level [LpSpj]l,K,J, described by the jl-coupling scheme, we have
(6.2.35)
= (2/0
+ 1)(2J, + 1)(2So + 1)(2Lo + 1)(2j + 1)(2K, + 1)
LOSPK [ 10 Joj
K,]2 !
Lp I, SoJ, The definition of the 12j symbol used here is given by (6.3.23). Averaging over J o and summing after that over J, gives for transition between the terms,
Q,,(Yoyd = ( 2/ 0 + 1) (2j
+ 1)(2K, + 1) I)2r + 1) {Lp I, r 2Sp + 1 r K Lo/o
}2 {LpK,Sp} I, ~}2
(6.2.36)
230
6. Tables and Formulas for the Estimation of Effective Cross Sections
Summing (6.2.36) over K I , we obtain Q (
KYO,
[L S .] 1 ) p p}
I
=
(2Lp
2j + 1 + 1)(2Sp + I)
.
(6.2.37)
By summing further over j, one has (6.2.38) Averaging (6.2.36) over Lo, we have _ 2KI + 1 Q ([L S ] I S, K P pO 0,Yd-(2L p +l)(2S p +I)(2/ 1 +1)
(6.2.39)
For transitions from the shell of equivalent electrons I~ -1;-1/ 1, the formulas )2. (6.2.35-38) should be multiplied by m(G£o~o p p
6.3 3nj Symbols and Fractional Parentage Coefficients Formulas for the angular factors Q~ and Q" contain 6j symbols, 9j symbols, 12j symbols, and the fractional parentage coefficients G£sp sp . The detailed description of their invariance properties, and formulas, sum rules, and numerical values can be found in [6.2-7]. Here we give only those which are necessary for this book. I) The 6j symbol {:: :~::} obeys the following symmetry relations: it remains invariant under any permutation of its columns and also on transposing the lower and upper arguments in each of any two columns. For example,
The 6j symbol is nonzero if the following triangular conditions are fulfilled: LI(al a2 a3),
LI(al b2 b3),
LI(b l a2 b3),
LI(b l b2a3) .
The triangular condition LI (a be) means that the sum of any two arguments is greater than or equal to the third argument and the modulus of the difference of any two arguments is less than or equal to the third one. The 9j symbol remains invariant under any permutation of its rows or columns and also under transposition (change of rows to columns). Triangular conditions are fulfilled for every row and column. Here we give summation formulas for j-symbols, including some formulas that are missing in most books. {abc} means ''OJ-symbol'': the set of triangle rules LI(abc) and condition that a + b + c is
6.3 3nj Symbols and Fractional Parentage Coefficients
231
integer. Sums of one j-symbol.
L [x]z {hjlx} = [jzjIl Z
(6.3.1a)
x
(6.3.1b) x
~ [x]z {j:j~~3} = (-I)Zh{hhh}
{f: {:~3} = L [x]z {f: {~{~ } = [lIl-zJ(jz, h 13x L t [x]z {f: {~{:} = hx
~ (-It [xf
(6.3.2a) (6.3.2b)
(-1 )-h -II [h IIlJ(h, 0)
(6.3.3a)
II)
x
(-1 iI2+h-/1 [jIl-zJ(jI, I z )
(-1
x
(6.3.3b)
13
Sums of two j-symbols.
(6.3.4a) (6.3.4b) (6.3.4c)
(6.3.5)
(6.3.6a)
L (-lt2 [XIXZ]Z XlX2
f{:{~{~}J{:~~{t} = (-lih+/3-/~ {{~{~{~} ~lxzk3 ~lxzk3
(6.3.6b)
j{ l{k3
Sums of three j-symbols.
{~l/zI3} {kl~zk3} = {{:{~{~}
L(-I)2x[xf {hhh} x 13 k3x Jzxkz
xJI/I
klkz k3
(6.3.7a)
232
6. Tables and Formulas for the Estimation of Effective Cross Sections
(6.3.8)
Sums of four j-symbol.
(6.3.9a)
(6.3.9b)
(6.3.10)
For what follows it is convenient to adopt the designations: {a
bk} = {a.'. b.k.} './' , a = (a2alao) i p,q, ,
pq /
(6.3.11) Then
L [k2kd 2f(abk)f(pqk) {a bk} P qI
kJk2
=
t:
[/of f(aql) f(pbl) {;
2
:i}
{a qbk}/ P
I
(6.3.12) 0
6.3 3nj Symbols and Fractional Parentage Coefficients
233
using the definition of the M by (2.2.23) this equation can be written as " Mk(a,b)Mk(P,q) {abk} k7k2 pq/ z {abk} pql ; [kzkd z/[ko] z q I} =EMq(l,a)Mp(b,l) {a qbkI} =EMI(a,q)MI(p,b) {abk POlo P 10
(6.3.13) . 0
We have also
E [kzk\ko]z f(abk)f(pqk) {a bk} {a bk} {a bk} {pqk} P q I z p q I \ U V s o u vt 0
to k\ k2
= E [lof f(aql) f(pbl) 10
P}
t s ub a qI V
{
(6.3.14)
, 0
. {a' b'k'} {a' b'k'} {a bk} {a bk} fJ(k' k)fJ(O' 2) p' q' I' z p' q' I' \ P q I \ P q I 0 ' ,
(6.3.16)
= E[lz]z f(a'q'I')f(p'b'I')f(aql)f(pbl)fJ(O', 2) 12
fJ(O', 2)
= fJ(a~b~p~q~/~,
azbzpzqzlz).
Sums including 3jm-symbols.
~(_I)}-m (~~m~') E(-I)}-m[j]Z }m
=
t
= [j]fJ(j'm', 00),
(6.3.17)
(h h (h ,h ) ) j) m\ mzm -m\ -mz-m
(-I)h-m\fJ(m\mz, m~mi), (_I)h- m\-h- m2 [j]z
m\m2
= (-I)}-mfJ(jm,j'm'),
(6.3.18)
(h hj) (h h j ,) m\ mzm
-m\ -m2- m
(6.3.19)
234
6. Tables and Formulas for the Estimation of Effective Cross Sections
(6.3.20)
In particular, if ml = m2 = m; =
E(-IY[X]2 x
= (-1 i
m~ =
0,
{x1 hh} (x0 jlh) (x0 011/2) 11/2 0 0 0
(I h h) (I 000
II h ) 000 .
(6.3.21 )
A summary of formulas for 6j symbols in which one of the arguments does not exceed unity is given in Table 6.14. II) 9j symbols and 12j symbols are defined in terms of the 6j symbols in the following way:
~;} = E( -lfX(2x + I) {afrx bC}{dbxq ef}{pxqr}, {~P qr ad x
Table 6.14. Formulas for 6} symbols s=a+b+c
{ o~
b c} = (-I),(2b+ 1)(2c+ IW I/ 2 c b
b c} { a 1/2 c - 1/2 b + 1/2
s [ (a + c - b )(a + b - c + I)] 1)2 (2b + 1)(2b + 2)2c(2c + I)
= (-I)
b c} s[(a+b+c+ 1)(b+c-a)]-1/2 { a 1/2c-I/2b-I/2 =(-1) 2b(2b+I)2c(2c+l) abc 2[a(a+I)-b(b+I)-c(c+I)] 1 c b =(-I'[2b(2b+I)(2b+2)2c(2c+I)(2c+2)p/2 {a
b
c}
1 c-I b-I
(I)S[ =
-
s(s+I)(s-2a-I)(s-2a) ]1/2 (2b-I)2b(2b+I)(2c-I)2c(2c+l)
C}_(_I,[ 2b(2b 2(s+ 1)(s-2a)(s-2b)(s-2c+ I) ]1/2 + 1)(2b + 2 )(2c - I) 2c (2c + I)
{a b 1c- 1b -
c }_(_I)S[(S-2b)(S-2b-I)(S-2C+I)(S-2C+2)]1/2 {a b 1 c- 1b+ 1 (2b + 1)(2b + 2)(2b + 3)(2c - 1)2c(2c + I)
(6.3.22)
6.3 3nj Symbols and Fractional Parentage Coefficients
[
235
a)a 2 a 3 a 4 ] b) b2 b3 b4
c) C2 C3 C4
= (-1 )bl-b2-b3+b4 L:(2x + 1) {C) C2
x} {C3 )b2x} {C) bx} {C3 bx} .
a3 a )b)
x
C4
a3 a
C2
C4
a4 a 2 3
a4a2 4
(6.3.23 ) III) Our notation for the fractional parentage coefficients, G£sp s p agrees with that of [6.2]. The Racah notation is related to this by
The values of fractional parentage coefficients for electron configurations p'" with m = 3, 4,5 are given by Tables 6.15-17. For configurations s2, p2, p6, the fractional parentage coefficients are equal to unity.
Table 6.15. Fractional parentage coefficients (p2[L pSp]pLS} p 3LS) p3 2p 4S
l
IS
Ji
0
ID
0
3 I
3p
I
-Vi
-{{s
0
Table 6.16. Fractional parentage coefficients (p3[L pSp]pLS} p4LS) p4 3p IS p3 4S
0
2p 2D
0
2D
I
-J3
Vi I -Vi
ID
0
I 2
2
H,
~
236
6. Tables and Formulas for the Estimation of Effective Cross Sections
p4 2p
p5 IS
3p ID
fFs fs If
7 Broadening of Spectral Lines
Various phenomena of spectral line broadening connected with the most interesting applicati0!ls of atomic spectroscopy to plasma diagnostics, astrophysics, laser physics, and other areas are considered in this chapter. The presentation of the general theory of impact broadening is based on the density-matrix and quantum kinetic equation methods. These methods permit not only the line shape to be described in the case of spontaneous emission or linear absorption, but also allow nonlinear effects arising in laser spectroscopy to be considered. There are many books and review articles discussing the progress in theoretical and experimental work on the problem of spectral lines broadening [7.1-16]. For an extensive bibliography on line shapes see [7.17-19]. For a brief review of recent developments in the theory with stress to applications to nonlinear laser spectroscopy see [7.20].
7.1
Model of a Classical Oscillator
7.1.1
Formulation of the Problem
The theory of spectral line broadening caused by the interaction of an atom with surrounding particles is closely connected with the general theory of atomic collisions. Moreover in the region of not very high pressure, when the impact approximation is valid, the calculation of the profile of a spectral line includes calculation of the scattering amplitudes or scattering phases. Nevertheless it is useful to begin the study of pressure effects by considering a model simplified to the maximum extent. We shall make the following assumptions: i) the relative motion of the atom and the perturbing particle is quasi-classical, which enables one to use the concept of the trajectory of the perturbing particle; ii) this trajectory is rectilinear; iii) interactions with the nearest perturbing particle (binary interactions) play the principal role in the broadening, therefore multiparticle interactions can be neglected; iv) the perturbation is adiabatic, i.e., does not induce transitions between different states of the atom. Within these assumptions, the picture of broadening is outlined as follows. The perturbing particle produces an external field V(R) = V
[J p2 + v2(t -
to)2] ,
I. I. Sobel'man et al., Excitation of Atoms and Broadening of Spectral Lines © Springer-Verlag Berlin Heidelberg 1995
(7.1.1)
7. Broadening of Spectral Lines
238
where R is the distance between the atom and perturbing particle at a given time t, p is the impact parameter, to is the time of nearest approach, and v is the relative velocity. As a result the energy levels of the atom and, consequently, the frequency of oscillations of the atomic oscillator vary in time. Therefore the oscillation of the atomic oscillator can be described in the form t
J
= exp [iwot + i
f(t)
(7.1.2)
K(t') dt'] ,
-00
where Wo is the unperturbed frequency and K(t) is the frequency shift due to the interaction. Perturbation of the monochromaticity of the oscillations leads to broadening of the corresponding spectral line. The line shape is given by the expansion of the function f(t) in a Fourier integral, 1 I(w) = lim 1 ~ T-oo v 2nT
T/2
J
f(t)exp(-iwt)dt
12
-T/2
(7.1.3)
= lim - 12 1 T/2 J exp [-i(w nT
T-oo
-T/2
wo)t + i11(t)] dt
12
,
t
11(t)
J K(t') dt'
=
(7.1.4)
,
-00
where 11(t) is the phase of the oscillation caused by interaction. If the frequency w is measured from the unperturbed frequency Wo, then the exponent exp (iwot) must be omitted. In this case, I(w)
1 1 T/2 exp [-iwt 2nT -T/2
J
= lim T-oo
+ i11(t)] dt 12
(7.1.5)
In the theory of spectral line broadening, conditions are usually considered when gas pressure and temperature, state of ionization, and so on, do not vary with time. This means that the functions ,,(t) and f(t) = exp [i11(t)] are stationary random processes, and (7.1.3) can be rewritten in the following way:
*
I(w)
=
4>(r)
= lim
(7.1.6)
Re{7 4>(r) exp (-iwr) dr} ,
T-oo
1 -T
T/2
J
f*(t)f(t
+ r)dt =
f*(t)f(t
+ r) ,
(7.1.7)
-T/2
where 4>( r) is the correlation function. Time averaging can be replaced by averaging over the statistical assembly of quantities defining the function f(t). We shall denote such averaging by angle brackets, 4>(r)
=
(f*(O)f(r») .
(7.1.8)
7.1 Model of a Classical Oscillator
= exp [i1](t)], we have <1>(,) = exp {i[1](t + ,) -1](t)]} =
239
For f(t)
7.1.2
(exp [i1](')]) .
(7.1.9)
Impact Broadening
We shall consider in this section an approximation which is called the impact approximation. This approximation is based on the assumption that the decisive factor in the broadening of a line is the disruption of the coherence of the oscillations of an atomic oscillator during collisions. In other words if the duration of collision is small as compared with the mean time between collisions, then one can neglect radiation during collisions and consider the collisions to be instantaneous. Therefore the collisions are manifested only in phase shifts 1]. Using this assumption of instantaneous collision, it is possible to calculate the correlation function <1>(,) in the following way [7.21]. In accordance with (7.1.9) the difference .,1 <1> = <1>(, + .,1,) - <1>(,) can be written in the form .,1<1>
=
(exp [i1](, + .,1,)]) - (exp [i1](')])
= (exp [i1](')] exp (iL11]») - (exp [i1](')]) ,
where .,11] is the phase shift produced by collisions during time interval .dr. Since collisions are instantaneous, the phase shift .,11] does not depend on 1](,). Therefore 1](,) and .,11] are statistically independent, and consequently .,1 <1>
= (exp [i1](')])[ (exp (iL11]») -
1]
= -<1>(,)(1 -
exp (iL11]») .
(7.1.10)
We shall denote the number of collisions per second with parameters p and v as P(p, v)dpdv. The number of collisions during time interval .,1, is equal P(p,v)dpdvL1,. Therefore (l-exp(iLl1]»)
= '!9L1"
'!9
=
f[1-exp (i1])] P(p, v)dpdv ,
(7.1.11)
where 1] is the phase shift produced by collision with parameters p, v. If the density of perturbing particles is N and their distribution over velocities v is given by the distribution function ~(v), then 00
00
o
0
() = N J v~(v)dv2n J pdp[1
- exp(i1])] .
(7.1.12)
Denoting 00
(i'
= 2n J(1 o
- cos 1]) pdp,
(7.1.13)
00
(i"
= 2n
J sin 1] pdp o
,
(7.1.14)
240
7. Broadening of Spectral Lines
we have () = N(v (a' - ia")) .
(7.1.15)
From (7.1.10,11) it follows that
= -()tfJ
dtfJ dr:
(7.1.16)
'
tfJ = exp (-()r:) .
(7.1.17)
By substituting (7.1.17) into (7.1.6), we obtain
y I(w)
= 2n . (w _
y = 2N (va');
1 LI)2 + (y/2)2 '
LI = N (va") .
(7.1.18) (7.1.19)
The spectral distribution given by (7.1.18) is usually called the Lorentzian distribution. The width of the distribution (the distance between symmetrical points WI and W2, for which I(wJ) = I(w2) = Imax/2) is y. The shift of the line peak from Wo is LI. The quantities a' and a" are called the width and shift effective cross sections. Let us assume that the perturbing particle at a distance R produces the frequency shift K = CnR-n. Then (7.1.20) (7.1.21)
r(~) rtn =
r
Vi
G) .
(7.1.22)
For n = 2, 3, 4, 5, 6, we have rtn = n, 2, n/2, 4/3, 3n/8. Substituting (7.1.21) in (7.1.13,14), it is not difficult to obtain the following formulas for y and L1 which we shall use below in estimations of the width and shift:
LI _
v'3
-TY'
n
=6
LI
~
Y ~ 8.16 C;/5 (V 3/5)N ,
0.36 y .
(7.1.23)
7.1 Model of a Classical Oscillator
241
It is not difficult to show that the main contribution in (1' is given by the strong collisions for which '1 ;::: 1 and P < Po, where Po is defined by condition
'1(Po)
=
1:
cx.nCn) I/(n-l) Po= ( - .
(7.1.24)
v
The impact parameter Po is usually called the Weisskopf radius. Therefore to an order to magnitude, (1'
~ np~
(7.1.25)
The shift cross section (1", see (7.1.14), is determined by more distant collisions P ;::: Po. In the case of n = 2, the phase '1(p) ex: P-I. Thus (1' diverges as In Pm and (1" diverges as Pm, where Pm is the upper limit of integration in (7.1.l3) and (7.1.14). The divergence of the integrals (7.1.13) and (7.1.14) means that the approximation of binary collision is not valid. It is evident that in this case broadening is determined by distant (weak) collisions with P > Po. 7.1.3 Quasi-Static Broadening If the external field varies sufficiently slowly, i.e., if it is quasi-static, it is pos-
sible to assume that I( w )dw is simply proportional to the statistical weight of the configuration of perturbing particles for which the frequency of the atomic oscillator is included in the interval w, w + dw. In the binary approximation the frequency shift is produced by the nearest particle. Consequently, to calculate I( w), it is necessary to find the probability W(R)dR of the nearest particle being within the range of distance (R,R + dR) from the atom. For R much larger than the atomic dimensions the interaction potential could be neglected and this probability is W(R)dR
= 4nR2N exp ( -
~n NR 3) dR = exp [- (:0
y] (:J 3, d
(7.1.26) where Ro = (3/4nN)1/3. Substituting R = (Cn/K)lln = [Cn/(w - wo)]lln in (7.1.26), we obtain the probability distribution for a frequency shift of an atomic oscillator. In accordance with the basic assumption of the quasi-static approximation, the shape of the spectral line is also determined by this distribution. If the notation .dw = CnR{jn is introduced it follows from (7.1.26) that 4n I(w)dw=-NC~/n(w_wo)-(3+n)/nexp n
/ [ - ( -.dw - - ) 3 n] dw.
(7.1.27)
w-~
This distribution is valid only for sufficiently large values of w - Wo for which
242
7. Broadening of Spectral Lines
R = C~/n(w - wo)-I/n ~Ro For R :<: Ro, the binary approx:imation is not valid. Thus (7.1.27) describes only the outer part of a line. The condition R ~Ro means that .1w~w - wo. Thus the exponential factor can be omitted in (7.1.27), after which we obtain I(w)dw = 4n Nc~/n(w _ wo)-(3+n)/n dw .
(7.1.28)
n
7.1.4
Relationship and Limits of Applicability of the Impact and Quasi-Static Approximations
Let us return to the general relations (7.1.3,4). We shall first of all consider (7.1.3) for high values of .1w = w - wo. If .1w is large, the integrand in (7.1.3) oscillates strongly everywhere, except in the vicinity of the points tk for which
(
~;}k = K(td = .1w .
Thus the principal contribution to (7.1.3) give small regions .1 't'k around these points and instead of (7.1.3) one can write
I(w)= lim T---too
_I_II: J 2nT
eXP{i['1(t)+(WO-W)(t-tk)+(WO-W)tkUdtI2
k Ark
(7.1.29) We shall expand the function '1(t) in a series near tk in powers of t - tk. Since (dy//dt)tk = .1w, the linear terms in the exponent in (7.1.29) cancel, and the series begins with the term 2
2:1 (ddt2y/)Ik (t -
2
tk) .
Only the region .1't'k, where this term is less than unity, is significant in the integration (beyond this region strong oscillations begin). Hence (7.1.30) If within the limits of this region the next term of the expansion
3
611 (ddt 3y/) (t -
tk)
31 ~ 1 , (ddt33'1)It -_ (ddt22K) It
'
(7.1.31)
which must fulfill the following inequality: (7.1.32)
7.1 Model of a Classical Oscillator
243
the series can be broken of at a term proportional to (t - tk )2, and in each term of the sum (7.1.29), the limits of integration can be extended from -00 to 00. In this easel /(w)= lim - 12 L exP {i[I1(tk)+(Wo -W)tk]) T--->oo nT k I
(7.1.33)
= lim.!.. L T--->oo
T
k
(dK)-1 . dt Ik
It is easy to see that Lk(dK/dt);/dw is the time during which K(t) is included in the interval w - Wo, w - Wo + dw. Since d!k and dw in Fig. 7.1 are connected by the relation (dK/dt)lkd!k = dw, (7.1.33) gives the quasi-static intensity distribution W(w - wo)dw. We shall replace the summation in (7.1.33) by integration. The number of particles incident on the annular element 2np dp in the time T is 2npdp NvT, where N is the density of perturbing particles. Taking into account that each collision with p :::: PAw = (Cn/AW)I/n, Kmax = Cnp-n~Aw gives two points tk and tk+l (Fig. 7.1), we obtain
/(w)dw
= dw
P-1w
{4np
(dK)-1 dt Nvdp
4n
dw
= -;;Nc~/n Aw 1+ 3/n
'
(7.1.34)
i.e., the quasi-statical distribution in the wing of the line.
/(
w~~--~+-~~--------------
Fig. 7.1 Instantaneous frequency shift K(t)
1 It is assumed that the phases ak will be discussed below.
=
['1(tk) + (w - Wo )ttJ are independent. This assumption
244
7. Broadening of Spectral Lines
If a small neighbourhood around the instant of closest approach is not considered, then
dJ( C"v dt ~ p,,+l'
d 2 J( c"v2 dt2 ~ pn+2 '
(7.1.35)
and relation (7.1.32) takes the form
C" vp"-
(7.1.36)
--I~I.
Only collisions with p ~ P,1QJ = (C"/Aw)l/,, give points (7.1.36) can be rewritten in another form
tk
and
tk+1.
Therefore
v"/(,,-l)
Aw~ C~/("-l) = D .
(7.1.37)
According to condition (7.1.37) the quasi-static distribution is valid for large Aw, i.e., in the wing of a line. We shall now consider (7.1.3) in the limiting case of small Aw. If Aw is so small that l/Aw is much greater than the duration of the collision -
I
Aw
~
p v
- ,
(7.1.38)
the change of phase in the collision can be considered to be instantaneous. Hence it follows that the impact approximation can be used. The main contribution in the impact broadening of a line is given by collisions with p '" Po = (a" C,,/V)l/(,,-l). Substituting Po in (7.1.38), we obtain a relation opposite to (7.1.37): v"/(,,-l)
Aw~ C~/("-l) = D . Thus in the center of a line, Aw~D, the impact (Lorentzian) distribution of intensity is valid. For high values of Aw, Aw ~ D, the impact distribution is replaced by the quasi-static one. The quasi-static wing can appear both on the long-wave and on the short-wave side depending on the direction of shift of the terms. If D considerably exceeds the impact width y, then the greater part of the integral intensity of a line is concentrated in the impact region. Taking into account that
y ~ 21tpt,Nv = 21CNv(aC,,/vi/(,,-I) , we obtain
21tpt,Nv~D = .!:. ; Po
whence (7.1.39) where the dimensionless parameter h determines the number of perturbers in the sphere of the Weisskopf radius. Thus, for low pressures and high velocities, so
7.1 Model of a Classical Oscillator
245
long as the inequality (7.1.39) is fulfilled, the impact mechanism of broadening plays a decisive role. A relatively negligible part of the total intensity is concentrated in the quasi-static wing. At high pressures and low velocities, when h
= p~N
'" I ,
(7.1.40)
the impact approximation is inapplicable even to the inner part of a line. Let us note that if condition (7.1.39) is not fulfilled then the binary approximation is violated. In fact relation (7.1.40) means that the effective radius Po is approximately equal to the mean distance between perturbers. Although when p~ ~ I the quasi-static distribution is applicable practically to the whole profile of a line, the expressions (7.1.27,28) obtained above in the approximation of binary interactions are valid only in the wing of a line. The assumption of the independence of the phases (1.k was made above in the derivation of the formula (7.1.33). Since only strong collisions for which '1 ~ C,.lp" • plv'$> I are responsible for the quasi-static wing, the difference (1.k+l(1.k'$> I. In a nonpublished work [7.4] Anderson and Talman investigated in detail the limiting expressions for /(00) valid for the central part of the line and for the wings, and obtained also an interpolation expression for the intermediate part. The same problem is discussed also in [7.22,23]. 7.1.5
Doppler Effect
The frequency observation is amount 000 vie. defined by the
of an oscillator whose velocity component in the direction of v is displaced in accordance with the Doppler principle by an Let the distribution of the radiating atoms with respect to v be function W(v). Then 00 = 000 + ooovle, v = e(oo - (00)/000, and
00-(00) e /(oo)dw = W ( e - - - doo . 000
.
(7.1.41)
Wo
With a Maxwellian distribution (7.1.42)
where Vo = J2k Tim, we obtain I
/(00 )
[ ( 00A-ooD000 ) 2]
doo = yin exp -
doo AWn'
AooD
= 000 -Voe
•
(7.1.43)
The intensity distribution (7.1.43) is symmetrical. The magnitude of the broadening is defined by the parameter AWn. The width of the line, which we shall denote by ~, and the peak density /(wo) are expressed in terms of the parameter
246
7. Broadening of Spectral Lines
Amo:
() = 2Jln 2 Amo l(wo) = 1/v'n Amo
(7.1.44) (7.1.45)
Here () is defined as a difference between the symmetrical frequencies WI and W2 for which lewd = l(w2) = l(wo)/2. The parameter Amo is usually called the Doppler width of a line. When deriving (7.1.41,43), it is assumed that there is only one frequency wo(1 + vic) in the spectrum of the oscillator with velocity v. This assumption is valid if v does not vary in time or remains a constant quantity during a sufficiently long time. If velocity is constant only during time interval 't, then this interval contributes to the intensity of radiation in a spectral interval with width l/'t around the frequency Wo + Wovle. Formula (7.1.41) is valid if wovle~ 1/'t. Substituting for 't the free path time 'to = Llv, where L is the mean free path, we have (7.1.46) In the general case, the Doppler broadening is determined by Fourier transform of the function f(t)
WO] = exp [i-x(t) e
,
x(t)
=
Jt
(7.1.47)
v(t')dt'
-00
Substituting (7.1.47) in (7.1.6,7), we have l(w)
= ~ Re
{?
4>('t) exp (-iw't) d't}, 4>('t)
= (exp [i
:0
x('t)]). (7.1.48)
The function ( 't) in the form f
4>('t) = (exp[ik· r('t)]), r('t) = Jv(t)dt ,
(7.1.49)
o and introduce the distribution function f(r, v,t) for the oscillator coordinate r and velocity v. This distribution function satisfies the Boltzmann equation
of -+v·Vf=
ot
(Of) -
ot
coil.
- Gf ( Of) ot coil. -
,
(7.1.50)
and the initial condition f(r,v,O) = W(v) {)(r) .
(7.1.51)
Here (oflot)coll. is the collisional integral or collisional term, G is the linear operator of collisions, and W(v) is the distribution function for v. The correlation
7.1 Model of a Classical Oscillator
247
function
= ~Re{fdvJ f(r,v,r)exp[-i(wr-k.
J(w)
= - Re{f Fw(v,k)dv}
(7.1.52)
(7.1.53 ) r)]drdr}. n Here the frequency difference w - Wo is replaced by w. According to (7.1.53), J(w) is expressed in terms of the Fourier component F(Av,k) of the distribution function: I
n
Fw(v,k)
=J
(7.1.54)
,
fer, v, r) exp [-i(wr - k • r)] drdr.
(7.1.55)
Carrying out the Fourier transform of (7.1.50) and taking into consideration the initial condition (7.1.51), we obtain the following equation for F w( v, k): -W(v) + i(w - k • v)Fa,(v,k) = (Gf)wk .
(7.1.56)
For simplificity, the functions Fw and (Gf)wk will be written below without indices w. In the absence of collisions (of/ot)coll. = O,(Gf)k = 0, and F(v,k)
W(v)
= l.(W - k
·V
)
For the Maxwellian W(v) this gives the usual Doppler distribution (7.1.43). In fact, W ( v )d v = W ( v )w( v.ddv d v ~ , where v is the velocity component in the direction of vector k, v~ is perpendicular to k. Integrating in (7.1.54) over v~ gives unity. When integrating over v, it is necessary to replace w - kv by w - kv - ie, considering e --> O. We find J(w)
.
e
W(v)dv
= hmJ -n ( w- kv)2 +e2 =
J J(w - kv) W(v)dv
(7.1.57) We shall consider now the influence of collisions assuming the model of Brownian motion [7.25J. This model can be used in the case of so-called weak collisions. In the framework of the model of Brownian motion, the collisional term in (7.1.50) has the form
a
( Of) t colI.
. = v dlV.(vf) + 2v~ v L1./ .
(7.1.58)
The effective frequency of collision v is assumed not to depend on velocity and v~ = 2kT/m. Solving (7.1.50) with the collisional term (7.1.58) and taking into
248
7. Broadening of Spectral Lines
account the initial condition (7.1.51), it is possible to obtain tP(t) = exp [/(w) =
~1 (vt - 1 + e-
vt )]
,
..1eoo = kvo ,
(7.1.59)
.! Re {A Wo2 2v 2.IVW tP (1,1 + ..12WV1' - i~;V ..121)} v
,
(7.1.60)
1[
where tP( a, 1; z) is a confluent hypergeometric function az a( a + 1) z2 a( a + 1)( a + 2) z3 tP(a,1;z) = 1 + 1I! + 1(1+ 1)2! + 1(1+ 1)(1+ 2 )3! + ....
For v = 0, (7.1.60) gives the usual Doppler distribution. When v v ~ AWn, for the central part of a profile W = 0 and for the far wing we have, respectively, 1
/(0) = Ji..1eoo
(
2
v)
1 + 3Ji ..1wo
'
v
1 ..1w~ /(w) ~ Ji..1eoo 2Jiw4 .
(7.1.61 )
#
0, but
W ~ ..1wo,
(7.1.62)
Thus due to collisions with v ~ ..1wo the intensity in the central part of a profile is increased and the wing with intensity distribution ()( w- 4 appears. In the limiting case of high densities when v ~ ..1eoo, 1 /(w) ~ 1[
2 W
Yd
•.2
+ Yd
Vd
1 ..1w~ = ---. 2 v
(7.1.63)
The central part of a line is described by the Lorentzian distribution (7.1.64)
with width 2Yd = ..1~/v. Since v ~ vo/L, 2Yd = ..1eoo 21tL/). i.e., the width decreases ()( L with increase of density. This result was first obtained by Dicke [7.26]. For w~v, (7.1.63) coincides with the intensity distribution in the wing from (7.1.62). The qualitative picture of modification of the Doppler distribution due to collisions does not depend on the specific model of Brownian motion used above. We shall consider now the model of strong collisions assuming that after every collision the distribution of velocities does not depend on the velocity before collision and is Maxwellian. In this case, the collisional term in (7.1.50) can be written in the form
( f)f)If) t
=-vf+vW(v)jf(r,v',t)dv'.
(7.1.65)
coil.
For (Gf)k in (7.1.56), we have
(Gf)k = -vF(v,k) + vW(v)j F(v',k)dv' .
(7.1.66)
7.1 Model of a Classical Oscillator
249
Substituting (7.1.66) in (7.1.56) we obtain
F(v,k) =
vW(v) " .( k )JF(v,k)dv V+IW- ·V
W(v)
+ V+IW.( k·V)
(7.1.67)
Integrating the right-hand side and left-hand side of this equation over v we have
J F(v,k)dv
=J
W.~V~dV) (v J F(v',k)dv' + 1) ·V
V+IW
and after replacing in the right-hand side v' by v
W(V)dV) W(v)dv JF(v,k)dv ( I-vJ V+IW-'V .( k ) =J V+IW-'V .( k ) It is possible now to find F(v,k). Then using (7.1.54) we obtain
_ { I-v. kJ v+:~v2~. v) W(v)dv
1(w)-Re
J v + i(W -
}
(7.1.68)
.
k . v)
When V~LlWD, the second term in the denominator of (7.1.68) has the order of magnitude of V/LlWD. If this term is neglected, (7.1.68) gives the usual Doppler distribution. In the general case, the intensity distribution (7.1.68) is similar to that given by (7.1.60). Instead of (7.1.62), it follows from (7.1.68) for 1(0) and I ( n-2 v ) 1(0) ~ y'nLlWD 1+ y'n LlWD '
1(w)
1 vLlWb ~ --=:--- y'nLlWD 2y'nw4
(7.1.69)
In the limiting case v ~ LI mo, (7.1. 68) leads to a Lorentzian distribution in the central part of a line with width LlwMv. In the region of high frequencies W > v, the Lorentzian distribution is replaced by a wing 1(w) <X w- 4 • Thus in both cases considered above (weak and strong collisions), with an increase of the density a narrowing of the central part of the line occurs. At high densities, when L < A/2n, the narrowing of a line is proportional to L <X N- 1, and in the limiting case of L ~ A/2n, the central part of a line is described by a Lorentzian distribution with width 2nL/A times less than the usual Doppler broadening LlWD. Such a narrowing of the Doppler profile caused by collisions can be observed only in cases when there is no broadening due to interaction with perturbers. In the general case there are no grounds for separating the effect of interaction and the Doppler effect. The same collisions can produce both a phase shift and a change of velocity of the atom. This means the statistical dependence of both effects. It must be noted that Doppler broadening is usually of interest just under the condition L > Aj2n. In fact, the condition LlWD ;;:: y, where y is the impact width can be rewritten in the form 2nv/A ;;:: Nva' = Nvaa'/a = va'/La, where a is the gas-kinetic effective cross section of the atom. As a rule, a' ;;:: a and, consequently, Limo ;;:: y when L > A/2n.
250
7. Broadening of Spectral Lines
Nevertheless the statistical dependence of Doppler and impact broadening in some cases must be taken into account. This problem will be considered below in the framework of the quantum theory of broadening. A bibliography on Dicke narrowing may be found in [7.27].
7.1.6 Convolution of the Doppler and Lorentzian Distributions If L ~ A/2n, the combined treatment of impact and Doppler broadenings (statistically independent) leads to the convolution of Doppler and Lorentzian distributions. The Lorentzian intensity distribution with width y and shift L1, corresponding to the atom with velocity component v in the direction of observation, is given by
y I ------::----=2n (w - L1 - wov/c)2 + (y/2)2
(7.1.70)
/v(w) = -
To obtain the intensity distribution for an assembly of atoms, it is necessary to average (7.1.70) over the velocity distribution W(v). Thus /(w)
=l
2n
J
W(V)d~
(w - L1 - wov/c)
+ (y/2)
2 •
(7.1.71)
For a Maxwellian distribution
/(w) = l _ l _ exp [-(v/voil dv 2n y'nvo J (w - L1 - wov/c)2 + (y/2)2
(7.1.72)
When L1wo~y/2 the term wov/c can be neglected in the denominator in (7.1.72), after which the integration over v gives a Lorentzian distribution with width y. Consequently, when L1wo ~y/2 Doppler broadening can be neglected. When L1roo~y/2 a significant contribution to the integral (7.1.72) can be given by two ranges of values of v: v '" 0 and v'" c(w - L1)/wo. In the first of those ranges, the term Wov/c in the denominator can be neglected and in the second v can be replaced in the numerator by c( w - L1 )/wo. After this it is easy to obtain two approximate expressions for / ( w) valid for the center of a line w - L1 ~.oo and for the wing w - L1 ~ .00 , where .00 is determined by the relation
Dt, =
L1w~ In [2n3/2 L1~ (L1'!: Yl
.
(7.1. 73)
In the center of a line w - L1 ~ .00 , / (w) coincides with the usual Doppler distribution. In the wing of a line, /(w) ex y/2nw2. Thus for any relation between L1wo and y/2 at sufficiently high values of w, the Doppler distribution is replaced by the Lorentzian wing. We shall write (7.1.72) in the form I o Re {(W-L1) /(w) = y'n L1w W L1roo '
(7.1.74)
7.2 General Theory of Impact Broadening i 00 exp (-t 2)dt 1 00 W(x,y)=-! . = r.;!exp[-z2+i(x+iy)z]dz, 1t -00 x + ly - t v 1t 0
251
(7.1.75)
where x = (w - A)/Awo, y = y/2Awo, t = (v/c)(wo/Awo). The function W(x,y) can be expressed in terms of the probability integral with complex argument!
1.
2 i(x+iy) W(x,y) = exp[-(x+iyi] [ 1- y'n { exp (_t 2) dt
(7.1.76)
The intensity distribution I(w) for any relation between parameters y and Awo can be calculated using (7.1.76).
7.2 General Theory of Impact Broadening 7.2.1
Density Matrix Method in the Quasi-Classical Approximation
In the quasi-classical approximation the interaction of the atom with the surrounding particles can be described by the time-dependent perturbation V(t). In this case the coordinates of the perturbing particles can be considered not as dynamic variables but as assigned functions of time, which enables one to introduce the perturbation V(t) instead of the perturbation V(R). It will be shown in this section how the shape of a line is calculated when an atom undergoes an arbitrary perturbation V(t). From the theory of the interaction of a quantum system with electromagnetic radiation we know that for dipole transition 0( --+ p [7.2] J(w) ex
I! pocp(i) exp (-iwt) dtl 2 ,
(7.2.1)
where P ocp(t) is the matrix element of the dipole moment of an atom calculated by means of the perturbed wave functions tpoc(t) and tp p( t). These functions are the solutions of the Schrodinger equation for the Hamiltonian H
= Ho + V(t)
(7.2.2)
.
Formula (7.2.1) is the natural generalization of the classical formula (7.1.3).·It is helpful to write this formula in a form similar to (7.1.6), I(w)
=
~ Re
{1
(7.2.3)
where (7.2.4)
1
Tables of function W(x,y) are given in [7.28,29]
252
7. Broadening of Spectral Lines
or (7.2.5) We shall consider further a transition between the two degenerate levels a and b, the indices 0( and p numbering the states belonging respectively to the initial and final levels. We shall assume that all states 0( are populated with equal probability. In this case /(w)
= E /a.p(w); a.p
therefore instead of (7.2.4,5) it is necessary to assume lJ>('r)
= E Pa.p(t + -r) P:p(t) ,
(7.2.6)
a.p
(7.2.7)
IJ>(-r) = E(Pa.p(-r)P:p(O») . a.p
Equations (7.2.6,7) are easily generalized to the case when a line is formed by a set of transitions between two groups of closely spaced levels. We shall indicate by the indices 0( states belonging to initial levels and by the indices p, those belonging to final levels, and we shall denote by Wa. the population of the state 0(, Ea. Wa. = 1. Then IJ>(-r)
= E Wa.Pa.p(t + -r)Ppa.(t) = E Wa. (Pa.p(-r) Ppa.(O»). a.p
a.p
(7.2.8)
The perturbed functions 'l'a.< t) and 'l' p(t) can be expanded in terms of timeindependent functions of the isolated atom 'l'a.(t)
= ~aa.la.(t)'l'a./exp( -*Ea.d) ,
'l'p(t) = f,aplp(t)'l'p/exp( -*Eplt) ,
where p~~~? = (a:/a.ap'p) is the density matrix of an atom, the matrix elements Pa.lpl and PPa. do not depend on t. The upper indices (O(P) define the initial conditions p~~~?(O) = ba.a.lbpp" The evolution of the density matrix with time is given by the following equation dp i dt = ",(Hp - pH),
H = Ho
+ V(t) .
(7.2.9)
7.2 General Theory of Impact Broadening
253
For correlation function
= L Wcxp;~~!(r) Pcx'p,Ppcx .
(7.2.10)
cxPrx'P'
In the framework of impact approximation, the equation for the density matrix p can be written in the form i -dp = -(Hop - pHo) + (d - P)
(7.2.11 ) . dt Ii dt colI. The last term in right-hand side of this equation describes the evolution of the operator p caused by collisions. We shall assume that the wave functions before collision I[' and after collision 1[" are connected by the relation 1["
= SI[' ,
(7.2.12)
where S is the collision S matrix. According to (7.2.12) the corresponding transformation of the operator p is p ____
st pS .
The increase of p caused by collision with parameters v (impact parameter, velocity, and so on) is
= st pS - p, S = S(v) , where Sit = Ski. Therefore ,1p
(7.2.13 )
(7.2.14) = J[st(v)pS(v) - p] P(v)dv ( ddP ) t colI. where P(v)dv is the number of collisions with parameters v in the interval v, v+dv per second. If by v are understood the impact parameter p and velocity v, then P(v)dv = NVf(v) 2rr.pdpdv, where N is the density of the perturbing particles, and f(v) is the distribution function for v. Substituting (7.2.14) in (7.2.11) and carrying out the Fourier transform, it is not difficult to obtain the system of algebraic equations for matrix elements p ;~~! w) with different indices r:t.' P' and the same indices r:t.P,
(
hcxcx,hW - i(w - wcx'P' )p~~~!(w)
(7.2.15) From (7.2.3) and (7.2.10), we have " WrxPrx'P'PPrxPcx'p'(w) (cxP) } . J(w) = -1 Re { L.J rr. cxpcx'P'
(7.2.16)
It is supposed in (7.2.16) that radiation of definite polarization is of interest. In the case of arbitrary polarization, Pcx'P'P:B must be replaced by Pcx'p,P';.p.
254
7. Broadening of Spectral Lines
Summing with respect to a.'P' and a."P" in (7.2.15) and (7.2.16) in the general case means summing over all stationary states of an atom. However, in calculation of the intensity distribution in a narrow spectral range corresponding to the transitions between the two groups of closely spaced states a. and P, one can assume that the indices a.', a." take the same values as a., and the indices p', P" , the same values as p. Therefore, if the S matrix is known, the spectrum /(00) can be calculated by solving the system of (7.2.15) and using (7.2.16). For an isolated line a. --t p, we have only one equation: 1 - i(oo - roo)Pa.p = Pa.p f[l - S;a.Spp] P(v)dv.
Thus /(00)
= WI Pa.pI2Ya.P
1
2n (00 - 000 - Aa.p)2 + (Ya.p/2)2 '
Yi - iAa.p = f[I-S;a.Spp] P(v)dv, (1' - i(1"
= f[l - S;a.Spp] 2npdp .
(7.2.17) (7.2.18) (7.2.19)
+ itla.), Spp = exp(-rp + itlP)' Therefore the width Ya.P and shift Aa.p are determined by the expressions
In the general case, the S matrix is complex: Sa.a. = exp ( - r a.
Ya.p
= f{1 - exp[-(ra. + rp)] cos(tla. - tiP)} P(v)dv,
Aa.p = f exp[-(ra. + rp)] sin(tla. - tiP) P(v)dv.
(7.2.20)
We shall consider now the intensity distribution in the wing of a line corresponding to the set of transitions a. --t p. If the differences 00 - ooa.'P' are high enough, one can substitute in the right-hand side of (7.2.15) the zeroth approximation p~~!J" = -~a.a."~pp,,(oo - roo)-I, where 000 is the mean value of the frequencies OOa.' p', After this it is not difficult to obtain (7.2.21) where Y=
(E Wa.IPa.pI2rI2Re { E a.p
a.Pa.'P'
Wa.Pa.'P'Ppa. f[~a.a.'~PP' - S:a.,Spp'] P(V)dV} . (7.2.22)
The intensity distribution in the central part of a line is more complex than in the case of a Lorentzian profile. If the S matrix is diagonal (for example, when the perturbation V(t) is adiabatic), the spectrum /(00) can be easily calculated in the general form. In this case the system of equations (7.2.15) splits into independent equations.
7.2 General Theory of Impact Broadening
255
Solving these equations, we obtain I(w)=EW" IP"p 12 y"P } "p 2n (W - Wap - LI"p)2
+ (Y"p/2)2
.
(7.2.23 )
This intensity distribution has the form of the sum of independent Lorentzian distributions. In general case in order to calculate I ( w) one must determine the S \ matrix and then solve the system of (7.2.15). In calculating the S matrix, it is possible to use different approximate methods and results of the genera} theory of atomic collisions. In particular, one can define the S matrix using the method of successive approximations of perturbation theory. The eigenfunction 'l'(t) of the Hamiltonian Ho + V satisfying the initial condition 'l'(to) =
where the coefficients of expansion Smn(t) satisfy the system of equations
We shall introduce the operator
for which V mk
= Vmk exp [*(Em - Ek)t]
Therefore the system of equations for Smn can be written in operator form as
inSmn = E VmkSkn, k
inS = Vs. We shall seek the solution of this equation by the method of successive approximations: S(t) = }
+ (--,;i)t_ J V(t')dt' + (i)2t -;- J V(t')dt' t'_ J V(t")dt" + .... ~
n
~
~
(7.2.24) In order to determine the S matrix corresponding to the collision with parameters v, it is necessary to replace V(t) by t\(t), where Vv(t) -+ 0 at t -+ ±oo, and
256
7. Broadening of Spectral Lines
assume to
=
-00,
S(v)=I+
t
= 00:
00 ~ (-"hj)2 _LV.(t)dt_LV.(t')dt'+ 00 ~ ~ (-"hi) _LV.(t)dt+ .... t
(7.2.25) Let us restrict ourselves to the first two terms of (7.2.25). In this approximation it is easy to obtain for the quantities r and t'/ in (7.2.20) the following expressions: I ~ 1-L 00 (txlV.ls) exp(iwlXSt)dt 12 ra. =21/,2 "a.
1
= - "h
-L00 (txlV.(t)la) dt -
1
{,OO
1/,2 1m ~
-L (txlV.(t)ls)exp(iwlXSt) dt (7.2.26)
The quantity 2ra. is the total probability of transitions from the state a into all other states of the atom. Such transitions shorten the lifetime of an atom in the state tx, which is equivalent to broadening of the corresponding level. The quantity "a. is the phase shift caused by the shift of the level during the collision. The increase of r a. and r fJ increases the width and reduces the shift of the line, see (7.2.20). The broadening caused by collisional transitions is usually called the broadening due to inelastic collisions. 7.2.2 Degeneracy of Levels We shall consider the isolated spectral line corresponding to the radiative transition between levels with angular momenta j\ and h- Such line is produced by the set of transitions between degenerated states hm\ - hm2, where m\ and m2 are the magnetic quantum numbers. We shall write down the equation (7.2.11) for density matrix in the form (7.2.27) where
roo =
whh' and in accordance with (7.2.14) and (7.2.15),
Let us introduce now linear combinations of Pmlm2 which have the same transformation properties as the irreducible tensor operators T; see [Ref. 7.30, Sect. 4.3]. Since
7.2 General Theory of Impact Broadening
257
the required transformation has the form PS(f
=
E (_l)-h-ml( -mlm2!sa)Pmlm2
mlm2
E (_l)-h- ml-(fV2s+ 1 ( h
=
mlm2
-ml
~a )
Pmlm2 '
~a )
PS(f ,
h m2
(7.2.28)
S(f
h m2
where (-mlm2!sa) are the Clebsch-Gordan coefficients [Ref. 7.30, Sect. 4.2]. Multiplying (7.2.27) by (_l)-h- ml(-mlm2!sa), summing with respect to ml and m2, and expressing Pmimi in the collisional term in terms of PS(f, we obtain d PS(f -d t
. " PSI(fIGSI(fI,S(f = lWOPS(f + L..
S'(f'
E
GSI(fI,S(f =
,
(_l)-ml+mi( -m~m~!s'a')Gmimimlm2( -mlm2!sa).
mlm2mimi
The collisional term in (7.2.14) must be averaged over different orientation of the vectors l' and p in space. The interaction of an atom with perturbing particles averaged in such a way is isotropic. This means that the equations defining the irreducible tensor quantities PS(f are invariant under rotations and the matrix G is diagonal with respect to s and a. Moreover the matrix G does not depend on a:
Thus, the system of equations for PS(f has the form d dtPS(f
.
= lWOPS(f + GsPS(f
(7.2.29)
.
This system splits into independent equations for each of the quantities PS(f. The similar approach to the density matrix equation based on the expansion of the operators Pmlm2 in terms of the irreducible tensor operators has been used in [7.17,18]. That the matrix G is diagonal with respect to s and a can be verified by direct calculation. The integrand in (7.2.14) averaged over directions of l' and P must have the form E(m~m~!( -1)qu;V'~_q!mlm2) Kq
K
-q x ( h -
m'2
K
h)
-q m2
'
258
7. Broadening of Spectral Lines
U;
V;
where and are the irreducible tensor operators acting on the functions 'hI ml and 'h2m2' Substituting this expression in the formula defining the matrix Gmjmimlm2 and carrying out the summation of the product of the four 3j symbols in the expression for Gs'q',Sq with respect to mJ, m2, m~, m~, we obtain Gs'q',Sq
=
f>ss,f>qq,G s ,
Gs
= 2: Gs(K) . K
Let us proceed to the calculation of the spectrum J(ro). From (7.2.16), we have J(ro)
=
~Re{ mlm2mjmi;' 2: Wml(P)Jmjmi(P;')~lm2P~~2)(ro)} ,
where p;. is the spherical component of the vector P. We shall assume that the population of the state ml is (2jl + 1)-1. Transforming (7.2.15) in the same way as (7.2.29), we have
h m2
S) -i(ro -
1
roo) + Gs
-(J
•
The quantities p~~2)(ro) are expressed in terms of p~~lm2) in accordance with the second of equation (7.2.28). For the matrix elements of p;., we have [Ref. 7.30, Sect. 4.3].
~ ~~) (jIIIPlih) , 1
A.
h) (jIIiPllh)* .
m2
Therefore, it is necessary to calculate the following sum of the product of the four 3j symbols: S -(J
x (
jl -ml
1
h
-m~
h
h
-m~
m'2
S
)(
-(J
h
-m~
h m'2
-(J S
)(
h
-ml
~) 1
=9f>sl ~ f>.J.,-q = 3f>sl .
Let us recall that 2h - 2ml is even.
h m2
1)( h
A.
-m~
h m'2
1
A
1 h) A m2
h =2:(h -ml m2 x (
)(
~(J)
h)
m~
7.2 General Theory of Impact Broadening
259
Finally we obtain I(w) =
iUlilPiihW . ~Re{ 2h + 1 11: -i(w iUlii P iih)i 2 Re{GJ} 2h+1
11:
1 wo)
+ GI
}
1 (w-wo-Im{G I })2+(Re{GI })2'
(7.2.30)
For width y and shift .1, we have y = -2Re{GJ},
.1
= Im{G I } .
(7.2.31)
Although the possible values of the numbers s are s = h + h, h + h - 1, .... UI - hi, the broadening is completely determined by the density-matrix element Plu and the width and shift of a line are expressed in terms of the real and imaginary parts of GI . As shown in Sect. 7.2.1 in the general cases of a line corresponding to the set of transitions IX - f3 between the two groups of closely spaced levels, the spectrum I (w) is not described by Lorentzian distribution. Only in the wings of a line is the intensity distribution determined by the simple formula (7.2.21). Nevertheless in the case of a line formed by a set of transitions between degenerate states ml and m2 belonging to the levels jl and h, (7.2.16) for I(w) gives the Lorentzian distribution. In order to determine the width y and shift .1 of this distribution, it is necessary to calculate only one quantity GI . Therefore the broadening of a line corresponding to dipole radiative transitions is completely determined by one of the equations (7.2.29), namely by the equation corresponding to the irreducible representation s = 1. Repeating the derivation of (7.2.30) for quadrupole radiative transitions, it is not difficult to show that in this case the broadening is determined by the density-matrix element Psu with s = 2, the width and shift being y = -2Re{ G2}, .1 = Im{ G2}. 7.2.3
Quantum Theory
It has been shown above that in cases when the relative motion of an atom and perturbing particles can be described in the framework of classical mechanics, the theory of the broadening of spectral lines is a natural generalization of the classical oscillator model. We shall consider now the quantum theory of pressure effects in which not only the motion of the atomic electrons but also the relative motion of the atom and perturbing particles is described by the Schrodinger equation. Such a quantum theory enables one to take into consideration the broadening caused by light perturbing particles, especially by electrons. Let us begin with a relatively simplified problem, assuming that the mass of the atom is large as compared with the mass of the perturbing particle, so that the atom is at rest. We also assume that only elastic scattering take place.
260
7. Broadening of Spectral Lines
We shall define the density matrix of the atom using the general rule [7.31]:
= J 'P*(r, R) 'P(r', R) dR ,
p(r, r')
(7.2.32)
where R is the coordinate of the perturbing particle. The stationary states of the system consisting of the atom and perturbing particle are described by the wave functions 1 [
'Prdc(r,R)= cPl1.(r).;v exp(ik.R)+II1.(19)
eXP(ikR)] R '
(7.2.33)
where cPl1.(r) is the atomic wavefunction, li19) is the scattering amplitude, k is the wave vector of the perturbing particle, and V is the normalization volume. Let us expand the wave functions on the right-hand side of (7.2.32) in terms of the wave functions (7.2.33): 'P(r, R)
=L
al1. 'P rdc(r, R) .
11.
We shall expand the density matrix p(r, r') in a sum over atomic stationary states P(r, r')
=L
(7.2.34)
pl1.pcPl1.(r)cPp(r') .
I1.p
As a result, we obtain Pl1.p
I
= a:ap~ [exP( -ik· R) + I: eXp(~ikR)] [eXP(ik. R)
+I
eXP(ikR)] dR _
P
R
*
{
2. J [I Pexp( -ik·RR + ikR)
- al1. ap 1 + V
J:lp] dR} 1 * exp(ik·R - ikR) +11. R +R2
(7.2.35)
The exponential factor exp (-ik· R + ikR) = exp( -ikR cos 19 + ikR) rapidly oscillates everywhere with the exception of the small region cos 19 ~ 1, 19 = o. Therefore in calculating the first two integrals in (7.2.35), we can use the approximation
2.V Jexp( -ik· R + ikR)/( 19) dR ~ 1(0) Jexp( -ik. R + ikR) dR R V R = 1(0)2:i ~ ,
where R is the radius of the spherical volume V and 1(0) is the amplitude of forward scattering. Thus Pl1.p
= a:ap{ 1- 2:i ~[I:(O) -
Ip(O)]
+ ~ J1:(19)/p(19) dO}.
(7.2.36)
If one neglects interaction and assumes that in (7.2.33) and (7.2.35) 111. = Ip = 0, then Pl1.p = a:ap. Therefore the last two terms in (7.2.36) give the collision
7.2 General Theory of Impact Broadening
261
contribution to the density matrix: Ll Pap = przPV R { -T[foc(O) 2ni * - fp(O)]
* + J frzfp
dO } .
(7.2.37)
This expression is the quantum generalization of the quasi-classical expression (7.2.13). In order to obtain the collisional term (dpldt)coli. in the general equation for the density matrix in the impact approximation (7.2.11), it is necessary to take into consideration that the wave functions (7.2.33) are normalized in such a way that volume V contains only one perturbing particle and the time during which one collision occurs is Rlv, where v = hklm is the velocity and m is the mass of the perturbing particle. After multiplying Ll Pocp by NVv I R and averaging over velocities v, we have
( ddPocP ) t
= -N(v«(J' - i(JII») Pocp ,
(J' - i(J" = i
2;
[f:(O) - f p(O)] - J f:f p dO .
We shall express the scattering amplitudes expansions
f oc
1 '" = 2ik -,[.,(21 + 1)[S f - 1] Pf(COS'l9) ,
f
(J' - i(J" (J
(7.2.38)
coIl.
,
and
(7.2.39)
f p in the form
Sf = exp (i2'11) ,
= ;E(21 + 1)(1 - S~*Sh),
of partial-wave
(7.2.40)
(7.2.41 )
n", I = k2LJ21 + 1)[1 - cos2(11rzf - 11p)] ,
(7.2.42) (7.2.43)
Thus the width and shift cross sections (J' and (J" are expressed in the terms of scattering amplitudes or scattering phases. [Equations (7.2.39,42, and 43) were obtained by a somewhat different way in [7.32,33]. Expressions (7.2.41-43) establish the connection between the broadening of lines and the elastic scattering of perturber. In those cases when the perturbation of one of the levels can be neglected, (J' = (J 12, where (J is the elastic cross section (let us recall that)' = 2Nv(J'). In the quasi-classical limit,
n
hl-t mvp, k 2E(21
+ 1) - t 2nJ pdp,
2(11~ - 11~)
-t
11(P) ,
(7.2.42,43) coincide with (7.1.13, 14). Equation (7.1.21) for 11(P) is the limiting expression of the general quasi-classical formula for the phase 2(11~ - 11~), which
262
7. Broadening of Spectral Lines
is valid (in the case of the field IiCnR- n) providing mCn k n -
2
~ 1.
Ii
This condition can be rewritten in the form Po~A.
= Ii/mv,
where Po is the Weisskopf radius (7.1.24). For heavy perturbing particles, this condition is always fulfilled. But in the case of light perturbing particles, in particular for electrons, it is violated. We shall consider the dependence of a' on the perturber velocity v at high v, i.e., in the Born approximation. The cross section a' of (7.2.42) can be written in the form
a' = ~ J If,,(~) - fp(~)12dO .
(7.2.44 )
For electron scattering in the Born approximation, f(~)
=
2me2
(7.2.45)
1i2q2 [.2" - F(q)] ,
where .2" is the total number of electrons in the atom, F(q) is the atomic form factor (scattering factor) and q = 2k1i- 1 sin ~/2. Substituting this expression for f(~) in (7.2.45), we obtain , _ 4nm 2e4 2Jk [F,,(q) - Fp(q)f d
a -
1i4k2
q4
0
(7.2.46)
qq.
At high velocities, the scattering amplitude has a very sharp maximum in the region of small angles. This means that the integral (7.2.46) does not depend on the upper limit (q = 2k, when ~ = n/2). Thus integration in (7.2.46) can be extended to q = 00. After this the integral in (7.2.46) no longer depends on k and
a' ex k- 2 ex v- 2 ,
y ex
V-I.
Thus at high velocities, the width of a line is inversely proportional to the velocity for any type of interaction. It is necessary only that the integral (7.2.46) converges. The formulas obtained above are easy to generalize so that they also include inelastic collisions. By repeating the derivation of the expression for the collisional term (dp/dt)col1. it is not difficult to show that (7.2.39) and (7.2.41) preserve their form. But the quantities Sl are now Sl = exp( - 2rl - i2f11). Therefore a' = ;2:.(21 + 1}{1 -
a"
= - ;
2:.(21
exp[-2(r~ + r~)] cos2(f1~ - f1~)},
+ 1)exp[ -2(r; + r~)]
sin 2(f1~ - f1~) .
(7.2.47)
(7.2.48)
7.2 General Theory of Impact Broadening
263
If the perturbation of one of the states can be neglected, then (I'
= ;'L-(21 + l){l - exp(-2rl)cos2t//} =
1 2«(lel.
where (leI. and scattering.
7.2.4
(7.2.49)
+ (lined, (linel.
are, respectively, the cross sections of elastic and inelastic
Quantum Kinetic Equation Method
In this section we shall generalize the density-matrix equation discussed above taking into consideration not only the motion of the perturbing particle but also the motion of the atom. Such a generalization is necessary for understanding the very important problems connected with the statistical dependence of the impact and Doppler broadening [7.20,34-38]. In many applications of the theory of spectral line broadening such as plasma diagnostics, effects of the statistical dependence of the impact and Doppler broadening do not play a significant role. They are of special interest for nonlinear laser spectroscopy [7.39]. The densitymatrix equation describing this general case has the same structure as (7.2.11),
i (d -dp = -(Hop-pHo)+ - P)
dt
dt
h
.
(7.2.50)
colI.
But now the unperturbed wave functions must be taken in the form ~mp
(7.2.51)
= ~m(r) exp (ip· R) ,
where R is the coordinate of the center of mass of the atom, m is the quantum number describing the atomic state, p is the wave vector of the atom as a whole, and hp is the momentum of the atom. In (7.2.16) for the intensity distribution /(0) in the case of an isolated spectral line m --t n, the following substitutions must be made:
ex --t mpo, p --t meo, ex'
--t
mp,
p' --t me, Wex = W(Po),
P
--t
d exp (ik· R) ,
where k is the wave vector of the photon, and d is the electric dipole moment. In addition, the sum over expex' p' must be replaced by an integral over Po, p, "0, ". As
(mprd exp (ik· R)lmc) ex: d mn t5( -p + k
+ K) ,
(nKold exp (-ik· R)lmpo) ex: d:z,.t5( -KO - k
+ Po) ,
264
7. Broadening of Spectral Lines
it is not difficult to obtain 1(w)
2 = Id mn l Re{f dp dp W(P ) pmpo,n(Po-k)} 1[ 0 0 mp, n(p-k)
(7.2.52)
= Id mn l2 Re{J dpF(P, p - k)} , 1[
where F(p, p - k) = f dpo W(Po) p:P~~~~~~) is the corresponding density matrix element, averaged over the initial distribution of Po. We shall omit the factor Id mn l 2 everywhere below. Let us introduce the notation (dp/dt)coli. = Gp, where G is the operator describing the evolution of p due to collisions. From (7.2.50), we obtain -W(P) +
i(
W -
~pok) F(p, p -
k) = (Gf)p,p-k,
(7.2.53)
where m is the mass of an atom I. Equations (7.2.52,53) have the same form as (7.1.54) and (7.1.56). Now, however, it is possible to express the collisional term (G f) in terms of the exact scattering amplitudes 2 • The general expression of (Gf) is very complicated due to the fact that density matrix is defined in the laboratory system of coordinates and the scattering amplitudes are defined in the system of the center of mass of the colliding particles. We shall give below the expressions for (GF) in two limiting cases of light and heavy perturbing particles, mp ~ m and mp ~ m, where mp is the mass of the perturbing particle, and m is the mass of the atom. In the first case, in the limit mp/m ~ 0, (GF)p,p_k
=-
G- iA) Fp,p-k ,
(7.2.54 )
y/2 - iA = N(vp(a' - ia"») , where a' and a" are respectively the width and shift cross sections, determined by (7.2.39-43), and vp is the velocity of the perturbing particle. Substituting (7.2.54) in (7.2.53), it is not difficult to show that the spectrum 1(w) has the form of a convolution of the Doppler and Lorentzian distributions: 1( ) =!R W
1[
e
{f i(w-A-hp W(P)dp } k/m)+y/2 ' o
hpok - - =v·k, m
(7.2.55)
where v is the velocity of an atom.
I
A tenn proportional to k2 is omitted in this equation: (Hop - pHo)mp,np-k
{Em -Eft 2
+ ~:[p2
- ki]} ~ (p -
pmp,np-k (IiWo
+~
The general expression for (Gf) is given in [7.37].
P.k).
= Pmp,np-k
7.2 General Theory of Impact Broadening
265
In the opposite limiting case of light atom and heavy perturbing particle mp~m,vp~v,
hp (GF)p,p-k = -N-;;[a'(p) - ia"(p)] F(p, p - k) A
- N hp 8(p) F(p, P - k)
m
+ N hp J dOq/~(q, P)!n(q, p) F(q, m
q - k) ,
(7.2.56) where a' and a" are, as before, the width and shift cross sections, but now they are dependent on the wave vector p of the atom: 8(p)
= J dOq/~(q, P)!n(q,
p)
=
n22 )21 + I)(S~ - I)(S~ - 1)*. (7.2.57) p
The equation (7.2.57) coincides with the expression defining the elastic cross section a if !;!n is replaced by l!nl 2 or l!mI 2 • In the collisional term (7.2.56), the cross section 8 plays the role of the elastic cross section a. The cross section 8 differs from a, being in the general case complex. Ifthe scattering is isotropic, or almost isotropic, then 8(p) '::::' 4n!;'!n. Taking this into consideration we obtain from (7.2.56)
= -Nv[a'(v) -
ia"(v)] F(p, P - k)
- Nv8(v) F(p, p - k)
+ Nv8(v)f dOg F(q,
(GF)p,p_k
(7.2.58) 4n
q - k) .
Equation (7.2.53) takes the form [cf.(7.1.67)] W(P)
i(w - k. v) + Nv(a' _ ia"
+ 8) = F(p, p -
Nv8 .( k )+Ni(' 1 w.v v a -
k)
dOq
. "+-/-4 la a n F(q,q-k).
Integrating the left- and right-hand side of this equation over dO p and taking into consideration that for isotropic distribution W(P)
= W(P2)' 4np
it is easy to find
w(p)dp
dO p
= dOv ,
JF(p, p-k)dOp and then using (7.2.52) to obtain the spectrum
/(w) = .!.Re { Jw(v)dv n
= w(v)dv,
d~ ~<;; - k.v) + Nv(a'l1 ia" + 8)
}
J 4iC
.
v
I-Nv8J 4n i(w-k.v)+Nv(a'-ia"+8)
(7.2.59)
266
7. Broadening of Spectral Lines
This equation differs from (7.1.68), taking account not only of the perturbation of the internal atomic state, but also of the perturbation of the motion of the atom as a whole. All the cross sections contained in (7.2.59), (1', (1", and ii, are dependent on v. When N ~ 0, (7.2.59) coincides with the usual Doppler distribution (7.1.57). At high densities when one can neglect the term k °v, (7.2.59) takes the form
I NV(1' /(w) = - fw(v)dv 2 2 11: (w - NV(1") + (Nv(1')
(7.2.60)
•
Instead of the usual Lorentzian distribution, (7.2.60) describes a superposition of Lorentzian distributions, each having width 2Nv(1', shift NV(1", and relative weight w( v). If one assumes that the scattering in one of the states m and n can be neglected, when ii = 0, then (7.2.59) takes the form
/( w ) -.!.R {f W(v)dv - 11: e i(w _ k oV) + NV(1' -
iNV(1"
}
.
(7.2.61)
This expression differs from the usual convolution of the Doppler and Lorentzian distributions containing lNV(1' ( v) and NV(1" ( v) instead of the averaged quantities y = IN(V(1') and LI = N(v(1"). The intensity distributions of (7.2.60,61) are asymmetric. In the case (1' = (1" = 0 (the scattering is purely elastic and 1m = In), (7.2.59) describes a narrowing of the Doppler profile similar to that given by (7.1.68). The parameter Nvii plays the same role as the frequency of collisions in (7.1.68). We shall consider now the case of high densities «(1' = (1" = 0, Nvii't>kov):
f
I ~ k 2 v2 -:-:-_ _ _=_=_ 411: i(w-kov)+Nvii iw+Nvii - -3-(iw+Nvii)3 .
dO"
For frequencies w4.Nvii (7.2.59) gives
II}
/(W)=.!.Re{fW(V)dV 11: iw + _k2V2(Nvii)-1 3
We shall introduce the notation D = v/3Nii. Then
/()
w =
2
f
-
()d k Re{D} W
v
V
11:
1
0
(w + k2Im{D})2
+ (k2Re{D})2
(7.2.62)
If 1m = In, and ii coincides with the elastic cross section (1, then Im{D} = 0 and Re{D} = D is the diffusion coefficient depending on v instead of (v). In the general case of complex ii and D, the real part of D determines the width and the imaginary part of D determines the shift. The width 2k2Re{D} is proportional to N- 1. Thus, at Nvii 't> k v, the Doppler distribution narrows due to collisions. The 0
7.2 General Theory of Impact Broadening
267
resulting line profile has the form of a superposition of Lorentzian distributions with widths 2k 2 Re{D} and shifts k2 Im{D}. This profile is asymmetric. If (J' and (J" are less than Ii but are not equal to zero, then on increasing N, there is first a narrowing of the Doppler contour to a width Nva', and then a broadening. The results of the calculation of the spectrum J (OJ) by means of the quantum kinetic equation contain a number of new elements, the most interesting of which are the following. Even in the treatment of the simplest example, purely impact broadening, qualitative differences from the formulas usually used arise. Only in the case of broadening by light particles, such as electrons, does a single Lorentzian contour arise, with width 2N(vp(J') and shift N(vp(J"), where vp is the velocity of the electrons and the angle brackets denote averaging over vp. In the general case of mp m, after averaging over the velocities of the perturbing particles vp, the cross sections (J' (v) and (J" (v) contained in the collisional term retain their dependence on the velocity v of the atom. As a result, the following intensity distribution arises: r-..J
r-..J
J(OJ) = /w(v)dvNv(J'(v) 1C
I [OJ - NV(J"(v)]2
+ [Nv(J'(v)F
.
(7.2.63)
This distribution is asymmetric. The greatest difference arises in the case of scattering of a light atom by heavy (almost at rest) perturbing particles. The perturbations due to different perturbing particles combine in completely different ways, depending on the masses of these particles. If the perturbing particles of type 1 and type 2 are light, then the sum of the corresponding widths and shifts arises:
~
- iii
= NI (VI (JD + N2 (V2(J~) + i NI (VI (J~') + i N2 (V2(J~) .
But if the perturbation is created by heavy particles (type 1) and electrons (type 2), then (at Ii = 0)
w(v)dv
}
All this is a reflection of the statistical dependence of the Doppler and impact broadenings. The second characteristic feature is the fact that the cross section Ii responsible for the collisional compensation of the Doppler broadening is complex. Let us recall that Ii =f:. 0 if both the scattering amplitudes 1m and In are nonzero. It is not difficult to show that in the examples treated, asymmetry arises for two reasons - the dependence on the atomic velocity of the parameters of the equation, and the fact that the cross section Ii is complex.
268
7. Broadening of Spectral Lines
In calculation of the width of the resulting spectrum, all characteristic features of collisional broadening connected with the effect of the statistical dependence of the Doppler and impact broadenings are usually not very important. Nevertheless they can be of interest for some other problems, for example, those arising in the theory of nonlinear resonances in the spectra of gas lasers [7.38,39] (see also the bibliography given in [7.20]. 7.2.5
Absorption Spectrum
The energy absorbed in one second by a system of electric charges interacting with an electric field tI(R, t)
= ~{tlo exp [i(wt -
k·R) +
tlo exp [-i(wt -
k·R)]}
is (in the electric dipole approximation)
Q = -tl.J = Re {iwtlo ·dro exp(ik.R)} , where d = dro(R) exp (iwt)
+ d~(R) exp (-iwt)
is the electric dipole moment induced by the field tI(R,t). The quantum generalization of this expression for Q has the form
Q = Re [iw
tlo Trace {d exp (ik.R) p(w)}] .
(7.2.65)
Here d is the electric dipole operator, R is the coordinate of the center of mass of the atom, k is the wave vector of the photon, and p( w) is the Fourier component of the density matrix, satisfying the equation dp i "i dt - h (Hop - pHo) - Gp = h (tI·dp - ptl·d).
(7.2.66)
This equation contains an additional term describing the interaction of the atom with the electric field. Solving this equation by the method of successive approximation, it is possible by means of (7.2.65) to determine the absorption (or emission) power Q. If a set of transitions IX --+ P are perturbed by the field tI (the frequencies wa.p ~ w), then using (7.2.65) we obtain
Q = Re {iw tloEda.pJ dp PPp,a.p+k(W)} , a.p
(7.2.67)
where p is the momentum of the atom. We shall neglect the collisional term simplicity and solve (7.2.66) in the linear approximation according to the field. We shall substitute in the right-hand side of (7.2.66) the zeroth-order density matrix, which is diagonal in indices IX, p and
7.2 General Theory of Impact Broadening
269
p,p':
p~ipp = NpW(p),
P~o;+k,rxP+k = NrxW(p + k) ~ NrxW(p) ,
where Np and Nrx are respectively the populations of the states p and IX, and W(p) is the distribution function for momentum p. Since k~p, we can assume that W(p + k) ~ W(p). In this approximation we have [cf. (7.1.57)]
i 1 Ppp,rxp+k = 2f/o·dpiNp-Nrx)W(P)i(w_wo+hp.k/m) '
1(w)
= !Re {lim J. n
6-+0
W(p)dp } hp·k/m) + e
I(W - Wo -
Therefore the absorbed power Q is proportional to the difference of the populations (Np - N r,.) and the function 1(w), which describes the usual Doppler distribution in the spectrum of spontaneous emission. In the general case, when (7.2.66) contains the collisional term, the expression for Q remains the same, but the function 1(w) has a more complex form describing the Doppler and impact broadenings. All results obtained above for the spectrum of spontaneous emission can be obtained also from (7.2.65, 66). By solving (7.2.65) in the next approximations according to the field, it is possible to calculate the power of nonlinear absorption [7.38]. 7.2.6
Interference Effects: Narrowing of Spectral Lines
In cases when the frequencies of some atomic transitions coincide or are so closely spaced that the corresponding spectral lines overlap, specific interference effects can arise [7.40]. In some particular cases, these interference effects are so important that they alter the entire picture of the broadening. We shall illustrate this by considering as an example the four-level system shown in Fig. 7.2. We shall assume that the transition frequencies Wkt = WI and Wmn = W2 are almost
~---I.--n
Fig. 7.2. Levels scheme and the radiative transitions which are considered
270
7. Broadening of Spectral Lines
the same, co, ~ CO2, but that all other transition frequencies differ very much from CO, and CO2. Therefore in (7.2.16) and (7.2.15), the indices a.,a.',a." stand for k,m and the indices p,P',P" stand for I, n. We shall denote the pair of indices k,1 by 1 and the pair of indices m, n by 2. We shall use the notation Wk = W, and Wm = W2. By solving the system of equations (7.2.15), we obtain J(co) = !Re {W,IP,1 2G22
+ W21P212G l1 -
W2 P ,Pi G'2 - W,pjP2G2'}, G" G22 - G2' G'2 (7.2.68)
11:
where Gl1 = i( co - cod + J (1 - SaSIl) P( v) dv , G22 = i(co - CO2) + J(1 - S;mSnn)P(v)dv, G'2
(7.2.69)
= - JS;kSnlP(v)dv ,
G2' = - JS;"'SlnP(v)dv. We shall assume that S matrix elements obey the relations
= SIl, Smm = Snn, Skm = Sin, Ski = Smn = Skn = Sml = 0 .
Sa
Smk
= Snl ,
(7.2.70)
This means that collisions produce only the mutual perturbation of the states I and n and also the states k and m. It will be shown that such a situation can arise in a number of systems. Using (7.2.70) and also the unitarity properties of the S matrix, L:ISab12
=
1,
b
we have S;kSnl = ISmk 12 = 1 - ISmm 12 , S;"'Sln
= ISkm 12 = 1 -
(7.2.71 )
ISa 12 •
From the general definition of the inelastic cross section u, it follows that (7.2.72) where N is the density of the perturbing particles, v is the relative velocity, and the angle brackets denote averaging over velocities. In Boltzmann equilibrium the level populations W" W2 and transition frequencies are connected by the relations N(vUkm)
=
i,
N(vumk)
Thus G" = i(co - co,) + y1/2, G'2
= -(WI/W2)yI/2,
=
i,
W,y,
= W2Y2
.
G22 = i(co - CO2) + (WI/W2)yI/2, G2'
= -y1/2 .
(7.2.73)
(7.2.74)
7.2 General Theory of Impact Broadening
271
We shall introduce the notation COl
= COo -
15,
CO2
= COo + 15,
215
= L1 .
(7.2.75)
After this (7.2.68) gives
I(co)
=~
. (WIYI + W2Y2)I(co - t5)PI - (co + t5)P21 2 2n [(co + I5)(co - 15)]2 + [YI(CO - 15) + Y2(CO + 15)]2
(7.2.76)
We shall consider now the limiting cases of small and high values of y. In this first case, when YI,2/t5~ 1, the second term in the denominator of (7.2.76) is small, and the function I(co) has two sharp maxima at co = ±t5. Equation (7.2.76) can be rewritten in the form
I(co)
~
.!. ( n
WIy!lP I 12 (co+t5)2+YI
+
W2Y2!P2 12
(CO-t5)2+y~
) .
(7.2.77)
In the other limiting case, when YI, 2/15 ~ 1, (7.2.76) has one sharp maximum at
co ~ COM = YI - Y2 t5 . YI +Y2 In the vicinity of this frequency, (7.2.76) gives
.!.
I(co) '" (WIYI + W2Y2)IY2 P I + YI P21 2 r 2YIY2(YI + Y2) n (co - COM)2 + r 2 '
(7.2.78)
where
r =
4y IY2 152 (YI + Y2)3 .
Equation (7.2.78) describes a Lorentzian distribution with width rex N- I . Therefore at low pressures, when Y\,2/t5 ~ 1, the two components of a line are independent and their widths YI and Y2 are proportional to N. On further increase of N when the components of the line begin to overlap, the picture of the broadening alters completely, and in the limiting case of YI, 2/15 ~ 1 a single Lorentzian distribution with width proportional to N- I arises. In the far wing of a line co~Y\' Y2, 15, in accordance with (7.2.76), the spectrum I(co) has the form
I(co)
~
WIYI ~ W2Y21w(P I -P2) :/(PI +P2)i2
(7.2.79)
Note that in the particular case PI = P2, I(w) ex co- 4 . All qualitative features of the example considered above are connected with the conditions (7.2.70) for the S matrix. There are a number of systems for which the S matrix obeys such conditions. We shall consider two subsystems I and II with the levels A, B and a, b, respectively, shown in Fig. 7.3a. Let us assume that subsystem I is perturbed by collisions, but they do not act on subsystem II.
272
7. Broadening of Spectral Lines 4 (8b) J(Ab)
8--
2 (8a)
A--
f(Aa)
b
a
Fig. 7.3. (a) Levels scheme of subsystems I and II (b) Levels scheme of the whole system.
The system as a whole has four levels: I(Aa), 2(Ba), 3(Ab), and 4(Bb), shown in Fig. 7.3. Two transitions 3 --+ 1 and 4 --+ 2 correspond to the tr~sition a --+ b of subsystem II. If the interaction between subsystems I and II is not great, the interaction produces a splitting of the frequencies W31 - W42 = A I- 0, but does not influence the probability of the collisional transition A-B in subsystem I. In this case the S matrix has the form SII [ S21 S31
SI2
SI3
S14]
S22 S32
S23 S33
S24 S34
S41
S42
S43
S44
_ -
SAB SBB
00 0] 0
0
0
SM
SAB
0
0
SBA
SBB
[SAA SBA
'
(7.2.80)
i.e., is in full agreement with the conditions (7.2.70). Thus the example considered above describes the rather typical situation when the relaxation processes in subsystem I perturb the spectrum of subsystem II. We assume of course that subsystems I and II interact. If this interaction, and consequently also the frequency splitting A, is great enough, i.e., YIA ~ 1, then relaxation processes in subsystem I produce broadening of the line, corresponding to the radiative transition is subsystem II. In the other limiting case of weak interaction (y I A --+ 00), the spectrum of subsystem II is not sensitive to the relaxation processes in subsystem I. For a given value of A, the inequalities YIA ~ I and YI A ~ 1 correspond respectively to low and high densities N. Therefore, on increase of N, there is first a broadening of the spectrum of subsystem II to a width rv y, and then a narrowing proportional to N- I . The spectrum narrowing with increase of N is due to the interference of the amplitudes of the radiative transitions when the corresponding line components begin to overlap. Let us consider for example the splitting of the term 2P in a strong magnetic field H [Ref. 7.30, Sect. 8.2]: (7.2.81 )
7.3 Broadening of Lines of the Hydrogen Spectrum in a Plasma
273
where J4J is the Bohr magneton, A is the fine structure constant, and ML,Ms are the magnetic quantum numbers of the orbital and spin angular momenta. We shall which gives three consider the magnetic dipole transition Ms = --+ M~ = components of the line corresponding to the three possible values of ML = 0, ± 1. The frequency splitting of these components is of the order of A. The cross section of the spin reorientation (is usually is less than the cross section of the orbital angular momentum reorientation (iL. Therefore one can assume '
!
-!,
If Y ~A, collisional reorientation of the orbital angular momentum produces broad(ML = 0, ± I). If density N is so ening of the transitions Ms = --+ M~ = high that y > A, then the relaxation transitions ML --+ M{ begins to be ineffective in broadening the spectrum of the transition Ms = M~ = Moreover, on increase of N, a narrowing of the spectra must be observed. In the limiting case of N(V(iL) ~A, the width of the spectrum is less than the initial splitting A. It must be noted that the condition N(V(iL) ~A can be fulfilled only for light atoms for which the fine splitting is not too great. For example, the fine splitting of the ground level of Li atom is 0.34 cm -I. As will be shown in Sect. 7.3 the interference narrowing of a line can take place in the spectra of highly excited hydrogen atoms.
!
-!
!-
-!.
7.3 Broadening of Lines of the Hydrogen Spectrum in a Plasma Preliminary Estimates
7.3.1
The main contribution to the broadening of lines of the hydrogen spectrum in a plasma is due to the linear Stark effect in the fields of electrons and ions. The perturbing particle with charge Ze produces the electric field S = ZeR - 2 • Using the well-known formula for the linear Stark effect [7.30] Am = 3/2n (nl-n2)ea oS/Ii, where n,nl,n2 are the principal and parabolic quantum numbers, we can assume Am = C2/R2. The constant C2 for the level with principal quantum number n has the order of magnitude Zn(n -1 )e2ao/1i ~ Zn(n -1) [cm2 s- I ]. We shall estimate the magnitude of the dimensionless parameters (7.1.39) h
rv
e
2 )3
N. (n(n - l)e ao e
liVe
k '
rv I
N (Zn(n - l)e2ao I IiVi
)3
(7.3.1 )
where Ve and Vi are the velocities of electrons and ions, respectively. The range of temperatures and densities for which hi ~ 1 and he ~ 1 is usually of greatest interest. This means that the field of the ions is quasi-static and the electrons cause impact broadening.
274
7. Broadening of Spectral Lines
7.3.2 Ion Broadening: Holtsmark Theory For hi ~ I, number of ions in the sphere of Weisskopf radius is large and the binary approximation is inapplicable. Thus the main problem which arises in considering ion broadening is to find the quasi-static intensity distribution taking into account the simultaneous action on the atom of a large number of ions. We shall consider the component ex-p of a line and denote the shift of this component in the field C by [Ref. 7.30, Sect. 7.2] (7.3.2) where ex and p are the set of parabolic quantum numbers nln2m and intensity distribution at a given field C is given by
n~n~m'.
The
(7.3.3 ) Averaging this expression by means of the distribution function W(C), we obtain (7.3.4 ) The resulting ionic field C is equal to the vector sum over all ions,
The function W(C) determines the probability of a given magnitude of the absolute value of C. This function was calculated by Holtsmark in the ideal gas approximation. (A detailed discussion is given in [7.25]). In this approximation, one assumes that each of the ions can with equal probability be located at any point of the volume independently of how all the other ions are located. Therefore the function W(C) can be calculated in the following way:
WH(C) dC
=
(15
(c -Ze I: R:) dC) k=IR k
= JdR I JdR2 ... 15 (c-zeI: R:) dC V V k=IR k = (2
1 1t
dR I dR2
.
NV
(.zep.R k )
)3 J - J - ... J dp exp (Ip· C) ~ exp -I V
V
k=l
R3
dC .
k
Here we use the well-known representation of the t5-function, introducing the additional integration over p. By changing the order of integration over R and
7.3 Broadening of Lines of the Hydrogen Spectrum in a Plasma p, we obtain in the limit V
WH(C)
275
--> 00
=
(2~)3 J dp exp (ip
=
(2~)3 J dp exp (ip
0
0
C) {I -
~J dRk [1 _ exp (-ize~tk )]}
N V
C) exp { -N J dR [I - exp ( _/e;;R) ] }
Integration over R gives
J dR [I - exp ( _i ze;3oR )]
=
1~(2nZep)3/2 .
Then it is possible to carry out the integration over the angular variables of the vector p. As a result we have
WH(C)dC
= d: .1t (~) ,
(7.3.5)
where
.1t(f3)
Co
=
~f3J:xsinx exp 4
= 2n ( 15
[-
(~r/2l
(7.3.6)
dx,
)2/3ZeN 2/3 = 2.6031 ZeN 2/3 .
(7.3.7)
Values of the function .1t(f3) for a wide range of values of the parameter f3 are given in Table 7.1. In addition the function .1t(f3) is shown in Fig. 7.4. The maximum of the function .1t(f3) corresponds to the point f3 = 1.607. In the two limiting cases, high and low values of f3, the function .1t(f3) can be approximated by the series 1.496 f3-S /2( 1 + 5.107 f3- 3/2
.1t(f3)
~
{
tn
f32 (1- 0.463f32
+ 14.93f3- 3 + ... )
+ 0.1227f34 + ... )
(f3~ 1).
(f3 ~>1),
(7.3.8) (7.3.9)
If in the expression for .1t(f3), the field Co is redefined by putting Co = ZeR(;2, where Ro = (3/4nN)I/3, then instead of (7.3.8) we have .1t(f3) ~ l.5f3- S/2 , which coincides with the binary distribution (7.1.26). We note that from the practical point of view the difference between the two definitions of Co is unimportant. In accordance with (7.3.8), in the wing of the line,
I(w) ~ (w - wO)-5/2l.5D~p(B~p)3/2C~/2 ,
(7.3.10)
~p
in full agreement with the binary distribution (7.1.28). This is due to the fact that the strongest fields are created mainly by the nearest ion. It must be noted that the distribution function of the binary approximation is fairly close to .1t(f3) everywhere, with the exception of the range of low values of f3. Weak fields,
276
7. Broadening of Spectral Lines
Table 7.1. Holtsmark distribution function
p
Jf(P)
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.2
0.00000 0.0042245 0.016665 0.036643 0.063082 0.094596 0.129587 0.166360 0.203233 0.238641 0.271221 0.299870 0.323782 0.342461 0.355702 0.363566 0.366334 0.364456 0.358502 0.349109 0.336939 0.306821
Jf(P) 0.272746 0.238221 0.205563 0.176063 0.150242 0.128118 0.109422 0.093753 0.080674 0.069765 0.060654 0.053023 0.046604 0.041180 0.036573 0.032640 0.029263 0.026349 0.023822 0.021619 0.019690 0.017993
P 2.4 2.6 2.8 3.0 3.2 3.4 3.6 3.8 4.0 4.2 4.4 4.6 4.8 5.0 5.2 5.4 5.6 5.8 6.0 6.2 6.4 6.6
P 6.8 7.0 7.2 7.4 7.6 7.8 8.0 9.0 10.0 11.0 12.0 13.0 14.0 15.0 17.0 20.0 24.0 28.0 33.0 38.0 43.0 48.0 53.0
Jf(P)
0.016494 0.015165 0.013981 0.012922 0.011974 0.011120 0.010350 0.007438 0.005561 0.004289 0.003392 0.002739 0.002249 0.001875 0.001351 0.0008856 0.0005537 0.0003733 0.0002457 0.0001718 0.0001256 0.0000952 0.0000741
0.4
/ '~
OJ 0.2
/ o
/
~
/
"~ .......
2
p-
3
r---5
4
Fig. 7.4. Holtsmark distribution Jf(P)
obviously, are produced by a large number of comparatively distant ions. The calculations of Holtsmark intensity distribution for a number of hydrogen spectral lines were carried out in [7.41]. It is convenient to rewrite (7.3.10) introducing the effective Stark-effect constant B for a line as a whole [7.42]
I(w) ~ 101.5(w - wO)-5/2(B80)3/2,
10
= L/~p, ~p
(7.3.11)
7.3 Broadening of Lines of the Hydrogen Spectrum in a Plasma
277
where in accordance with (7.3.2) B
3/2 -_10-I",
L.. I~p
(e)3/2
h
~p
(Z~~
- Zpp)
3/2
(7.3.12)
.
Here Z is the coordinate of the atomic electron. Comparison with the results of accurate numerical calculations shows that for a hydrogenlike ion with nuclear charge ~e, the constant B can be approximated by the expression B
= (~)2/3 _h_(n2
_ n'2 ),
(7.3.13 )
~me
8
where n and n' are the principal quantum numbers of the initial and final levels. Similarly for the contour of the line 1(OJ) = E~p/~p( OJ), one can also use the approximate expression [7.42] (7.3.14 ) The dependence of TH(fJ) on [3 is given in Table 7.2. At high values of [3, TH ([3) ---+ 1.5 [3-5/2. Since the contour of the line (7.3.4), and also (7.3.14), is symmetrical with respect to OJo, the Holtsmark width of a line LlOJH is approximately equal to 8BSo. Using (7.3.13), we obtain for the hydrogen spectrum, (7.3.15) Formula (7.3.14) describes sufficiently well the contour of the line everywhere apart from the central region. In order to improve the Holtsmark theory one must take into consideration the mutual correlation of ion positions. In the Holtsmark theory, the exponential factor exp[-V(RI' R 2 ,
•••
)jkT]
in the expression for probability of an ion configuration R 1, R 2 , ••• with potential V is neglected. Thus, the relative probability of such configurations to which high positive values of V correspond are overestimated. In particular, the Holtsmark theory overestimates the probabilities of large frequency shifts /C, i.e., of high values of S, and underestimates the probabilities of low /c. The simplest way of introducing the corresponding corrections to the Holtsmark theory is to take the Debye-Hiickel screening into account. The field of the ion surrounded by a cloud of other ions and electrons of the plasma decreases at large distances as
Table 7.2. Function TH(P)
P TH(P)
0 0.1
0.5 0.1
1 0.098
2 0.086
3
5
7
10
15
0.070
0.039
0.02
0.0072
0.0023
20 0.00099
278
7. Broadening of Spectral Lines
0.6,-------,----,----,---...,-----, 0.5 t-----.~---+----+---_::__+--___l 0.41------h~+_'<~-+__/_1'
§. ~ 0.2t--tJ~f_+--~~~---+--___l
o
4
5
jJ-
Fig. 7.5. Hooper distribution £'D(/1) for the neutral point [7.43]
exp (-RjRo), where Ro is the Debye radius
Ro=
kT
+ Z2)
4nNe2(1
(7.3.16)
•
The difference between the distribution function Jfo(f3) taking this screening into account and the Holtsmark one depends on the magnitude of the parameter IX
= Ro
Ro
ex N I / 6 T- I / 2
(7.3.17)
.
The quantity IX- 3 is equal to the number of ions inside the Debye sphere No. As IX -+ 0 (Ro -+ 00), the function Jf o(P) coincides with Jf(P). The dependence of the function Jfo on P is shown in Fig. 7.5. [7.43].1 The difference between Jfo(P) and Jf(P) becomes noticeable at IX ~ O.4(No ~ 16). Thus, the condition of applicability of the Holtsmark distribution is the inequality -3 _ IX
_
-No -
4n 3
(
kT ) 4ne2 (1 +Z2)
3/2
-1/2:.;
N
~1.
(7.3.18)
A special situation arises in those cases when the broadening of lines of hydrogenlike ions He+, Li 2+, and so on is considered. In calculating W(C) it is necessary to take into account the repulsion between emitting and perturbing IOns.
I Calculations in [7.43] are not based on the simple picture of Debye shielding and are more rigorous and rather complicated.
7.3 Broadening of Lines of the Hydrogen Spectrum in a Plasma
279
7.3.3 Correction for Thermal Motion
Due to the thermal motion of ions, the amplitude and direction of the vector tff varies with time. Changing the amplitude of tff causes the changing of the level splitting and leads to a phase modulation. If the vector tff rotates very slowly, the angular momentum of the atom follows tff adiabatically. This results in the change of the dipole moment component in the direction of a photon wave vector k. Therefore the slow reorientation of vector tff produces amplitude modulation. The level splitting with respect to M components is of the order of Btff. Reorientation of the vector tff can be considered to be slow when Btff ~ 1/., where • is the typical time of reorientation of tff. In the opposite limiting case Btff ~ 1/., the magnetic field arising in the rotating coordinate system induces transitions between sublevels M. This means that perturbation is no longer adiabatic. The corrections for thermal motion of ions taking into consideration all above-mentioned effects were calculated in [7.44,45]. According to these calculations, the central part of a line is the most sensitive to the thermal motion of ions. The experiment [7.46] revealed that the dynamic effects of the ion influence substantially the shapes of the hydrogen lines. These effects can be taken into account by a modified relaxation theory of line broadening [7.47,48] and the "Model Microfield Method" [7.49-52]. The dynamic effects can be very important in case of multiply-charged ions [7.51]. 7.3.4
Electron Broadeningl
A theory of broadening of lines of the hydrogen spectrum by electrons must take into account the nonadiabatic nature of the perturbation. Collisional transitions between the states of the same level play the main role in the broadening. We shall consider the spectral line corresponding to a radiative transition between the level a (the states (x, (X' ••• ) and the level b (the states p, P' ... ). The intensity distribution J(w) can be calculated by means of (7.2.16). It is necessary to determine the elements ofthe S matrix and solve the system of equations (7.2.15). The collisional term in (7.2.15) can be written in the form (7.3.19) where
f]J
is the collision operator, 00
f]J
00
= N I vf(v)dv I2rcpdp{1 o
S;Sb} .
(7.3.20)
0
1 A detailed treatment of the different aspects of electron broadening in hydrogen and hydrogenlike spectra using different approaches is given in [7.6,53--64].
280
7. Broadening of Spectral Lines
Here f( v) is the Maxwellian distribution function, the braces { } denote the averaging over directions of vectors p and v, and the notation (7.3.21 ) is used. We shall determine the S matrix using the perturbation theory expansion in series (7.2.24). The perturbation V(t) produced by collision with the electron has the form 2
V(t)
r·(p + vt)
= e (p2 + v2t 2)3/2 '
(7.3.22)
where r is the radius vector of an atomic electron. As already noted above in the case of the interaction V ex R- 2 , the principal role in the broadening is played by collisions with high values of p ~ Po, Where Po is the Weisskopf radius. This means that we can restrict ourselves to the first nonvanishing term in (7.2.24). After averaging (7.2.25) over all directions of the vectors p and v, we have (V v) = 0 and ,
[V(t)V(t )]
p2
r .r
+ v2tt'
= -3- (p2 + v2t2 )3/2(p2 + v2t,2 )3/2
(7.3.23)
.
Therefore
.(7.3.24) The first term of this expression is e4
p2
+ v2tt'
-L-L dtdt (p2 + v2t2)3/2(p2 + v2t'2)3/2 00
-"3 ra •rb
00,
2e4 =
1
-3 ra ·rb p2V2' (7.3.25)
The second and the third terms can be calculated as follows: ~IX"P"I
00
t
J Va(t)dt J Vit')dt' IIX'P'~ -00
(7.3.26)
-00
We shall introduce the dimensionless variables vt' vt Xl
=-,
P
X2= - .
P
(7.3.27)
7.3 Broadening of Lines of the Hydrogen Spectrum in a Plasma
281
Then (7.3.26) can be expressed in tenns of the integrals A(Z\,Z2) + iB(z\,Z2) 1 00 XI = 'LL dx'_L dX2 (1
1 + Xt X2 . + xf)3/2(l + xD3/2 exp [l(Z,Xt
- Z2 X2)] .
(7.3.28)
The summation over IX is restricted to the states of the level a. The perturbation due to all the other levels is neglected. The matrix elements 'alia are nonzero only for neighboring Stark components IX",IX. At IX" = 1X',Zt = Z2 = z, and at IX" :F IX', Zt = -Z2 = z. Let us denote the corresponding integrals by A+(z),B+(z) and A_(z),B_(z). All these integrals can be expressed in tenns of Bessel functions A±(z) = z2[Kf(z)±Kg(z)] B±(z)
= 21zlp j n
-00
~ {~lzlexp(-2Izl)
(z~
1),
(7.3.29)
(z~l),
A±(z') dz' ~ {~ (z~ 1), z2 - zl2 ' --+ 0 (z ~ 1).
(7.3.30)
For low values of p, the approximation (7.3.23) is not valid. The region of p < Po gives a comparatively small contribution to the broadening. Therefore it is possible to assume 00
J2npdp(1 - S;Sb) ~ np~
o
00
+ J2npdp(1
- S;Sb) .
~
The upper limit of integration must be taken as p = RD, see (7.3.16). It is not difficult to prove that for typical plasma parameters, the quantity Zmax = RDWall a/v, where Wall a is the Stark splitting in the field $0 = 2.6 ZeN 2/ 3 , can be neglected as compared to unity. Therefore one can assume A = 1 and B = 0 1• As a result (7.3.31 ) It must be noted that in some cases the upper limit of integration over p must be chosen not as RD but as v/Aw. The spectrum i(w) in the region of the frequencies Aw is determined by the correlation function lP('r) at T rv I/Aw. The impact approximation can be used only if the duration of the collision p/v > I/Aw, or p < Pm = v/Aw. Therefore the upper limit must be chosen as the minimum value of the two values RD,v/Aw. When integrating over v in (7.3.31) the lower limit of integration must be determined from the condition Po(vmin);:SRD • As a result we obtain the following
1 The same integrals are encountered in the problem of the broadening of nonhydrogenlike spectral lines in plasma (Sect. 7.4).
282
7. Broadening of Spectral Lines
expression for the operator tP:
Here (v-I) = 4/n(v) -I, and the constant 0.215 gives the relative contribution of the strong collisions P < Po. We shall determine the Weisskopf radius Po in accordance with that of Sect. 7.1 as
2
Po
2
e2)2
= 3 ( h(v)
,
2
(7.3.33 )
l(n,n )ao ,
l(n,n') = (2::IP"pI2)-1 lIP
2::
P"'p,Pp,, ~~Plra"ra
"p,,'P'
+ rb"rb -
2ra"rbl~' P' ~ao2 .
(7.3.34 )
where n and n' are the principal quantum numbers of the levels a and b. The intensity distribution in the wing of a line is given by (7.2.21) and (7.2.22), where in accordance with (7.3.32-34), the effective constant of the impact broadening ')' is
) , 332 N (v) -I mh 2 (RD In Po + 0.215 l(n,n), 2
')' =
(7.3.35)
The same quantity gives the order of magnitude of the broadening by electrons. The quantity l(n,n') can be written in the form l(n,n')
= len) + l(n') -
2K(n,n') .
(7.3.36)
As (ra"ra) ~ aijn 4 we have len) rv n4 and l(n') rv n,4. (For hydrogenlike ion with a nuclear charge !l'l(n) rv n4!l'-2 and l(n') rv n,4!l'-2). If n ~ n', then to an order of magnitude K(n,n') rv len), len'). For example, in the case of radiative transition n = 3 ---- n' = 2, we have len) = 56, len) + l(n') = 68, and l(n,n') = 27. In the case of the transition n = 4 ---- n' = 2, we have len) = 359 and l(n,n') = 291. Nevertheless using (7.3.36) for estimates of the broadening in the case of transitions between lower excited levels, one can assume I (n, n') ~ n4, where n is the maximum value of n,n', or l(n,n') ~ (n4 + n,4)/2. In the case of transitions between neighbouring highly excited levels n ~ 1, n' ~ 1, and In - n'l ~n,n', the term 2K(n,n') leads to a significant reduction of the broadening. This effect will be considered in Sect 7.3.6. In order to calculate the total intensity distribution produced by electrons for a given ion field, one must solve the system of equations (7.2.15). The Hamiltonian of an atom in the electric field being diagonal in parabolic coordinates, the calculation of the matrix tP must be carried out using parabolic atomic wave functions. The resulting effect of impact broadening by electrons in the presence of a fixed ion field can be described in the following way. The ion field splits the
7.3 Broadening of Lines of the Hydrogen Spectrum in a Plasma
283
line into the Stark components, each of these components being broadened by electrons. If the ion splitting is less than the impact broadening produced by the ,electrons B8;$ y, then the Stark components overlap. In this case, nondiagonal matrix elements of cP are of importance. But the main contribution to the line shape is given by the ion fields 8 rv 8 0 for which B80 > y. The transition from the impact distribution to the quasistatic wing produced by electrons in the case of a hydrogen .spectral line must be considered taking into account nonadiabatic effects. This problem is very complicated. For a discussion see [7.59-65]. 7.3.5
Combined Effect of Electrons and Ions
The intensity distribution resulting from the combined effect of electrons and ions can be obtained by calculating the electron broadening with a fixed ion field 8 and averaging the result over all possible values of 8. If the electron broadening is described by the Lorentzian distribution with width y from (7.3.35) and ion broadening in the same approximation as in (7.3.14), then for the normalized distribution of intensity it is easy to obtain [7.42] [(OJ) =
B~o T(OJB-8: B~J 0
,
.
(7.3.37)
The function T(x, y) is defined by the expression
y
T(x, y) =
TH(x')dx'
211/ (x _ x')2 + (y/2)2 .
Values of the function log T(x,y) are given in Table 7.3. When y
(7.3.38) -+
O,T(x,y)-+
TH(X).
In the line wing (high values of x), T(x,y)
~ 1.5
X- 5/ 2
+ ,Jnx-2 .
(7.3.39)
In order to improve the description of a line shape one must take into consideration two effects: (i) in the far wing of a line impact distribution is replaced by quasistatic one; and (ii) in the central part of a line, ion broadening must be calculated taking into consideration the thermal motion of ions; moreover the distribution function Wo(8) instead of WH(8) must be used (see Fig. 7.5). Detailed calculations of the hydrogen line shapes have been carried out in [7.66-69]. The results of these calculations are in many cases in a reasonable agreement with the experimental data [7.70-73]. The difference between experiment and calculations is, however, noticeable in the central part of the lines, especially for the lines having an unshifted Stark component (L(h Hat). When plasma density is not high the discrepancy of experimental [7.74,75] and theoretical linewidths for Lat and Hat can exceed a factor of 2, see also [7.48]. In
284
7. Broadening of Spectral Lines
Table 7.3. log T(x,y) x y
0
0.5
0.0 0.5 1.0 1.5 2.0 3.0 4.0 5.0
i.004 2.963 2.912 2.874 2.837 2.768 2.706 2.651
i.ooo 2.958 2.911 2.872 2.834 2.766 2.704 2.649
2.992 2.943 2.905 2.864 2.826 2.759 2.699 2.646
2
3
5
7
10
15
20
2.936 2.912 2.862 2.826 2.794 2.734 2.678 2.628
2.846 2.828 2.794 2.768 2.742 2.692 2.645 2.600
2.251 2.579 2.588 2.592 2.588 2.570 2.545 2.518
2.292 2.313 2.356 2.385 2.402 2.415 2.417 2.410
3.860 3.975 2.050 2.092 2.123 2.175 2.208 2.228
3.370 3.455 3.580 3.666 3.729 3.822 3.888 3.938
4.996 3.159 3.252 3.354 3.434 3.550 3.633 3.698
case of hydrogenlike ions the accuracy of methods used in [7.66-68] can even be poorer for such lines [7.51]. As noted above (Sect. 7.3.3) the dynamic effects of the ion must be taken into account.
7.3.6
New Approaches to the Theory of Stark Broadening
The new, very promising approaches to the problem of spectral line broadening by charged particles have been given in [7.47-52,76-79]. In [7.76,77] the study of Stark profiles for hydrogen lines is carried out by means of direct computer simulation. The radiating atom is assumed to be placed in some volume together with a fixed number of charged particles, electrons and ions, the motion of which is described by classical orbits. Numerical solution of the Schrodinger equation for a radiating atom perturbed by Debye-screened fields of charged particles is averaged over the initial coordinates and the velocities of the perturbers. The Stark profiles are obtained as a result of such a procedure. A new version of relaxation theory proposed in [7.47, 48] showed good agreement with experiment and with the results of computer simulation [7.76, 77]. In the so called "Model Microfield Method" proposed in [7.78, 79] the intensity distribution of a spectral line is expressed in terms of a correlation function for the plasma microfield. This method proved to be very successful in taking into account the "ion-radiator dynamic effects" [7.49-52], and also showed good agreement with experiment and with the results of computer simulation. The above-mentioned theoretical methods can be applied to the nonhydrogenic spectra, too.
7.3.7 Highly Excited States The reduction of electron broadening due to the term K(n,n') in (7.3.36) is connected with the interference effects discussed in Sect. 7.2.
7.3 Broadening of Lines of the Hydrogen Spectrum in a Plasma In the case of high n and n' = n -I the matrix elements for large values of [ are almost the same:
Snl,nl±l
and
285
Snll,nll±1
Snl,nl±l - Snll,nll±1 ~ Snl,nl±l .
Moreover the matrix elements P nl, n' I± I and Pni', n' I' ± h where [' = [± I, are also almost the same. Therefore there arises a very close similarity with the four-level system considered in Sect. 7.2.6. It can be shown [7.6, 80, 81] that in the case of radiative transitions between neighboring highly excited levels, n ~ I, n' ~ I, and
In - n'l ~n,n', J(n,n')~ J(n),l(n') .
Thus for transitions n - n - I, n ~ I we have J(n,n - I)
rv
I "2J(n) . n
(7.3.40)
According to (7.3.40) for such transitions the dependence Ye ex: n4 is replaced by the dependence Ye ex: n2 • This means that one cannot neglect the perturbation due to the all other atomic levels. As a result the broadening due to the quadratic stark effect as in the case of nonbydrogenlike spectra begins to be of importance. Broadening of this kind is considered in Sect. 7.4. As a rule the lines corresponding to radiative transitions between highly excited levels are observed in plasmas with very low electron density, when he ~ 1 and hi ~ I. Expression for the width of a line n - n' is given by Y = Ye + Yi, Ye = Ne[(vO'e(n)} Yi = M[(vO'i(n)}
+ (vO'e(n'»)] ,
(7.3.41 )
+ (vO'i(n'»)] ,
where O'(n) = L:1kl>oO'(n, n + k) are the effective cross sections of inelastic scattering. Using the quasi-classical calculations of cross sections for highly excited level described in Sect. 3.5, one can write for the quantity (vO'(n)} the following approximate formula: (vO'e(n)}
~
4
10- 8 z3~1/2 CP(x) f( 8) [cm3 s- I ],
(7.3.42)
where 8 = T/~Ry,
x = En/T = l/n2 8 , CP(x) = 2.18{0, 82q>(x) + 1.47[1 - xq>(x)]}, 1 + 1.4yx ] q>(x) = -exp(x)Ei( -x) ~ In [ 1 + y.x.(l + 1.4x) ,
f(8) = In
[1 + z(1 +nvle vie ]1n(1 + nvle/z) 2.5/z 8)
(7.3.43) Y = 1.78
(7.3.44)
7. Broadening of Spectral Lines
286
when z -+ 00 or 8 -+ 00,/(8) -+ 1. If perturbing particles are protons, the temperature T in (7.3.42-44) should be replaced by the quantity Tm/M, where m is the mass of electron and M is the reduced mass of the colliding particles. Stark broadening of the lines in the far-infrared solar spectrum corresponding to the transitions between highly excited hydrogenlike states is of interest for diagnosing the structure of the solar atomosphere [7.82].
7.4 Line Broadening of Nonhydrogenlike Spectra in a Plasma 7.4.1
Preliminary Estimates
The spectral lines of nonhydrogenlike atoms in the presence of a constant and homogeneous electric field undergo a shift and also a splitting proportional to @"2-the quadratic Stark effect. We shall assume that the field @" = QR- 2 , produced by a charge Q, varies little for atomic dimensions (this is valid for sufficiently large values of R). Then in (7.1.20) for the shift of oscillator frequency, n = 4 and K = C4R- 4 . The constant C4 for a transition n -+ k is defined as C4
= (C4 )n -
(C4 )k; (C4 )n
= Q2/h 2: 1(~~nmI2 m
,
nm
where (Dz )nm are the matrix elements of the z component of the electric dipole operator, .1Enm = En - Em (see [1.1]). The parameters he (electron broadening) and hI (ion broadening) are he = N
(~ C4) 2
, hi = N
Ve
(~ C4 ) 2
.
(7.4.1 )
Vi
The quadratic Stark-effect constants C4, as a rule, have the order of magnitude 10- 12 -10- 15 cm4 s-I, although values of C4 < 10- 15 and C4 '" 10- 11 - 10- 10 are also encountered. For C4 = 10- 12 - 1O- IS,ve = 5.107 cm s-I and Vi = 2.105cm S-I, we have he = 3.(10- 19 - 1O- 22 )N, hi = 0.75(10- 17 - 1O- 2o )N. At not very high values of the density of charged particles N < 1015 cm -3, he ~ I, and hi ~ 1. This means that both electrons and ions produce impact broadening. According to (7.1.23) Y4,.1 4 ex: vl / 3. Thus electrons play the principal role in the broadening of a line. The interaction with ions only slightly increases the impact width and shift of a line, by approximately 15-20%, because (Ve/Vi)I/3 ~ (M/m )1/6 ~ 5-6. Since K ex: Q2 the sign of the shift of a line is the same for electrons and for ions.
7.4.2 Electron Broadening We shall describe electron broadening of lines of a nonhydrogenlike atom in the framework of quasi-classical theory discussed in Sect. 7.2. In the case of the
7.4 Line Broadening of Nonhydrogenlike Spectra in a Plasma
287
isolated spectral line the spectrum I (w) is described by Lorentzian distribution (7.2.17). The width and shift are given by (7.2.18) and (7.2.20). The elements of the S matrix averaged over M components of atomic levels must be substituted in these equations. As a rule the main contribution to the broadening is given by collisions with relatively large values of the impact parameter p. Therefore in calculating the S matrix we can restrict ourselves to the first terms of the expansion in powers of rand 1'/. Therefore one can average over M directly the quantities r and 1'/. In the case of the dipole interaction between a neutral atom and a charged particle V = -d·iff the linear term in (7.2.25) for the S matrix S(v), being averaged over M (or over directions of the vectors p and v), is equal to zero. Only the next term containing C\(t) C\( (I) in the integrand is nonvanishing. We shall assume now that the perturbation of one of the levels (initial or final) can be neglected. Then for the radiative transition n-k, assuming that the level k is not perturbed, we can obtain (7.4.2)
r
= ~'rs = ~'2 s
s
(.!!...)2 (Ins Ry ) ~A (W ns P ) mv JEns P
.
(7.4.3 )
V
Here JEns = Es - En, Ins is the oscillator strength of the transition n -+ s (see [Ref. 1.1, Sect. 9.2]), and the sum over s extends over all atomic levels, for which Ins =I O. The functions A and B coincid~ with the functions A+ and B+ defined by (7.3.29, 30). Values of the functions A and B are given in Table 7.4. As a rule the principal contribution to (7.4.2,3) is provided by the nearest perturbing levels and, in some cases, by only one of them. In the approximation of one perturbing level, y
= 2N (v)(J~( (v))J' (f3)
,
(7.4.4 )
J
= N(v)(J~( (v) )J"(f3) ,
(7.4.5)
Table 7.4. Functions A(z) and B(z). z
A(z)
B(z)
0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6
1.000 1.035 0.962 0.829 0.680 0.540 0.418 0.318 0.239
0.000 0.160 0.359 0.498 0.576 0.606 0.603 0.580 0.546
z
A(z)
B(z)
1.8 2.0 2.4 2.8 3.2 3.6 4.0 5.0
0.177 0.130 0.0688 0.0355 0.0181 0.0090 0.0045 0.00075 nze- 2z
0.507 0.467 0.393 0.331 0.283 0.245 0.216 0.166 n/4z
~oo
7. Broadening of Spectral Lines
288
where (J~ and (J~ are the width and shift cross sections defined by (7.1.13,14),
(J~ = (~r/3 r (~ ) C~/3 (v) -2/3 ':::!. 5.7C~/3 (v) -2/3 , (7.4.6)
(v) is the mean value of the electron velocity, and the constant C4 is defined as C 4
= 2t?a~f(Ry)2
ft
,1E
The functions J'(P) and J"(P) depend on the dimensionless parameter
P =lfRyll/2 I,1EI2 . ,1E m(v) As
P---- 00, J', J"
(7.4.7 )
---- 0.97. This case corresponds to adiabatic perturbation when
r = 0, and the broadening is determined by the phase shift '1.
For
P~ 1, on the
contrary, inelastic collisions play the main role. In this case,
,
Ry
(v(J ) = 4nf ,1E (v
(ft) 2In (mv2 1 Ry 11/2) ) , mv 21,1EI f ,1E
(7.4.8)
(7.4.9) The results of numerical calculations of the functions J'(P) and J"(P) are given in Table 7.5. We shall now consider to what extent the results obtained above can be generalized to the case of several perturbing levels. This problem obviously arises
Table 7.5. Factors J'(fJ) andJ"(fJ).
fJ
J'
J"
64 32 16 8 4 2 I 0.5 0.25 0.125 0.625 x 10- 1 0.312 x 10- 1
0.97 0.97 1.02 1.03 1.06 1.12 1.17 1.20 1.15 1.09 0.927 0.764
0.97 0.97 0.97 0.96 0.94 0.90 0.861 0.746 0.604 0.455 0.326 0.223
fJ 0.156 0.78 0.39 0.195 0.97 0.48 0.24 0.12 0.61 0.305 0.15
xlO 1 X 10- 2 X 10- 2 x 10- 2 x10- 3 X 10- 3 X 10- 3 X 10- 3 x 10- 4 x 10- 4 X 10- 4
J'
J"
0.594 0.451 0.334 0.239 0.171 0.119 0.0824 0.056 0.038 0.024 0.017
0.151 0.094 0.063 0.0405 0.0245 0.0167 0.0103 0.0065 0.004 0.0026 0.0016
7.5 Broadening by Uncharged Particles
289
only in the case when, for one or several perturbing levels, the parameter P is of the order of or less than unity. If P~ 1 for all perturbing levels, then the perturbation is adiabatic and y and LI are expressed by means of (7.1.23) in terms of the quadratic Stark effect constant C4 for a given line. The magnitude of this constant is determined by the total perturbing effect of all atomic levels. If for the nearest perturbing levels which give the principal contribution to '1 and r in (7.4.2,3), the parameters P~ 1, then the width y can be obtained by summing (7.4.4):
y = 2N(v)LI(J~S«V))J/(PS)'
(7.4.10)
Such an approximation is valid because in this case the broadening is caused by inelastic collisions, and the partial widths corresponding to different collisional transitions are additive. The shift of a line cannot be calculated by summing (7.4.5) even if for all perturbing levels Ps ~ 1. In the general case when both levels nand k (initial and final) are perturbed, r
= rn + rk,
'1
= '1n - 17k,
where r n, rk, '1n and 17k must be calculated by means of (7.4.2, 3). An extensive bibliography on numerical calculations of shapes of the nonhydrogenlike spectral lines in plasma can be found in [7.6]. Results of numerical calculations of widths and shifts for a large number of nonhydrogenlike spectral lines of different atoms and ions also are given in [7.6]. The experimental data on Stark broadening in nonhydrogenlike spectra may be found in [7.12.13]. The very accurate experimental data on the lines of neutral He are given in [7.83].
7.5
Broadening by Uncharged Particles
7.5.1
Perturbation by Foreign Gas Atoms (Van der Waals Interaction)
The interaction of neutral atoms at large distances has the form V(R) ex: R- 6
.
Therefore usually one assumes K
= C6R-6.
(7.5.1 )
The crude estimate of the constant C6 is given by C6 ~
e2(r2)IX.
- f j , - ' IX. ~
4
(Ry)2 ao (rp)2,
"3 m T
(7.5.2)
where (r2) ~ 5n*4a~/2 is the mean value of r2 for the excited state of the
290
7. Broadening of Spectral Lines
radiative atom, (r~) is that for the perturber, n* is the effective principal quantum number, IX is the polarizability of the perturbing atom, I is its ionization potential, and m is the number of equivalent electrons. The constant C6 has the order of magnitude 10- 30 n*4. Thus for v rv 105 cm s-I, we have h = (387t
~6 )
3/5
N
~ 10- 21 N
.
(7.5.3 )
This indicates that at not very high pressures, of the order of few atmospheres or less, line broadening can be described in the impact approximation. We shall also compare the quantities Q = V6/5C;:I/5 and Awo. As Q ~ 10 12 S-I and Awo ~ IO IO s- l , we have Q~Awo. Consequently the region of impact broadening extends far beyond the limits of the Doppler width. In accordance with (7.1.23) the width and shift of a line can be estimated using the relations (7.5.4 ) The typical values of yare y rv 10- 8N. In order to treat impact broadening by uncharged particles more accurately it is necessary to take into consideration that at small distances the interaction VCR) has a more complicated form than VCR) ex R- 6 . Depending on the type and states of interacting atoms both attraction and repulsion can take place at large distances R. At small distances the potential VCR) is repulsive. In some cases atom and perturber can form a quasi-stable molecule. Moreover in the general case, the interaction V is dependent not only of R but also of the angular variables. The results of calculations in which a more realistic interaction than V(R) ex R- 6 is used cannot be described by a simple Lorentzian distribution with width and shift as in (7.5.4). In particular, the intensity distribution depends on the type of the transition j-j'. A detailed treatment of the foreign gas broadening is given in [7.4,10,11,1414-16]. The repulsive part of the interaction is usually taken into account in the form of the Lennard-Jones potential V(R) = CI2R-12_C6R-6. The line shift A and the ratio ylA are especially sensitive to the form of the potential VCR). Experimental data on line broadening in the spectra of alkali atoms obtained at low values of foreign gas pressure, less than 10 atm, are in qualitative agreement with the impact theory. The broadening and shift of the lines are proportional to the concentration of perturbing particles. For the initial members of a principal series perturbed by different foreign atoms (He, Ne, Ar, Kr, Xe, H2, N2, and so on), as a rule, a red shift is observed, the ratio ylA being close to 2.8. In some cases (usually for the higher members of a principal series), a blue shift instead of a red one is observed. The sign of the shift of one and the same line can be different for different perturbing particles. The dimensionless parameter h reaches values of order unity only when N > 1021 , i.e., at pressures of about tens of atmospheres. In this case the mean distance between atoms has the same order of magnitude as atomic dimensions and consequently the simplest expression VCR) ex R- 6 is not valid. The experi-
7.5 Broadening by Uncharged Particles
291
mental data on line shapes are usually used to obtain information about the form of potential V(R) at small distances. Specific features of molecular-lines broadening have been described in [7.4,
8,9]. 7.5.2
Self-Broadening
We shall consider now the single-component gas. With an increase of density of such a gas, resonance lines broaden considerably more than on the addition of a foreign gas. This is due to the fact that in the case of collision of two identical atoms, one of which is excited, a resonance transfer of the excitation energy is possible, the effective cross sections of such collisions being extremely large. They can exceed considerably (by several orders) the gas kinetic cross sections. The effective cross sections of resonance energy transfer (J were calculated in Sect. 4.2. For electric dipole transition, the energy transfer is caused by the dipole-dipole interaction V ex: R- 3 • The cross section (J and corresponding line width yare of the order of magnitude
e2 y'" -IN,
mwo
(7.5.5)
where S is the line strength and I is the oscillator strength. Assuming that I ~ 1 and Wo ~ lOIS, we have y 1O- 7N. In the case of foreign-gas broadening, typical values of widths are y rv (l0-9-10-8)N. The effective cross section of energy transfer can be relatively large not only under conditions of exact resonance but also in the case of a collision of two atoms with close energy levels. Thus, when calculating the width of the component 2P1/2-2S1/2 of the resonance doublet of an alkali atom, it is necessary to take into account not only energy transfer 2P I /2 -+2 SI/2 (radiating atom), 2S1/2 -+2P 1/2 (perturbing atom), but also the excitation 2S1/2 -+2P3/2 of the perturbing atom. The cross section of the energy transfer 2P I /2 -+2S1/2 , 2S1/2 -+2P3/2 has the same order of magnitude as the cross section of the resonance energy transfer 2P I/2 -+~\/2' 2SI/2 -+P3/2, if the following condition is fulfilled (Sect. 4.2): <'V
(
e2
-2-1 mwo
) 2/3
(LJE) 4/3 --;:n
1 2«1, V
where LJE is the doublet splitting. Of all alkali atoms, only Li atom satisfies this condition. In the case of Li the doublet splitting of the resonance level is 0.34 cm- I . In order to calculate the line broadening due to resonance energy transfer more accurately it is necessary to take into consideration the degeneracy of levels and dependence of the interaction on the angular variables. Such calculations using the impact approximation have been carried out by many researchers [7.84--89].
292
7. Broadening of Spectral Lines
The summary of the results can be given as follows (7.5.6) where Jo and J 1 are the angular momenta of the ground and excited levels, respectively, and 101 is the line oscillator strength. The values of the factor A(JoJI) for isolated lines calculated numerically in [7.87,88] are given in Table 7.6 together with the ratios of the width y/2 to the shift A from [7.89]. As was said above, in the special case of Li atom one has to take into consideration the perturbation of both excited levels 2PI/2 and 2P3/2. Because of that one can expect almost equal widths for both lines of the resonance doublet. The approximate value of y/2 in this case can be obtained using (7.5.6) and assuming Jo = 0, JI = 1 [7.85]. For the case of interaction V ex R- 3 the intensity distribution in quasistatic wings lco-cool 't> V3/2C:;I/2 = V3/2(t? l/mcoO)-1/2 is also proportional to (CO-COO)-2 as in the impact approximation. However, the intensity /(co) in the quasistatic wings is somewhat different from that in the impact approximation [7.84,85,90] /(co)
= a (JoJd
2nt? 1 -lOIN ( )2 . mcoo co-coo
(7.5.7)
The factors a(JoJd are also given in Table 7.6. In the case of Li resonance doublet Jo = 0, JI = 1 should be assumed in (7.5.7). The calculations taking into account the accurate adiabatic potential curves [7.90] show a slight asymmetry of blue and red wings. The direct experimental studies of the resonance broadening as a rule encounter very serious difficulty connected with extremely large optical depth in the center of the lines [7.91]. The lines corresponding to transitions between the resonance level and other excited levels also undergo broadening due to the resonance interaction. The resonance contribution to the widths y of such lines can be evaluated to be equal to the linewidth of the resonance line.
TabIe7.6. Parameters describing the resonance broadening Jo
0
112
112
1
JI
1
112
3/2
1
1.042
0.903
1.039
0.092
-0.031
0.050
0.698
1.047
0.805
A(JoJl)
2
Aly
a (JoJl)
0.983 -0.01
7.6 Spectroscopic Methods oflnvestigating Elastic Scattering of Slow Electrons
293
7.6 Spectroscopic Methods of Investigating Elastic Scattering of Slow Electrons 7.6.1 Perturbation of Highly Excited States The broadening of a line corresponding to a transition between the ground state and a state with a large value of the principal quantum number n is completely determined by the perturbation of the upper level. For sufficiently large values of n, the mean distance of the valence electron from the nucleus rv aon2 is so large that the neutral perturbing particle either interacts with the electron and does not interact with the atomic core, or interacts only with the atomic core. In this case, the broadening is caused by the scattering of the atomic electron by the perturbing particles and by the scattering of the perturbing particles by the atomic core. These two mechanisms of the broadening are statistically independent. We shall first consider the interactions of the first type. If only one level is perturbed, then in accordance with (7.2.39) we have
2n
(I'
= kIm {/(O)},
2n
(I"
= -k Re {/(O)}
,
(7.6.1)
where 1(0) is the amplitude of forward scattering of the perturbing particle by the atom, and hk is the momentum of the perturbing particle (we assume for simplicity that the mass of the atom is large as compared with the mass of the perturbing particle). If aon2~Peff. ~ (nlX/4)1/3(e'2/hve)I/3, where Peff. is the effective radius of the interaction between the electron and the perturbing particle and IX is the polarizability of the perturbing particle, then in the volume of interaction the field produced by the atomic core and consequently the electron velocity Ve are practically constant. In the state with principal quantum number n, Ve is of the order of magnitude vo/n, where Vo is the atomic unit of velocity. If the velocity of the perturbing particle vp = hk/M is less than Ve rv vo/n, then the scattering amplitude 1(0) in (7.6.1) can be expressed in terms of forward scattering amplitude 1;(0) of a free electron with momentum hq by the perturbing particle [7.92] for the derivation of this, and subsequent formulas of this section):
1(0) = M
m
J I G(nlmlq)1 2/;(0)dq.
(7.6.2)
Here m is the electron mass, and G(nlmlq) are the coefficients of the expansion of the atomic function I/!nlm in plane waves: (7.6.3) States with large values of the principal quantum number n are hydrogenlike. It is therefore possible to use as the expansion coefficients G(nlmlq) the well-known expressions for hydrogen functions in the momentum. representation in terms of Gegenbauer polynomials [7.93].
294
7. Broadening of Spectral Lines
By substituting (7.6.2) in (7.6.1), integrating over the angular variables, and averaging over all possible orientations of the perturbing particle angular momentum, we have
41t1i Y = N-;;- dq W(q) 1m {Jq(O)} ,
(7.6.4)
21t1i A = -N -;;- dq W(q)Re {fq(O)} ,
(7.6.5)
= q2 IGn,(qW, J W(q)dq = 1 .
(7.6.6)
J
J
W(q)
As already noted above these formulas describe the width and shift caused by scattering of the atomic electron in the highly excited state by perturbing particle if the following conditions are fulfilled: (7.6.7) (7.6.8) We shall now consider interaction of perturbing particle with the atomic core. As the charge of the atomic core is e, this interaction has the form (7.6.9) It produces the polarization of the perturbing particles by the atomic core and leads to a shift of the frequency of the atomic oscillator, IX 2 1 K(t) = - 21i e [R(t)]4 .
(7.6.10)
Broadening due to interactions of this type was examined in Sect. 7.4.- If
hi=PfN~l'Pi=C:)
1/3 (
~
) 1/3
livp
,
(7.6.11)
where N and vp are the density and velocity of the perturbing particles, then the central part of the line lro-rool ~D = (2Iiv:/lXe 2 )1/3 is described by the Lorentzian distribution with width l' and shift A' given by the following formulas: ~
y'= 114 . (~) 21i
2/3
;;:;
1/3N. Vp '
A' = _~ 2 Y, .
LJ
(7.6.12)
It can be shown that when hi ~ 1, the corresponding quasi-static distribution has width of the order of lON4/ 3 ~ Iii. The case hi ~ 1 corresponding to pressures of the order of or less than an atmosphere is the most interesting. In this case, one can calculate l' and A' with sufficiently good accuracy. Subtracting the cal-
7.6 Spectroscopic Methods ofInvestigating Elastic Scattering of Slow Electrons
295
culated values y' and ,1' from experimental values of the width and shift, one can determine y and ,1 from (7.6.4,5). Expressing in these equations the amplitude 1;(0) in terms of the phase of scattering of the electron by the perturbing particle 111, we also have
N~m J
y=
,1
=
[4n E(21 + l)sin2111] W(q)dq q 1
-N -h J m
= N~ Jqa(q) W(q)dq, m
[n- E(21 + l)sm2111 . ] W(q)dq. q
(7.6.13)
(7.6.l4)
1
Here a( q) is the effective cross section for elastic scattering of the electron with momentum hq by the perturber. If exchange interaction is also taken into account, then the following substitution must be made in (7.6.l3, 14): (7.6.l5) sin 2111 -+ C+ sin 211~ +)
+ c- sin 211~ -) ,
(7.6.l6)
where 11~ +) and 11~ -) are the scattering phases calculated taking exchange into account for states of the system perturbing particle plus electron with given value of the total spin S = Sp ± Ij2,Sp being the spin of the perturbing particle; and C+
=
Sp
+ 1,
C-
2Sp +1
=
(7.6.l7)
Sp
2Sp +1
We shall now consider the resonance transitions no atoms. For np state [7.93] W(q) = 2
(~2
n n - 1
) (_1_)2 [(n nqao
-(n - l)sin(n
+ l)sin(n -
+ l)qJ]2 ao ,
s-np(n~
1) of the alkali
l)qJ
(7.6.l8) (7.6.19)
The function W(q) has n peaks, nj2 peaks being located in the range 0 < q < Ijnao. In this range, the envelope behaves approximately as (1 + n2q2a~)-2. For q~ 1jnao, the function W(q) decreases monotonically: 27 (n 2
W(q)C::'3
1 )n3
_
n
(
1 ) 8 -. nqao
(7.6.20)
Thus the principal contribution to the integral over q in (7.6.13, 14) is given by the range 0 < q < Ijnao.
296
7. Broadening of Spectral Lines
If n is so large that the principal contribution to the sum with respect to 1 is given by the term 1 = 0 (s scattering) and in addition q-l sin 21'/1 differs little from its limiting value
1. (1. ) 1m
q-+O
- sm 21'/1 q
=
-I1'1'//-I00 ~ -0"(0) , n
(7.6.21 )
then
fL t=:7i\\. 1'/0
.1 = -;,;;vna(O)i%TN.
(7.6.22)
Here a(O) is the limiting expression for the elastic scattering cross section at q - t O. By 1'/0 is understood that part of the phase which after subtraction of pn where p is integer, lies in the interval -nI2, n12. Since as q - t 0, qa(q) - t 0, in the range of applicability of (7.6.22), Y~I.1I. Some additional effects of broadening are discussed in [7.94-96]. Experimental data on broadening of Rydberg levels can be found in [7.97-100].
7.6.2 Fermi Formula Equation (7.6.22) has been obtained by Fermi [7.4]. In accordance with this equation it is possible using the experimental value of .1 to determine the elastic scattering cross section for extremely slow electrons (in the limit q - t 0). Thus the cross section a(O) for the atoms He, Ne, Ar, Kr, and Xe have been found by the shift of the absorption lines of Cs in an atmosphere of noble gases. Some other gases have also been investigated by the same method (see [7.4] and also [7.101]). The Fermi method enables one to obtain information on elastic scattering of electrons at very small energies, i.e., in the range most difficult to investigate by other experimental methods. It must be noted that shift .1 is sensitive not only to the magnitude but also to the sign of the phase 1'/0. In the general case, when several terms of the sum over 1 contribute to y and .1, it is not possible to determine the scattering phases from known values of y and .1. Knowledge of these quantities, however, enables one to control the quality of approximate calculations of the scattering phases [7.102, 103].
References
Chapter 1 1.1 1.2
1.1. Sobel'man: Atomic Spectra and Radiative Transitions, 2nd edn., Springer Ser. Atoms Plasmas, VoU2 (Springer, Berlin, Heidelberg 1992); 1st edn., Springer Ser. Chern. Phys., VoU (Springer, Berlin, Heidelberg 1979) M. Venugopalan (ed.): Reactions under Plasma Conditions (Wiley-Interscience, New York 1971) VoU
Chapter 2 N.F. Mott, H.S.F. Massey: The Theory of Atomic Collisions (Pergamon, Oxford 1965) 2.2 M.L. Goldberger, K.M. Watson: Collision Theory (Wiley, New York 1964) 2.3 ChJ. Joachain: Quantum Collision Theory (North-Holland, Amsterdam 1975) 2.4 M.R.H. Rudge: Rev. Mod. Phys. 40, 564 (1968) 2.5 R.P. Peterkop: Teoriya Ionizatsii Atomov Elektronnym Udarom (Theory of Ionization Atoms by Electron Impact, in Russian) (Zinatne, Riga 1975) 2.6 1.1. Sobel/man: Atomic Spectra and Radiative Transitions, 2nd edn., Springer Ser. Atoms Plasmas, Vol.12 (Springer, Berlin, Heidelberg 1992); 1st edn., Springer Ser. Chern. Phys., VoU (Springer, Berlin, Heidelberg 1979) 2.7 L.A. Vainshtein, 1.1. Sobel'man: Zh. Eksp. Teor. Fiz. 39, 767 (1960) 2.8 M.J. Seaton: Proc. Phys. Soc. 77, 184 (1961) 2.9 MJ. Seaton: Adv. Atom. Molec. Phys. 11,83 (1975) 2.10 H.S.W. Massey, E.H.S. Burhop, H.B. Gilbody: Electronic and Ionic Impact Phenomena VoU (Clarendon, Oxford 1969) 2.11 R. Courant, D. Hilbert: Methoden der Mathematischen Physik (Springer, Berlin 1931) VoU 2.12 L.A. Vainshtein: Phys. Scripta 33,336 (1986) 2.1
Chapter 3 3.1 3.2 3.3 3.4
3.5 3.6
L.A. Vainshtein, 1.1. Sobel/man: Zh. Eksp. Teor. Fiz. 39, 767 (1960) B.L. Moiseiwitsch: Rep. Prog. Phys. 40,843 (1977) K. Smith: The Calculation of Atomic Collision Processes (Wiley-Interscience, New York 1971) 1.1. Sobel'man: Atomic Spectra and Radiative Transitions, 2nd edn., Springer Ser. Atoms Plasmas, Vol.12 (Springer, Berlin, Heidelberg 1992); 1st edn., Springer Ser. Chern. Phys., VoU (Springer, Berlin, Heidelberg 1979) M. Inokuti: Rev. Mod. Phys. 43, 297 (1971) K. Omidvar: Phys. Rev. 188, 140 (1969)
298
3.7 3.8 3.9 3.10 3.11 3.12 3.13 3.14 3.15 3.16 3.17 3.18 3.l9 3.20 3.21 3.22 3.23 3.24 3.25 3.26 3.27
3.28 3.29 3.30 3.31 3.32 3.33 3.34 3.35 3.36 3.37 3.38 3.39 3.40
References
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Chapter 4 4.1 4.2 4.3 4.4 4.5 4.6 4.7 4.8 4.9 4.10 4.11 4.12 4.13 4.14
4.15 4.16 4.17 4.18 4.19 4.20
4.21 4.22 4.23 4.24 4.25 4.26 4.27 4.28 4.29 4.30 4.31 4.32 4.33
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Chapter 5 5.1 5.2 5.3 5.4
5.5 5.6 5.7 5.8 5.9 5.10 5.11 5.12 5.13 5.14 5.15
5.16 5.17 5.18 5.19 5.20 5.21 5.22
1.1. Sobel 'man: Atomic Spectra and Radiative Transitions, 2nd edn., Springer Ser. Atoms Plasmas, VoU2 (Springer, Berlin, Heidelberg 1992); 1st edn., Springer Ser. Chern. Phys., VoU (Springer, Berlin, Heidelberg 1919) I.L. Beigman: Zh. Eksp. Teor. Fiz. 131729 (1917) [English trans!': SOy. Phys.JETP 46, 908 (1977)] H. Van Regemorter: Astrophys. J. 132,906 (1962) H.W. Drawin: Rep. EUP-CEA-FC-383 Assoc. EURATOM-CEA (1967) Fontenay-aux-Roses, France; ibid: in Plasma Diagnostics, ed. by W. Lochte-Holtgreyen (North-Holland, Amsterdam 1968) R. Mewe: Astron. Astrophys. 20, 215 (1972) M. Gryzinski: Phys. Rev. 115, 374 (1959) M. Gryzinski: Phys. Rev. A 138, 305,322,336 (1965) V.P. Shevelko, E.A. Yukov: Phys. Scripta 31,265 (1985) M.J. Seaton: Planet Space Sci. 12,55 (1964) W. Lotz: Z. Physik 232, 101 (1970) R.C. Stabler: Phys. Rev. A 133, 1268 (1964) A. Burgess: Astrophys. J. 139, 776 (1964) B. Shore: Rev. Mod. Phys. 39,439 (1967) E. Trefftz: J. Phys. Atom. Molec. Phys. B 3, 763 (1970) M.I. Seaton, P.J. Storey: Dielectronic Recombination, in Atomic Processes and Applications, ed. by P.G. Burke, B. Moiseiwitsch (North-Holland, Amsterdam 1976) A. Burgess, M.I. Seaton: Mon. Not. Roy. Astron. Soc. 125, 355 (1964) A. Burgess, H.P. Summers: Astrophys. J. 151, 1007 (1969) A. Gabriel, T.M. Paget: J. Phys. Atom. Molec. Phys. B 5,673 (1972) Yu.I. Grineva, V.I. Karev, V.V. Koreneev, V.V. Krutov, S.L. Mandelshtam, L.A. Vainshtein, B.N. Vasilyev, I.A. Zhitnik: Solar Phys. 23, 441 (1973) L.M. Biberman, V.S. Vorobyov, N.T. Yakubov: Usp. Fiz. Nauk 101, 353 (1972) [English trans!.: SOy. Phys.Usp. 15,375 (1972)] H. Griem: Plasma Spectroscopy (McGraw-Hill, New York 1964) R.H. Huddlestone, S.L. Leonard (eds.): Plasma Diagnostics Techniques (Academic, New York 1965)
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6.3 6.4
L.A. Vainshtein: Trudy FIAN 15, 3 (1961) 1.1. Sobel/man: Atomic Spectra and Radiative Transitions, 2nd edn., Springer Ser. Atoms Plasmas, VoLl2 (Springer, Berlin, Heidelberg 1992); 1st edn., Springer Ser. Chern. Phys., VoLl (Springer, Berlin, Heidelberg 1979) D.A. Varshalovich, A.N. Moskalyv, V.K. Khersonske: Quantum Theory of Angular Moment (World Scientific, Singapore 1988) A.R. Edmonds: Angular Momentum in Quantum Mechanics (Princeton Press, Princeton, NJ 1957)
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Chapter 7
7.1 7.2 7.3 7.4 7.5 7.6 7.7 7.8 7.9 7.10 7.11 7.12 7.13 7.14 7.15 7.16 7.17 7.18 7.19
7.20 7.21 7.22 7.23 7.24 7.25 7.26 7.27 7.28
R.G. Breene Jr.: The Shift and Shape of Spectral Lines (Pergamon, New York 1961) M. Baranger: In Atomic and Molecular Processes, ed. by D.R. Bates (Academic, New York 1962) G. Traving: In Plasma Diagnostics, ed. by W. Lochte-Holtgreven (NorthHolland, Amsterdam 1968) S. Chen, M. Takeo: Rev. Mod. Phys. 29, 20 (1957) H.R. Griem: Plasma Spectroscopy (McGraw-Hill, New York 1964) H.R. Griem: Spectral Line Broadening by Plasmas (Academic, New York 1974) J. Cooper: Rev. Mod. Phys. 39,167 (1967) C.J. Tsao, B. Curnutte: J. Quant. Spectrosc. Radiat. Transf. 2, 41 (1962) H. Rabitz: Ann. Rev. Phys. Chern. 25, 155 (1974) W.R. Hindmarsh, J.M. Farr: in Progress in Quantum Electronics, Vol.2 (Pergamon, Oxford 1972) p.141 F. Schuller, W. Behmenburg: Phys. Rpt. 12,273 (1974) N. Konjevic, J.D. Roberts: J. Phys. Chern. Ref. Data 5,209,259 (1976) N. Ksonjevic, M.S. Dimitrijevic, W.L. Wiese: J. Phys. Chern. Ref. Data 13, 619 (1984) E.L. Lewis: Phys. Repts. 58,1 (1980) G. Peach: Advances in Physics 30,367 (1981) N. Allard, J. Kielkopf: Rev. Mod. Phys. 54,1103 (1982) J.R. Fuhr, L.J. Roszman, W.L. Wiese: Bibliography on Atomic Line Shapes and Shifts, NBS Spec. Publ. 366 (19720; Suppl.1 (1974) J.R. Fuhr, G.A. Martin, B.J. Specht: Bibliography on Atomic Line Shapes and Shifts, NBS Spec. Publ. 366, Suppl.2 (1975) J.R. Fuhr, B.J. Miller, G.A. Martin: Bibliography on Atomic Line Shapes and Shifts, NBS Spec. Publ. 366, Suppl.3 (1978) J.R. Fuhr, A. Lesage: Ibid., Suppl.4 (1993) P.R. Berman: Appl. Phys. 6, 283 (1975) P. Anderson: Phys. Rev. 76, 647 (1949) J. Szudy: Acta Phys. Polon. A 40,361 (1971) J. Szudy, W.E. Baylis: J. Quant. Spectrosc. Radiat. Transf. 15,641 (1975) S.G. Rautian, 1.1. Sobleman: Usp. Fiz. Nauk 90, 209 (1966) [English trans!': Sov. Phys. - Uspekhi 9, 701 (1967)] S. Chandrasekhar: Rev. Mod. Phys. 15, 1 (1943) R.H. Dicke: Phys. Rev. 89, 472 (1953) D.R.A. McMahon: Austral. J. Phys. 34, 639 (1981) V.N. Faddeyeva, N.M. Terentyev: Tables of the Probability Integralfor Complex Argument (Pergamon, Oxford 1961)
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7.101 H. Massey, E. Burhop: Electronic and Ionic Impact Phenomena (Clarendon, Oxford 1952) 7.102 MA Mazing, M.A. Vrubleyskaya: Zh. Eksp. Teor. Fiz. 50, 343 (1966) [English trans!.: SOY. Phys. -JETP 23, 228 (1966)] 7.103 M.A. Mazing, P.D. Serapinas: Zh. Eksp. Teor. Fiz. 60, 541 (1971) [English trans!': SOY. Phys. -JETP 33, 294 (1971)]
List of Symbols
Constants
Bohr radius Velocity of light e Elementary charge If = h/21t Planck's constant divided by 21t m Mass of electron Ry = me 4 /2lf 2 Rydberg unit of energy a o = If/me 2
c
Quantum numbers j J JT
Electron angular momentum Atomic angular momentum Total angular momentum of a system including atom and outer (scattered) electron / Electron orbital momentum L Atomic orbital momentum Lp Orbital momentum of atomic core (of parent ion) LT Total orbital momentum of a system including atom and scattered electron m, M Magnetic quantum numbers n Principal quantum number s Electron spin momentum S Atomic spin momentum Sp Spin momentum of atomic core (of parent ion) ST Total spin momentum of a system including atom and scattered electron A. Orbital momentum of outer (scattered) electron Basic Notations
ao
a, a 1 A Aij
Set of quantum numbers for initial state of an atom Set of quantum numbers for final state Fitting parameter for approximation of rate coefficients (vu) Einstein coefficient for spontaneous emission (radiative transition probability) [S-I]
C
Fitting parameter for approximation of cross sections u D Fitting parameter for analytical approximation of calculated cross sections and rate coefficients DE Energy scaling parameter E. Energy of bound electron in state a .to,.t Initial and final energies of free electron lij Oscillator strength 1(8) Scattering amplitude F)., F;" FJ, Radial functions of scattered electron in various representations g(a) Statistical weight of level a G:;L.=(/n-l[SpL p]/SL} /nSL) Coefficient of fractional parentage [see Ref. 1.1] G (P) Function of analytical approximation for rate coefficients (vu) Gr(r,r') Green's function jx(z) Spherical Bessel function Jf (P) Holtsmark distribution function n* = Z2 Ry/I E I Effective principal quantum number N Number density of particles [cm - 3] PI (cos 8) Legendre polynomials P" Pn/ , P"I (r) = r Rnl (r), where Rnl (r) is radial function for bound electron Principal value of integral P Q, QK Angular factor defining the dependence of cross sections on angular momenta for transitions with no change of spin Q", Q; Angular factor for exchange cross sections S, Sit Scattering matrix T Temperature in energy units 7;k Transition matrix u = .t/AE = (.to - AE)/AE Electron energy in threshold units v Velocity of particles (vu) Rate coefficient averaged over Maxwellian velocity distribution [cm 3 S-I] Dimensionless transition probability, frequency of collisional transitions [S-I]
J
J
w.o.
307
List of symbols
w. (c)
Autoionization probability for atomic state c [S-I] z Charge of atomic core (of parent ion) Z = z -1 Charge of ion !E Charge of nucleus y Line width (full width) in Chapter 7, set of quantum numbers for atomic term in Sect. 6.2 y = aM lmm 3 Set of quantum numbers for a system including atom and scattered electron r = aA1/2L T ST Set of quantum numbers for a system including atom and scattered electron in representation of total momenta LI Line shift in Chapter 7 LIE = E j - Ek Energy difference for levels i and k K Multipole order Kd Rate coefficient of dielectronic recombination [em 3 s - 1] K, Rate coefficient for three-body recombination [cm 6 s- 1] K. Rate coefficient of radiative recombination [cm 3 s- 1j
o
Solid angle Impact parameter, density matrix P.u Spherical components of density matrix uaoa,u(ao, a) Effective cross section u(aoAo,aA) Partial cross section cp Fitting parameter for approximation of cross sections q. (u) Functions of analytical approximation for cross sections X Fitting parameter for approximation of rate coefficients Ud2" ·jn] = J(2jl + 1)(2j2 +1) ... (2jn+ 1) (ml m2lsu) Klebsch-Gordan coefficients (abbreviated notation)
p
Wigner's 3j symbol
6j symbol
~U} (aoll
Til
9j symbol a)
Reduced matrix element
Subject Index
Action function 80 Analytic approximate formulas for cross sections 78,85,86,111,112,117, 118, 119 for rate coefficients 79, 86, 111, 112, 113, 114, 116, 117, 118, 120, 123, 130, 285 for recombination coefficient 153 Angular factors 30-35, 225-231 Atomic core 1 Autoionization 1, probability of 126, 127 Bethe formula 40 Bohr quantization condition 80 Boltzmann distribution 4 Born approximation 36, 74 Born formula 37 Born-Oppenheimer approximation 31 Brinkman-Kramers formula 102, 104 Broadening by neutral particles 289-296 Doppler 245-251,263 impact theory of 239, 251-263 of highly excited (Rydberg) states 284-286 Cascade matrix 137, 138 Clesch-Gordan coefficient 257 Collision strength 23 Collisional-radiative model 136 Coronal model 136 Correlation function 238 Coulomb-Born approximation 31,51 Cross section differential 9 normalization of 54-56 of broadening 239, 240, 254 of shift 239, 240, 254 partial 21 Debye radius 278 Density matrix method in broadening theory 251-273 Detailed balance, principle of 5 Dicke narrowing of spectral lines 250
Dielectronic recombination cross section of 122 rate coefficient of 122, 123 semiempirical formula for the rate coefficient of 130 simplified model of 120, 121, 127 Dielectronic satellites 130 -136 Differential cross section 9 Distorted wave approximation 31 Doppler broadening 245-251,263 Effective principal quantum number 159, 203 Exchange radial integral 31, 32, 51 Fractional parentage coefficients 39, 235, 236 Green's function free electron 61 Coulomb 67,68,75 Holtsmark distribution 276 Hooper distribution 278 Impact parameter 14,84 Intercombination transitions 50 Intermediate coupling 32 Ionization cross sections 45-47 Ionization equilibrium 7, 8 OJ symbol 231 3j symbol, Wigner's 20 6j symbol 231 9j symbol 21, 236 12j symbol 236 Klein-Rosseland formula 5 Kramers approximation for radiative recombination 115, 116 for radiative transitions 139
309
Subject Index Landau-Zener formula 91 Line strength 99 Local thermodynamic equilibrium 136 LS coupling 20, 29 Matrix, density 252 K 22 S 22 T 22 Maxwell distribution 4 Milne formula 6 Normalization of cross sections 54 Ochkur approximation 51, 52 Optical electron 1, 17 Optical theorem 11 Orthogonalized functions approximation 51 Oscillator strength 40 Partial cross section 21 Partial wave expansion 10 Partition function 4 principle of detailed balance 5
Radial integrals, direct 31 exchange 31 Recombination collisional-radiative 143 dielectronic 1 radiative 1 three-body 1, 150-153 Reduced matrix element 229 Saha-Boltzmann equation 141 Saha distribution 4 Satellites, dielectronic 130-136 Scattering amplitude 10 Scattering channel 15, 69 Scattering matrix 22 Spherical Bessel, Hankel, and Neumann functions 27 Sum rules for cross sections 225 for 3nj symbols 232-235 Thermodynamic equilibrium 3 Thomson formula 119 Three-body recombination 1, 150-153 T matrix 22 Triangular condition 231 Unitarity of S matrix 16
Q-factors 30-35, 225-231 Quadratic Stark effect constant 286 Quantum theory of broadening
Weisskopf radius 241 Wigner-Eckart theorem 38 Wigner's 3j symbol 20
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