PLACE IN RETURN BOX to remove this checkout from your record. TO AVOID FINES return on or before date due. MAY BE RECALLED with earlier due date if requested. DATE DUE DATE DUE DATE DUE 2/05 p:/C|RCIDateDue.indd-p.1 AB INITIO CONFIGURATION INTERACTION (CI) CALCULATION OF THE CHARGE-DENSITY SUSCEPTIBILITY OF MOLECULAR HYDROGEN AND HIGHER-ORDER VAN DER WAALS INTERACTIONS FROM PERTURBATION THEORY By Ruth L. Jacobsen A DISSERTATION Submitted to Michigan State University in partial fulfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY Department of Chemistry 2006 ABSTRACT AB INI T10 CONFIGURATION INTERACTION (CI) CALCULATION OF THE CHARGE-DENSITY SUSCEPTIBILITY OF MOLECULAR HYDROGEN AND HIGHER-ORDER VAN DER WAALS INTERACTIONS FROM PERTURBATION THEORY By Ruth L. J acobsen The charge-density susceptibility x(r, r’;w) of a molecule is defined as the change in the w-frequency component 5pc (r, w) of the electronic charge-density at a point 1‘ within a molecule, due to a perturbing potential ’08 (1", w) of frequency w applied at a point r’ (within linear response). This work includes a derivation of an ab initio expression for the charge-density susceptibility and its application to calculate x(r, I"; w) of the H2 molecule as a function of r, r’, and w in the aug-cc-pVDZ basis set using a configuration interaction wavefunction with single and double excitations (CISD). Since CISD theory is equivalent to full configuration interaction (CI) theory in a two-electron case, the results are exact within a given basis set. Results of the calculations of X (r, r’; w) for the H2 molecule are analyzed, with emphasis on the behavior of the function when the frequency w is close to a molecular transition frequency from the ground electronic state. In order to test the calculations of x(r, r’; w) for the H2 molecule, the result for x(r, I"; (.0) has been used to calculate the frequency-dependent polarizabilities an, (w), ayy (w), and an (w) of H2 as a function of w in the DZ, DZP and aug-cc-PVDZ basis sets. Excellent agreement has been obtained between our results for static polarizabilities and the corresponding finite-field polarizabilities obtained with the MOLPRO quantum chemistry software package. Following a review of known results for the second-order and third-order correc- tions to the energy of interaction of two molecules in the polarization approximation, complex contour integration is used to derive a new equation for the third-order dispersion energy of two interacting molecules. The results for the second- and third— order interaction energies are used to obtain approximations to these energies for pairs and clusters of hydrogen fluoride molecules, in terms of the properties of the individual molecules. In Loving M emor‘y 0f Juan M. Lafuente June 27, 1940 - September 11, 2001 iv ACKNOWLEDGEMENTS There are several people that I would like to thank for helping me through graduate school and with this work: my advisors, Dr. Kathy Hunt and Dr. Piotr Piecuch, for their leadership, guidance, patience, and for teaching me with endless energy and enthusiasm; my former advisor, Dr. Warren Beck, for giving me a working knowledge of ongoing research in biophysical chemistry; my advisorial committee, indcluding Dr. Robert Cukier, Dr. James McCusker, and Dr. Jetze Tepe, for facilitating my understanding of the role of my work in theoretical chemistry as a whole; Dr. James Harrison, for his encouragement and for help with MOLPRO; Dr. D. J. Gearhart, Dr. Karol Kowalski, Dr. Mike McGuire, Dr. Ian Pimienta, Dr. Marta Wloch, Dr. Armagan Kinal, Dr. Peng-Dong Fan, Jeff, Maricris, Anirban, and Lisa Green, for their help and for their camraderie; Bronwyn, Emily, and Lisa Taylor, for cycling, swimming, and running with me; Chi Alpha Christian fellowship, especially Mark and Cheryl McKeel, Anne Grain, and Janet Lewis, and also to Mary Frances and Victoria, for being as solid as bedrock; my extended family and my in-laws, Sue, Jake, and Katy, for all of their love and support; my sisters Cynthia, Christine, and Catherine, for their unconditional love, acceptance, encouragement, and for always reminding me to laugh; my late father, for being my hero in so many ways; my mother and Mike, for being much more than I can ever explain; and finally, my Lord Jesus Christ, the Ultimate Mystery — I live and breathe in you, my Hope and Strength forever. TABLE OF CONTENTS List of Tables ix List of Figures xii 1 Ab Initio Configuration-Interaction (CI) Calculation of the Charge- Density Susceptibility of H2 from Perturbation Theory 1 1.1 Introduction ................................ 1 1.2 x(r,r’;w) at C1 Level: Derivation .................... 8 1.3 Algorithm for x(r,r’;w) ......................... 12 1.4 Results of x(r, r’ ;w) Calculations .................... 12 1.5 Results of (10,300) Calculations ...................... 18 Higher-Order van der Waals Interactions from Perturbation Theory 23 2.1 Introduction ................................ 23 2.2 The Quantum Mechanical Theory of Intermolecular Interactions . . . 24 2.3 The Polarization Approximation ..................... 25 2.3.1 Introduction ............................ 25 2.3.2 The First-, Second-, and Third-Order Polarization Energies . . 28 2.3.3 The Convergence of the Polarization Expansion ........ 31 2.3.4 Summary ............................. 31 2.4 The Multipole Approximation ...................... 32 2.4.1 Introduction ............................ 32 2.4.2 The Cartesian and Spherical Formulations of the Intermolecular Interaction Operator in the Multipole Approximation ..... 33 2.4.3 The van der Waals Constants .................. 35 2.4.4 Removing the Angular Dependence from the Multipole Expan- sion for the Interaction Energy ................. 36 2.4.5 The Convergence of the Multipole Expansions of the Inter- molecular Interaction Operator and Interaction Energy . . . . 40 2.4.6 The Multipole Approximation and Nonadditive Interactions . 42 2.4.7 Summary ............................. 42 2.5 The Bipolar Expansion .......................... 43 2.5.1 Introduction ............................ 43 2.5.2 The Bipolar Expansion of Buehler and Hirschfelder ...... 44 2.5.3 The Fourier Integral Formulation of the Bipolar Expansion . . 45 2.6 Symmetry-Adapted Perturbation Theory ................ 46 2.6.1 Introduction ............................ 46 2.6.2 Weak Symmetry Forcing: Symmetrized Perturbation Theories 48 2.6.3 Strong Symmetry Forcing: Hirschfelder-Silbey Perturbation The- ory ................................. 49 vi 2.6.4 The First and Second-Order Energies in Symmetrized Rayleigh- Schr6dinger Perturbation Theory ................ 2.6.5 The Convergence of the Symmetrized Rayleigh-Schrodinger and Hirschfelder-Silbey Perturbation Theories ............ 2.7 Many-Body Perturbation Theory .................... 2. 7.1 Introduction ............................ 2.7.2 The Electrostatic Energy in Many-Body Perturbation Theory 2.7.3 The First—Order Exchange Energy in Many-Body Perturbation Theory ............................... 2.7.4 The Second-Order Induction Energy in Many-Body Perturba- tion Theory ............................ 2.7.5 The Second-Order Dispersion Energy in Many-Body Perturba- tion Theory ............................ Molecules A and B 50 52 53 53 58 61 63 65 3 The Second-Order Correction to the Energy of Two Interacting 67 The Third-Order Correction to the Energy of Two Weakly Interact- ing Molecules 4.1 Non-Zero Contributions to AEéi: .................. 4.2 Higher-Order Induction: Terms of First-Order in Both 11’“) and [13° . 4.3 Hyperpolarization: Terms of Third-Order in p30 or it“ ........ 4.4 Induction-Dispersion: Terms of F irst-Order in 11’“) or p30 ....... 4.5 Third-Order Dispersion: Terms of Order Zero in Both HA0 and p30 80 80 81 85 89 114 Numerical Estimates of the Second— and Third-Order Corrections to the Interaction Energy of Two or Three Hydrogen Fluoride (HF) Molecules for Various Geometries 5.1 Leading Contribution to the Second-Order Correction to the Interac- tion Energy of Two Molecules ...................... 5.1.1 The Second-Order Correction to the Interaction Energy of Two Colinear Molecules ........................ 5.1.2 The Second-Order Correction to the Interaction Energy of Two Colinear HF Molecules ...................... 5.1.3 The Second-Order Correction to the Interaction Energy of Two Parallel Molecules ......................... 5.1.4 The Second-Order Correction to the Interaction Energy of Two Parallel HF molecules ...................... 5.1.5 The Second-Order Correction to the Interaction Energy of Two Perpendicular Molecules ..................... 124 124 125 129 133 137 5.2 The 2nd -Order Correction to the Interaction Energy of Three Molecules 139 5.2.1 The Second-Order Correction to the Interaction Energy of Three HF molecules, Arranged Colinearly ............... 5.2.2 The Second-Order Correction to the Interaction Energy of Three Parallel HF molecules ...................... vii 140 5.3 The Third-Order Correction to the Energy of Interaction of A and B 143 5.3.1 The Third-Order Correction to the Interaction Energy of Two Colinear Molecules ........................ 145 6 Summary, Concluding Remarks, and Future Perspectives 163 Appendix A. Fortran CISD Code for Calculating x(r, r’ ;w) and am; (w) 179 Appendix B. Tables 247 Appendix C. Figures 251 References 268 viii List of Tables Table 1. Non-zero terms in the third-order interaction energy of molecules A and B, classified by order in the permanent dipoles of A and B. Note that we have let \I/gi) = (0) _ WA) and \I’OB — '03). 248 Table 2. Comparison of an (w) , Orgy (w) , and azz(w) values calculated by inte- grating x(r, I"; w) using the algorithm described here and by finite-field calculations performed with the MOLPROl7 quantum chemistry software package. Polarizabilities were calculated in the DZ, DZP, and aug-cc-pVDZ basis sets, and polarizabilities are given in a.u. 249 ix List of Figures Fig. 1. The charge-density susceptibility of the H2 molecule at the CISD level with w = 0 a.u., r’ = 0, 0,0,:r = 0, -3.25 S y S 3.25 a.u., —3.25 S 2 S 3.25 a.u., and Ag = A2 = 0.05 a.u. in the aug-cc-pVDZ basis set. For this calculation, the internuclear axis of H; was oriented along the Z -axis of the laboratory frame. 251 Fig. 2. The charge-density susceptibility of the H2 molecule at the CISD level with w = 0.3858668352248763 a.u., r’ = 0,0, 0,3: = 0, —3.25 S y S 3.25 a.u., —3.25 S 2 S 3.25 a.u., and Ag = A2 = 0.05 a.u. in the aug—cc-pVDZ basis set. For this calculation, the internuclear axis of H2 was oriented along the Z -axis of the laboratory frame. 252 Fig. 3. The charge-density susceptibility of the H2 molecule at the CISD level with w = 0.4812104263202694 a.u., r’ = 0, 0, 0, :L' = 0, —3.25 S y S 3.25 a.u., -3.25 S 2 S 3.25 a.u., and Ag = A2 = 0.05 a.u. in the aug—cc—pVDZ basis set. For this calculation, the internuclear axis of H2 was oriented along the z -axis of the laboratory frame. 253 Fig. 4. The charge-density susceptibility of the H2 molecule at the CISD level with w = 0.3858668352248763 a.u., r’ = 0,0, 07,513 = 0, —3.25 S y S 3.25 a.u., Ay = A2 = 0.05 a.u., and Ag = AZ = 0.05 a.u. in the aug-cc-pVDZ basis set. For this calculation, the internuclear axis of Hz was oriented along the Z -axis of the laboratory frame. 254 Fig. 5. The charge-density susceptibility of the H2 molecule at the CISD level with w = 0.4648380650856789 a.u., r' = 0,0, 07,3: = 0, —3.25 S y S 3.25 a.u., —3.25 S 2 S 3.25 a.u., and Ag = A2 = 0.05 a.u. in the aug-cc—pVDZ basis set. For this calculation, the internuclear axis of Hz was oriented along the z-axis of the laboratory frame. 255 Fig. 6. The zz component of the frequency-dependent polarizability Ozzz (w) of H2 as a function of frequency w at the CISD level in the DZ, DZP, and aug—cc-pVDZ basis sets. 256 Fig. 7. The 22 component of the frequency-dependent polarizability Ozzz (w) of H2 at the CISD level as a function of o.) in the DZ, DZP, and aug-cc-pVDZ basis sets. Here, we show the data included in —200 S an (w) S 200 a.u. in Fig. 6. X 257 Fig. 8. The xx component of the frequency-dependent polarizability an (w) of H2 at the CISD level as a function of w in the DZP and aug-cc-pVDZ basis sets. 258 Fig. 9. The xx component of the frequency-dependent polarizability am (0}) of H2 at the CISD level as a function of w in the DZP basis set. 259 Fig. 10. The yy component of the frequency-dependent polarizability ayy (w) of H2 at the CISD level as a function of w in the aug-cc-pVDZ basis set. 260 Fig. 11. The semi-circular contour C of radius R1 in the upper complex half plane. In this figure, 1m and Re denote the imaginary and real axes, respectively. Also 0 is the angle between the real axis and R1, and S is the portion of C off the real axis. 261 Fig. 12. Colinear arrangement of molecules A and B. In this figure, as, y, and 2 denote the axes of the laboratory frame, and :r’, y’, and ;’ denote the axes of the molecular frames of A and B. Also, A1 and A2 are the nuclei of molecule A, 81 and 82 are the nuclei of molecule B, COM A and COMB are the centers of mass of molecules A and B, and RAB is the distance between the center of mass of A and the center of mass of B. 262 Fig. 13. Parallel arrangement of molecules A and B. In this figure, :13, y, and 2 denote the axes of the laboratory frame, and :r’, y’, and z’ denote the axes of the molecular frames of A and B. Also, A1 and A2 are the nuclei of molecule A, Bl and 82 are the nuclei of molecule B, COM ,4 and COMB are the centers of mass of molecules A and B, and R AB is the distance between the center of mass of A and the center of mass of B. 263 Fig. 14. Perpendicular arrangement of molecules A and B. In this figure, 2:, y, and z denote the axes of the laboratory frame, 27’, y’, and 2’ denote the axes of the molecular frame of A, and x”, y”, and 2" denote the axes of the molecular frame of B. Also, A1 and A2 are the nuclei of molecule A, BI and B2 are the nuclei of molecule B, COM ,4 and COMB are the centers of mass of molecules A and B, and RAB is the distance between the center of mass of A and the center of mass of B. 264 xi Fig. 15. Colinear arrangement of three HF molecules. In this figure, we have labeled the three HF molecules HFI, HF2, and HF3 in order to distinguish between them. Also, as, y, and z denote the axes of the laboratory frame, 33’, y’, and 2’ denote the axes of the molecular frames of each HF molecule, H1, H2, and H3 are the hydrogen nuclei in HFl, HF2, and HF 3, F1, F 2, and F3 are the fluorine nuclei in HFI, HF 2, and HF3, and COMHFI, COMHF2, and COMHF3 are the centers of mass of HF], HF2, and HF3. Finally, RHF1_HF2, RHF1_HF3, and RHF2_HF3 are the distances between the centers of mass of HF1 and HF2, HF1 and HF3, and HF2 and HF3, respectively. 265 Fig. 16. Parallel arrangement of three HF molecules. In this figure, we have labeled the three HF molecules HF1, HF2, and HF 3 in order to distinguish between them. Also, :13, y, and 2 denote the axes of the laboratory frame, :r’, y’, and 2’ denote the axes of the molecular frames of each HF molecule, H1, H2, and H3 are the hydrogen nuclei in HF1, HF2, and HF3, F1, F 2, and F3 are the fluorine nuclei in HF 1, HF2, and HF3, and COMle, COMHF2, and COMHF3 are the centers of mass of HE, HF2, and HF 3. Finally, RHFl—HF2, RHF1_HF3, and Ryp2_Hp3 are the distances between the centers of mass of HFl and HF2, HF 1 and HF3, and HF2 and HF3, respectively. 266 xii 1 Ab Initio Configuration-Interaction (CI) Calcula- tion of the Charge-Density Susceptibility of H2 from Perturbation Theory 1.1 Introduction The charge-density susceptibility x(r, r’; w) gives the change in the w-frequency component 5pc (r, w) of the electronic charge density at point r within a molecule, due to a perturbing potential ve(r’ , w) of frequency an applied at r’ (within linear response),1 6pe(r,w) = fx(r,r';w) ve(r',w) dr’. (1) Molecular properties, such as dipole and higher-order polarizabilities, Sternheimer electric field shielding tensors,5 induction energies for interacting moleculesf"10 van der Waals dispersion energies,11 infrared intensities,5 electronic reorganization terms in vibrational force constants,6’7 and intramolecular dielectric functions4 depend on the charge-density susceptibility x(r, r’; w). The dipole polarizability 003(0)) of a molecule is the first moment of the charge-density susceptibility x(r, r’; w) ,with respect to both r and r' , (1.30) = f 7.. r2. x, (8) where we have let w = w . The states Ip) are the eigenstates of the unperturbed atom (which is either atom A or B in this case), and I0) is the ground state of the unperturbed atom. Again, we are using Koide’s notation in Eq. (8). Also, fiwp — Ep—EO, where E'p and E0 are the energies of states | p) and I0). Finally, Q)” (It) and Q)" (’6') are multipole moment operators which are defined in Koide’s work in terms of spherical harmonics and Bessel functions. The polarizability a; (k, k’; w) in Eq. (8) can be approximated using the variational method of Karplus and Kolker19 or other variational methods. After calculating Oz; (’9, k’; w) , one can use his or her results for Oz; (k, k’; w) and the appropriate spherical harmonics to obtain 01A (k, k'; w) and a3 (—k, —k’; zu) . Finally, using the resulting expressions for 01A (k, k’; w) and Oz B (—k, —k'; W) and Eq. (7), one can obtain an approximate dispersion energy of interaction of atoms A and B. References 1, 25—30 and 31 give equations for second-order dispersion energies that depend on approximate charge- 4 density susceptibilities and include other derivations and calculations that are related to these equations. Recently, Kohn, Meir, and Makarov20 have used density functional theory (DFT) to derive a seamless expression for the van der Waals interaction energy of two atomic or molecular systems. The expression is seamless in the sense that it yields accurate van der Waals energies at any intersystem distance. They began their derivation by using either the local-density approximation (LDA) or the generalized-gradient approximation (GGA) to describe the electron density 7) (r). Next, they separated the Coulomb potential into short and long-range parts, and assumed that the van der Waals energies could be completely attributed to the long-range interactions. At this point, they used the adiabatic connection formula to write the long-range interaction energy. After transforming this expression into the time domain, they obtained the correct long-range limit for the van der Waals energy EvdW of two spherically symmetric atoms A and B, Co EvdW = _E’ (9) with the following expression for Cg : 3 °° °° (t) (t > X2Z 1 X213Z 2 C = - dt dt . 10 6 71' f l/ 2 t1 + t2 ( ) 0 0 In Eq. (9), R = IR A — RBI, where RA and R3 are the coordinates of the nuclei of atoms A and B, respectively. In Eq. (10), X22 is the 2 component of the response of the electron density to a perturbation applied in the 2 direction. In equation form, this response is X” = fdr1dr2X(r1,r2)ZIZ2a (11) where X (r1, r2) is the static charge-density susceptibility. Dobson and co—workers""1723 have developed a seamless density functional for cal- culating the van der Waals interaction energy of atomic, molecular or other physical systems. The functional is defined by four equations, and Dobson and Wang give spe— cific forms of these equations for the interaction of two jellium metal slabs in reference IGA( 21. The first equation gives the average ground-state electron density 77' z, z’) of 5 the interacting system. The second equation, which depends on fiIGA (Z, Z') and the Kohn—Sham polarization response a??? of the system, gives the Kohn-Sham density- density response function X KS (2, 2’, q”, 28) of the interacting system. The third equation is the Dyson-like screening equation for the Kubo density-density response function )0 (r, r’; w = 28) of the interacting system. When A = 1 in the Kubo density-density response function, we obtain the frequency-dependent charge-density susceptibility x(r, r’; w) defined in this work. The equation which gives the Kubo density-density response function depends on the Kohn-Sham density-density re- sponse function, the exchange-correlation kernel fch (r, r’;w = 28) of the system, and a modified electron—electron interaction AVCoul . Finally, the fourth equation for the van der Waals density functional is the adiabatic connection fluctuation-dissipation (ACFD) formula. This equation uses VCoula X» and X KS as input, and gives the correlation 1 notation to energy of the system. In this work, we have used Dobson and Wang’s2 refer to all quantities contained in the four equations that yield their seamless density functional for van der Waals interactions. Also, all quantities mentioned in this work that appear in Dobson and Wang’s equations are defined in reference 21. Dobson and Wang have carried out a related derivation (and calculations) in reference 24. Equations for the second-order dispersion energy that depend on charge-density susceptibilities are superior to the corresponding point-multipole expressions for the second-order dispersion energy because the former equations account for charge- overlap effects that are neglected in the latter expressions. Because charge-overlap effects are accounted for, the dispersion energy as defined in terms of charge-density susceptibilities is finite as R —> 0 , whereas the corresponding infinite series for the point-multipole dispersion energy diverges. The static charge—density susceptibility x(r, r’) determines the derivative of the electronic charge density with respect to nuclear coordinates,5 5P8(r)_ A —1/ I I A r A-1 BRA —Z (47reo) dr x(r,r)V Ir R| , (12) 6 where Z A is the charge of nucleus A with coordinates RA , and VA denotes the derivative with respect to RA . Eq. (12) holds because the electronic charge density responds via the same susceptibility to an applied potential and to the change in the nuclear Coulomb potential when a nucleus shifts.5 Changes in the electronic dipole moment as a molecule vibrates depend on linear combinations of the deriva- tives 8p8(r) /8RA ; thus the intensities of vibrational transitions are related to the internal charge redistribution in the molecule by Eq. (12). Similarly, the electronic charge redistribution term in harmonic force constants depends on x(r, r’) ; this term corresponds to the induction energy energy of the molecule, due to changes in the nuclear Coulomb field, as the molecule vibrates.7 A non-local intramolecular dielectric function ev‘1(r, r’; w) characterizes the screening of an applied potential ve(r; w) by the electronic charge redistribution, to give an effective potential veff(r, w) within the molecule veff(r,w) = [651(r,r';w) ve(r',w) dr'. (13) The dielectric function is related to x(r, I"; w) by4 60 e;1(r,r’;w) = 6(r — r') + (47reo) 1./r—-dr”| r”| 1)((r”,r';tu). (14) The correlations of the spontaneous quantum mechanical fluctuations in charge density are determined by the imaginary part of the charge—density susceptibility x”(r, I"; w) via the fluctuation-dissipation theorem,57 $<5pe(r,w) 6pe(r’,w’) + 6pe(r’,w’) 5pe(r,w)> = (5;) x”(r, r’;w) x6(w+w)coth (2%). (15) For this reason, the total electronic energy of a molecule is determined by x(r, r’; w) and the permanent molecular charge density,58 _ _ 1 r r,

> 25,32” ("r Ir—R_7I W/d d lr-r’l (a) / . /M It? — (é) (3) g 2;. R... / dr 04:31:}; r)“. (16) In Eq. (16), 266 is an electronic self-energy. Additionally, the charge—density susceptibility x(r, r’;w) is related to the softness kernel as defined in density functional theory.”34 The static charge—density susceptibility x(r, I") has been calculated ab initio using a finite field CI approach for water by Li, Ahuja, Hunt, and Harrison.32 Ando,35 Zangwill and Soven,36, Gross and Kohn,”:38 and van Gisbergen and coworkers39 have developed techniques for calculating the charge-density susceptibility within density functional theory (DF T). The charge-density susceptibililty can also be calculated ab initio using time-dependent perturbation methods, 40’44’41743’45_5° or by quantum Monte Carlo methods.51-53 Fur— pseudo—state techniques, thermore, an ab initio expression for the charge-density susceptibility x(r,r’;w) can be formulated by deriving the linear response function within coupled-cluster (CC) theory. 54 1.2 x(r, r’ ;w) at CI Level: Derivation Quantum mechanically, X(1‘a 1";w) = (‘I’olpe(r) C(01) Pelr')|‘1’0> + (wfllpeh'l) G(—W)pe(r)|\110), (17) where \Ilo is the ground-state wavefunction, pe(r) is the electronic charge-density operator at r , N r) = —Z (5(r — ri), (18) i-l pe (r’) is the charge-density operator at r’ ,and C(w ) is the reduced resolvent, G(w) = (1— mm — Eo - n...) =2 E'waf’flw. (19> K750 In Eq. (19), H is the electronic Hamiltonian for the unperturbed molecule, 90 is the projection operator for the ground-state wavefunction, and W K is the Km excited-state wavefunction. Also, E0 and E K denote the energies of the ground and K th excited states, respectively. Thus x = Z00040011,.)(“WWW K9“) EK - E0 — hw ((r‘l’olpe’ )l‘I’Kll‘I’KlpeO‘ )I‘I’0> + K220 EK- E0 + m . (20) At CI level, the ground and Kth excited- state wavefunctions ‘1'0 and \I/ K have |\IIO) = 0)| +;c’a(K )Icrgl) + Zcfif i>j.a>b + =le Olll‘DJ J 26.11“ MM) (21) the form I‘I’K) In Eq. (21), IQ) is the reference determinant for the ground state, VP?) is a singly- excited determinant, and I933?) is a doubly-excited determinant. Additionally, |J) represents all possible determinants in the full CI expansion. The coefficients CJ(K) are the CI coefficients, determined by solving the Schrédinger equation at C1 level, HI‘I’Kl = EKl‘I’Kl- (22) From Eqs. (20) and (21), x(r, r'; w) = A(r, r’; w) + A(r’, r; —w), (23) Where A(r,r’;w)= Z :c 0ch, Kc)J~(K)ch(0) K750 J,,J' J” J’” Ian/2400.1)<J~IpeIJ~I> (24) Ex — E0 _ hw . Since pe(r) is a one-electron operator, the matrix elements in Eq. (24) vanish unless J and J ' differ by at most one orbital occupancy. We separate A(r, I"; 02) into 9 four sets of terms, based on the relationship between the determinants [<13 J), |JI), ICIDJH) ,and |¢Jm> , A(l‘, I"; w) = Z AJ’J”(r, 1"; OJ) + Z AJ,J”#JW(I', I"; w) '1le J": J,” J:JI~JH#JIN + Z: AJ¢J’,J”(r, I"; w) J¢JI,JII=JIH + Z AJ¢JIJH¢JW(I', I"; w). (25) J75J’,J"§£J'" Terms in Eq. (24) with J = J’ and J” = J,” are included in AJ,J"(r, r’;w) , etc. In terms of the atomic spin orbitals (b1, , qfiq, (fit , and (Du and the expansion coefficients dls that relate molecular orbital l to atomic orbital ((93 , AJ,J~(r.r';wI = Z ¢p(r)¢q(r)¢t(r’)¢u(r’) pflqtu x Z J): CJ(0)CJ(K)CJ”(K)CJ”(O) K740 i( j(,J”) occ dipdizdjtdju EK— E0 — hw = Z 83??wa (rr)¢q( )cMr’) 0.0“). (26) pmqtu In Eq. (26), the sum over i(J) runs over all molecular orbitals i that are occupied in determinant J and similarly for the sum over j(J”) . The sum over p, q, t , and It runs over all atomic orbitals. For J aé J ' ,we define l(J, J’) as the molecular orbital occupied in J but not in J ', 7'(J, J ’) as the molecular orbital that is occupied in J ' but not in J , d)”, J’)? is the coefficient of atomic orbital p in molecular orbital l, and dr(J,J’)q is the coefficient of atomic orbital q in molecular orbital 7‘ (and similarly for J ” 75 J m ). We obtain AJ=JI’JII#JIII E AJJII¢JHI( r, 1‘" ,LIJ) —Z ¢p(r) 05t( I") gbu(r’) pqtu X Z Z CJ(0)CJ(K)CJ"(K)CJ”’(O) K#Oi(J),occ dipdiqdl(J/I,Jlll)tdr(JII,JIII)u EK— E0 — hw = Z BJJ"¢J'"(‘*’ “01M )¢q(r)¢t(r')¢u(r’) (27) pmqtu 10 AJ¢J’,J”=J”’(rar,;w) = Z ¢p(1‘)¢q r) (M M75 N ) p, q,t, u X 2 Z CJ(O )(CJ' KC)J"(K)CJ"(O) K960j(J”) ,occ dI(J,J’) pdr(J,J’)qdjtdju EK— E0 — fiw = 2 333:3,» J... an )¢q(r)¢z(r’)¢u(r’)(28) pmqtu AJ¢J’,J"#J’”(rIrI;w) = Z ¢p(r)¢q(r)¢t(r’)¢u(r’) mam d I dT‘ I d n m d7. II In x Z l(J,J)p g,J)q It: ,Jfi); (J ,J )u K760 K_ 0" X CJ(0)CJ'(K)CJ"(K )ch(0) : Z B3231J1195Jm(w LU) pq,,tu X ¢p(r)¢q(r W) WK )¢u( I")- (29) The calculations of the charge-density susceptibility x(r, r’; w) in this work are based on Eqs. (26) - (29). To check the calculations of x(r, r’; w) , we have calculated a03(w) from x(r, r’;w) and Eq. (25). The frequency-dependent polarizability 04030.0) is given by aaW) = :Wolflal‘l’mmwm K #0 E K - E0 — hw + Z (‘I’olual‘I’KI (\I’KIHaI‘I’M (30) K #0 EK— E0 + M where ya and #3 denote the a and fl components of the dipole moment Operator, given by [10: 2: 62-730, + £431 Z jRja where N IS the total number of i=1 J: electrons in the molecule and M 18 the total number of nuclei. Also, 62- is the charge on the ith electron, ZJ - is the charge on the jth nucleus, Tia is the a component th of the vector from the origin to the z electron, and Rja is the a component 11 of the vector from the origin to the jth nucleus. Eq. (2) follows from Eqs. (20) and (30). From Eqs. (25) - (29), ' t OCH/3(a)) = Z B3?J3fJ",-]m(w) [liq ”:3”, (31) J,JI,JII,JIH where Bqujzf‘lfls‘l’” (LU) = 333;}:(01) ($le 6JIIJIII + 33?;gaéJ/n (LU) 6JJI (1 — 6]”,1’”) + ngzjivjfl (w) (1 _ 6JJI) 6JIIJIII t + B‘gzétjl,Jll¢JI/I(w) (1 — 6JJ’) (1 — 6J"J’”); (32) uflq and [1.2" are dipole moment integrals in the atomic orbital basis, defined as #2." = (Plfialcv and Mfg“ = (tlfialm - 1.3 Algorithm for x(r, r’ ,w) We have used the General Atomic and Molecular Electronic Software System (GAMESS)16 to calculate the one- and two-electron integrals, to find the molecu- lar orbitals at restricted Hartree-Fock (RHF) level, and to transform the one- and two-electron integrals from the atomic orbital basis to the molecular orbital basis. Then we have solved the CISD (CI singles and doubles) equations to find the CISD coefficients C J(K ) , the ground-state energy E0 , and the excited-state energies EK . Using these quantities, the atomic orbitals, and the transformation coeffi- cients from the atomic orbital to molecular orbital basis, we have calculated AJJH, A Jaé J', J”, AJ,J”¢J’” and A J¢ Jl’ Jrr¢ Jm and then summed to obtain the charge- density susceptibility x(r, r’ ;w) of the molecule. To calculate 003(w), we have used dipole moment integrals f 7‘0, q§p(r) ¢q(r) dr and f T’fi ¢t(r’) qfiu (r’) dr’ computed in the linear-response coupled-cluster pro- gram written by Kondo and co—workers.55’56 1.4 Results of x(r, r’ ;w) Calculations We have calculated the charge-density susceptibility of the H2 molecule at the CISD level as a function of frequency w and points r and r’ using a program based on 12 the algorithm presented here. Since CISD is equivalent to full CI in a two-electron case, our results are exact within the basis set that we used. Each plot of the charge- density susceptibility that we will present here was generated by fixing w, r’ , and :17 ,and calculating x(r,r’;w) for all y and 2 included in —3.25 S y S +3.25 and —3.25 S 2 S +3.25 a.u. with Ay = A2 = 0.05 . The aug-cc-pVDZ basis set was used for the plots. Note that the internuclear axis was aligned with the z -axis for all calculations, and that we used the equilibrium geometry of the H2 molecule (the equilibrium bond length of H2 is 1.40126 a.u.). Before presenting the results of our calculations, let us discuss some important pr0perties of the charge-density susceptibility that we will use to understand the behavior of x(r, r’;w) . Recall Eq. (20) from Sect. 1.2, x KaéO EK — E0 — fiw (\Polpe(rr’)l‘l’1<><\1’xlpe(We) + 1;)(EK — E0 + fiw . (33) According to Eq. (33), x(r, r’; w) is singular for energies fiw that are equal to :t (EK - E0) , if the corresponding terms in the numerator do not vanish. We have verified this property of x(r, r’; w) by calculating x(r, r’; w) of H2 at r’ = 0,0,0, :13 = 0 , and w = E1 — E0 (data not shown). For these conditions, x(r,r’;w) of H2 was approaching infinity at —3.25 S y S 3.25 and —3.25 g z s 3.25 with Ay = Az = 0.05 . If W0 is a singlet state and \11 K is a triplet state, then the matrix elements (‘I’olpe(r)l‘I’K> , (‘I’olpe(r’)l‘I’K>, (‘I’Klpe(r)l‘l’o>, and <‘1’Klpe(r’)l‘1’o> van- ish. This holds because ,0.3 (r) and pg (1") are spin-independent operators, so that it is impossible for pe(r) and pe(r’) to change the spin of \I1 K to a singlet. Therefore, triplet states will not contribute to x(r, r’; w) , and x(r, r’; w) will not be singular at energies which correspond to transitions to triplet states. This will be true for all of our data, since W0 is a CI singlet ground state for all of our calculations. 13 In the aug-cc-pVDZ basis, H2 has 18 spatial orbitals and 36 spin orbitals. Eigh— teen of the spin orbitals have a spin functions, and the other eighteen have fl spin functions. We label a spin orbitals with odd integers, and 5 spin orbitals with even integers. In terms of spatial orbitals, the lowest energy spatial orbital (the lag orbital) is doubly occupied in the ground-state configuration of H2. In terms of spin orbitals, the lowest energy a and fl spin orbitals are occupied in the ground- state configuration of H2. Recall from Eq. (21) that the ground- and excited-state CISD wavefunctions are generated from a linear combination of all possible singly- and doubly-excited determinants. Therefore, according to Eq. (21), the ground-state wavefunction for H2 in the aug-cc—pVDZ basis is: lilo) = 00(0)|>+C§(0)|<1>l>+C%(0)|<1>l> + 03(0)|3> + 03(0)| + + C§i(0)l¢l§> + C§§(0)l¢l3> + = 00(0)|‘1>>+ 01(0) “‘1’?) - |<1>3>l + + C§3(0)l@l3> + (34) where (1):), (13?, (1)4 , and § are singly-excited determinants which correspond to exciting an electron from spin orbital 1 (1090,) to spin orbital 3 (10m) , from spin orbital 1 (1090) to spin orbital 5 (2090,) , from spin orbital 2 (1095) to spin orbital 4 (low) , and from spin orbital 2 (1095) to spin orbital 6 (2093) , respectively. Also, (1)333 and (Pig are doubly-excited determinants corresponding to exciting electrons from spin orbitals 1 and 2 to spin orbitals 3 and 4, and from spin orbitals 1 and 2 to spin orbitals 3 and 6, respectively. In Eq. (34), the quantity lib?) — ((1)3) is a singlet spin-adapted configuration state function. This is because each determinant involved in the linear combination in either quantity involves exciting an electron from the same lower energy spatial orbital to the same higher energy spatial orbital, and the resulting determinantel configuration is an eigenfunction of S2 and S = 0 . If we write configuration ICE?) — |§> in terms of spatial orbitals $5 and spin functions Oz and fl, where (i/I,|21Ij) = (525 and (alfi) == 503 , we have: IiI — I3I = (1)0(2 - fi(2)a(1)l- (35) According to Eq. (35), the spin part of FF?) — [@3) is antisymmetric with respect to electron exchange. We can carry out a similar analysis on each excited-state \I’ K 14 in the aug—cc—pVDZ basis set in order to determine whether a particular W K is a singlet or a triplet state. Let us return to our discussion of the properties of x(r, I"; w) . To do this, consider the symmetry of the H2 molecule. Since H2 belongs to the Dooh point group, there are an infinite number of irreducible representations that can be used to classify the symmetries of its orbitals and states, including 23', 2;, 2;, E; , Hg, Hu, Ag , and Au . If I" = 0 and W0 is a 129 state, then matrix elements (‘I’olpe(r)|‘I’K>, (‘I’olpe(l")|‘I’K>a (‘I’Klpe(l‘)|‘1’0> ,and (‘I’Klpe(r')|‘1’0> are nonzero only for ‘11 K states that have 129 symmetry. Therefore, when I" = 0 , x(r, r’; (.0) will only be singular for energies fiw approaching the energy of transition to 29 states. In order to understand why this is true, we need to consider the composition of the charge-density susceptibility. According to Eqs. (25) - (29) in Sect. 1.2, the charge-density susceptibility is essentially a sum of products of atomic orbitals evaluated at r and I" which is weighted by CI coefficients, coefficients for converting atomic orbitals to molecular orbitals, and energy denominators. Although we have not done so here, we can also write the charge-density susceptibility as a sum of products of molecular orbitals evaluated at r and r’ and weighted by C1 coefficients and energy denominators. Now, consider the molecular orbitals of H2 as a function of r’ . The 0'g orbital is nonzero at Z, = 0 , and the au orbital is zero when 2’ = 0 . The 7rg and 7ru orbitals are also zero when 2’ = 0 . Therefore, the only orbitals and states which will contribute to X (r, I"; w) of H2 when r’ = (0,0,0) are Ug-type orbitals and 29 -type states. Note that this property of x(r, I"; w) is also true when r = 0 . If 1" lies along the molecular axis and W0 is 129 state, then matrix elements (‘I’olpe(r)|‘1’K>, (‘I’olpe(r’)|‘1’K>, (‘I’Klpe(r)l‘1’o) ,and (‘I'KIpe(r’)l‘Po> will only be nonzero for 129 and 12:1 states. Therefore, when r’ lies along the molecular axis, the only singularities in x(r, r’; w) will occur at transitions to 129 or 12,, states. This property of x(r, r’; w) can also be explained in terms of 15 the molecular orbitals of H2. The 09(r’) and 0,,(r’) orbitals are nonzero for all z’ except 2' = 0 . Therefore, these orbitals will contribute to x(r, r’; w) for all r’ = (0,0, i2) except I" = (0,0,0) . Since the 7rg(r’) and 7n,(r’) orbitals are zero for all 2" , they will not contribute to x(r, r’; w) when r’ is on the large 2’ axis. This property of x(r, I"; w) is also true for r = 0 . Note these results hold when the molecular axis is along the z’ (or z ) axis, which applies for all of our calculations. If r’ is somewhere in the 5132: plane, then the matrix elements (\I’Olpe(r)|\IJK), (ll/olpe(r')|\IJK), (\lelpe(r)|‘1’0), and (‘I’Klpe(r’)|‘1’0> will only be nonzero for 1H,; and 1AxLyz-type states (of the states generated by the basis set used). As a result, if r’ is in the 332 plane, x(r, r’; w) will only blow up for energies which correspond to transitions to 111$ and 1A5,:2_y2 states in these calculations. Figure 1 shows the charge-density susceptibility of the H2 molecule with w = 0 and r’ = (0,0, 0) . As expected, x(r,r’;w) does not become singular when w = 0 , since we are not near any transition energies. Also, note that X (r, I"; (.0) has the general shape of a 0'9 molecular orbital of H2. This is as expected, since I" = (0, 0,0) , for which only 0’9 type orbitals and 29 type states contribute to X(r, 1"; w) - Figure 2 shows the charge-density susceptibility of the H2 molecule when r’ = (0,0, 0) and w = 0.3858668352248763 a.u. Note that fiw is near (E1 — E0) in the aug—cc-pVDZ basis set. As in Fig. 1, the susceptibility has the general shape of a 0'9 molecular orbital of H2. Again, this is observed because I" = (0, 0, 0) ; since only 0'9 - type orbitals and 29 «type states contribute to x(r, r’; w) for I" = (0,0, 0). Also, although M is near (E1 — E0) , x(r,r’;w) of H2 does not become singular at any r . This is because \111 is a triplet state, and, as we have discussed, triplet states will not contribute to x(r, I"; w) at any frequency, r or r’ value. The charge-density susceptibility of the H2 molecule at r’ = (0,0, 0) and 16 w = 0.4812104263202694 a.u. is shown in Fig. 3. This value of fin) is near (E4 — E0) for the aug-cc-pVDZ basis set. As was the case for w = 0 and w = 0.3858668352248763 a.u., x(r, r’; w) has the general shape of a 09 molecular orbital of H2 because r’ = (0,0, 0) . However, in contrast to x(r, I"; (.0) at w = 0 and at w = 0.3858668352248763 a.u., x(r, r’;w) is singular near w = 0.4812104263202694 a.u. This happens because \114 is a 129 state. Figure 4 shows the charge-density susceptibility of the H2 molecule at r’ = (0,0, +0.07) and w = 0.3858668352248763 a.u., which is near (E1 — E0) . This is the same frequency that was used to calculate X (r, r’; w) as shown in Fig. 2. As was the case for x(r, I"; w) as shown in Fig. 2, x(r, r’; w) is not singular at this frequency, since \111 is a triplet state. However, the shape of X (r, r’; w) in Fig. 2 is different from the shape of x(r, r’;w) in Fig. 4. Whereas x(r, I"; w) as shown in Fig. 2 has the general shape of a 09 molecular orbital of H2, X (r, r’; w) as shown in Fig. 4 resembles a 0,, molecular orbital of H2. This results from the fact that r’ lies on the molecular axis. Recall that when r’ lies on the molecular axis, both 09 and au-type orbitals can contribute to x(r, r’; (.0). Therefore, both 0’9 and O'u-type orbitals contribute to x(r, r'; (.0) when r’ = (0,0, 0.7) , and the overall shape of x(r, r’;w) depends on a sum of products of 09 and an orbitals. The charge—density susceptibility of the H2 molecule at I" = (0, 0, 0.7) and w = 0.4648380650856789 a.u., which is near (E3 — E0) , is shown in Fig. 5. According to Fig. 5, x(r, r’; w) is singular near this frequency. This results from the fact that \113 is a 12,, state, since x(r, r’;w) of H2 at r’ = (0,0, 0.7) is singular for transitions to Eu or 29 states. Notice also that the charge-density susceptibility of H2 in Fig. 5 resembles a 0,, molecular orbital of H2. Again, this occurs because both Ug-type and (Ia-type orbitals contribute to x(r, r’; w) when 1" lies on the molecular axis, but I" 75 (0, 0, 0). 17 1.5 Results of 010,300) Calculations In order to test our calculations of the charge-density susceptibility of H2, we have cal- culated the 01,3012), ayy (w) and azz(w) components of the static and frequency- dependent polarizabilities of the H2 molecule at the CISD level in the DZ, DZP and aug-cc—pVDZ basis sets. Table 2 provides a comparison of the am (w), ayy (w) , and (122 (w) components of the frequency-dependent polarizability 0105 (w) ob- tained by integration of x(r, r’; w) (using the algorithm described here) and by finite-field calculations carried out with the MOLPRO17 quantum chemistry software package. There is excellent agreement between the 01m (w), ayy (w) , and an (w) values calculated here and the corresponding values calculated with MOLPRO”. Figure 6 shows the azz(w) component of the polarizability of H2 in the DZ, DZP and aug-cc-pVDZ basis sets as a function of frequency for various frequencies within the range from 0 to 1.5 atomic units (a.u.). Note that for these calculations, the bond length of H2 was set to 1.40126 a.u. (the equilibrium bond length of the H2 molecule). According to Fig. 6, an (w) in the DZ basis set becomes singular at approximately 0.58 a.u., and azz(w) in the DZP basis has a singularity at approximately 0.57 a.u. In the aug-cc-pVDZ basis set, (122(6)) is singular at frequencies of approximately 0.47 and 0.6 a.u. Figure 7 shows the same data as shown in Fig. 6, however, the range of the (122(0)) values in Fig. 7 is restricted to :1: 200 a.u. We will now explain the singularities of an (w), ayy (w) , and an (an) in the DZ, DZP and aug-cc—pVDZ basis sets in terms of the spin states which contribute to 010300) of H2 and the symmetries of these states. According to Eq. (30), Crag (w) can be written in terms of matrix elements (\I’OI/lal‘I/K) and (WKIugIWO) of dipole moment operators #0 and 1L3 , respectively. Because pa and [Lg are spin independent and ‘110 is a singlet state, matrix elements (\IJOIMQIWK) and . (ll/Klpglqlo) will be nonzero only if the ‘11 K states are singlet states. Therefore, only singlet \I/K’S will contribute to (rag (w) . We can determine which singlet excited states contribute to 010304)) by analyzing 18 the symmetries of the matrix elements which contribue to 0403 (w) . To begin this analysis, consider Eqs. (21) and (30). If Eq. (21) is substituted for [\110) and I‘I/K) , then (103(00) becomes aag(w) = P(a, flea) + P(,3, a, —-w) (36) and P(a,6,w) = Z Z CJ(0)CJ'"(0)0J"(K)CJ'(K) K>0 J,J’,J”,J”’ (‘I’Jlfial‘I’J'>@fllfifll‘I’J'") (37) Ex — E0 — fiw where all quantities in Eq. (37) have been defined previously. According to group theory, the matrix element (@JlfiQIQJI) will be nonzero only if the direct product of the irreducible representations of (DJ , [La , and (by: equals or contains the totally symmetric irreducible representation for the molecular point group. We will determine the symmetries of (DJ, fro, and (by that make (@JIIZQICDJI) nonzero for a=$,a=y,and 0:2. Let us begin by determining the symmetries of (1).], (by, and [12 that make ((PJIfiZIQJI) nonzero when J = J'. Eqs. (21) and (37) indicate that determinants (1)] are contained within the ground state CI wavefunction \I’O . Because all determinants within a CI wavefunction must have the same symmetry as the overall wavefunction, determinants (PJ must have the same symmetry as the wavefunction \I’o. Therefore, since we have required that ‘110 has 23' symmetry (in the D00}, point group), (DJ must also have 2; symmetry. If we let 0;, = - (e 21 + e 22) in <¢Jlfizl¢J> , we have (q’Jlfizlq’Jl = “6(‘1’lerl‘I’Jl — 8 <¢JIZZI¢J>- (38) In the Dooh point group, 2 transforms as Z: . Therefore, the direct product corresponding to either (@JIleqJJ) or ((PJIZQICPJ) is 23' Z: 23' = 2:, which does not equal or contain 23' . Therefore, matrix elements <¢J|fi2|¢Jl) vanish for all J = J’ . Now, let us determine the symmetries of (DJ, (1),]: and [1,; that make ((PJIfiZICPJr) nonzero when J 75 J' . If we let 112 = — (e z1+ e 22) in <¢J|fi2|¢JI> , we have (‘I’Jlfizl‘I’J'l = —6 (q’lellq’J') — 6 ((PJIZ2I‘I’J'l- (39) 19 Let us assume that (DJ: has 2;" symmetry. Since (DJ has 2'; symmetry and 21 has 2: symmetry, the direct product corresponding to either (‘13le1 ICDJI) or (<1) J|ZQICI> Jr) is 23' 2: 2:" = 23' , which is the totally symmetric representation. Therefore, ((PJI/lzICIJJI) will contribute to an (w) when (In: has 2,“: symmetry. Since the excited states ‘11 K that contain (DJ: must have the same symmetry as (PJI , we can also conclude that excited states with 2: symmetry will contribute to an (0.2). If (DJ: has a non-zero projection of the angular momentum along the z axis, (@JlfizICPJI) vanishes. Therefore, only states of 2.: symmetry contribute to azz(w) . At this point, let us determine the symmetries of (DJ, (1)], and fix that make ((PJI/lxICPJr) nonzero when J = J’. If we let [LI : —(e 5131 +ex2) in (Clefixqu), we have (q’Jlfixlq’Jl = -€<J|2:2|J). (40) In the Dooh point group, 1‘ transforms as Hu . Therefore, the direct product corresponding to either (@JI$1|J) or ((DJISL‘QICDJ) is 2; IL, 23' = Hu , which does not equal or contain 23'. Therefore, matrix elements ((1) Jl fiIIQ J!) vanish for all J = J, . Let us determine the symmetries of (DJ, (1),]: and fix that make ((DJIfixICPJI) nonzero when J 75 J'. If we let fix 2 — (6 11:1 + am) in <¢J|fix|¢JI>, we have (‘PJlfixl‘I’J'l = -€<‘PJ|$1|‘I’J'> - 8 (‘I’Jl172lq’wl (41) Let us assume that (DJ: has 11,, symmetry. Since (DJ has 2; symmetry and 1:1 has Hu symmetry, the direct product corresponding to either ((1) J|$1| J') or (CI) J|z2|<1> J!) is 2:11,, 11,, = 23' + 2; + Ag, which contains the totally symmetric representation. The matrix element ((1) Jl 113M) Jr) will contribute to on (w) when (DJ: has HUI symmetry. Since the excited states ‘I’K that contain (1)]: must have the same symmetry as (PJI, we can also conclude that excited states with Hug symmetry will contribute to an (w). Excited states of other symmetries do not contribute. In the Dooh point group, y also transforms as Hu. Therefore, matrix elements ((1) JI [1qu) J) will also vanish, matrix elements (@JlflyIQJI) 20 will also be nonzero when (DJ! has Hug symmetry, and excited states with Hug symmetry will be the only ones to contribute to ayy (w) . In Fig. 7, we see that an (w) in the DZ basis set is singular at two frequencies, approximately 0.58 and 1.47 a.u. We also see that an (w) in the DZP basis set is singular at 0.57 and at 1.43 a.u. For the three basis sets, each of the frequencies where an (w) blows up corre- sponds to a specific (EK — E0) value. In the DZ basis, 0.58 a. u. and 1.47 a. u. correspond to (E2 — E0) and (E7 — E0), respectively. In the DZP basis, 0.57 a. u. and 1.43 a. u. correspond to (E2 — E0) and (E7 — E0). Finally, 0.47 a.u. and 0.6 a.u. correspond to (E3 — E0) and (E10 — E0) in the aug—cc-pVDZ basis set. According to an analysis of the spins and symmetries of states 2 and 7 in the DZ and DZP basis sets, state 2 corresponds to the 112: of H2, and state 7 corresponds to the 212: state of H2. A similar analysis of states 3 and 10 in the aug—cc-pVDZ basis set shows that these states correspond to the 112,: and 212: states of H2, respectively. Figure 8 shows the an (w) component of the polarizability of the H2 molecule in the DZP and aug-cc-pVDZ basis sets as as a function of (.0, where w varies from 0 to 1.75 a.u. Note that the am. (w) component of the polarizability of H2 in the DZ basis set vanishes, since there are no p—type atomic orbitals on either of the H atoms in the DZ basis set. According to Fig. 8, am (w) of H2 in the aug—cc-pVDZ basis set is singular at approximately 0.57 a.u. Figure 9 shows the on (w) component of the polarizability of H2 as a function of w in the DZP basis set, where w varies from 0 to 1.75 a.u. Note that these data were also shown in Fig. 8, however, in Fig. 8, the an (w) scale is too large to show the behavior of an (w) in the DZP basis. According to Fig. 9, the an (02) component of the polarizability of H2 in the DZP basis is not singular within the 0 to 1.5 a.u. frequency range. Only Hu-type states will contribute to the am (on) component of the polariz- ability of H2. The energy ha) of the frequency at which an (w) is singular in the aug-cc-pVDZ basis set corresponds to the degenerate energy differences (E3 — E0) 21 and (E9 — E0). According to an analysis of the spins and symmetries of \Ilg and ‘119, these states are the 111-qu and Ill—lay states of H2, respectively. Transitions to the 1111”: state account for the singularity of am (w). The ayy (w) component of the frequency-dependent polarizability of H2 in the DZP and aug—cc-pVDZ basis sets as a function of w , where 0 S w 3 1.75 a.u., is shown in Fig. 10. Note that the ayy (w) component of the frequency- dependent polarizability of H2 in the DZ basis set vanishes. Fig. 10 shows us that the ow (w) component of the polarizability of H2 in the aug-cc-pVDZ basis set also has a singularity at w = 0.57 a.u. Only I'Iu-type states will contribute to ayy (w) of the H2 molecule. As was the case for the an, (w) , the energy hw corresponding to the frequency at which ayy (ad) has a singularity corresponds to the degenerate energy differences (E8 — E0) and (E9 -— E0). As mentioned above, lIlg and \Ilg in the aug—cc-pVDZ basis are the III-lugc and Ill—lug states of H2, respectively. 22 2 Higher—Order van der Waals Interactions from Perturbation Theory 2.1 Introduction This chapter provides an introduction to intermolecular interaction phenomena and a brief summary of the methods used to calculate these interactions, within pertur- bation theory. In chemistry, the interaction energy Em of molecules A and B is given by Eint : EAB — EA _ EB (42) where E A B is the total energy of the two interacting molecules. Also, in Eq. (42), E A and E B are the energies of molecules A and B when they are separated from one another. In comparison to covalent bond energies, intermolecular interaction energies are weak. Whereas covalent bond energies are on the order of one hundred kilocalories per mole, intermolecular interaction energies range from fractions of kilocalories per mole to kilocalories per mole. Despite the relatively small magnitudes of intermolecular interaction energies, several phenomena are affected by these interactions. Some of these phenomena include the structures and properties of intermolecular complexes, molecular dynamics, solvation, and the behavior of bulk gases, liquids, and solids. This chapter is organized as follows: In Sect. 2.1, we introduce the idea of an in- termolecular interaction energy and briefly discuss the importance of this kind of interaction in chemistry, biology, and physics. In Sect. 2.2, we present the basic quantum mechanical theory of intermolecular interactions. In Sects. 2.3 and 2.4, we present and discuss the polarization and the multipole approximations, respectively. We use Sect. 2.5 to introduce various formulations of the bipolar expansion. Fi- nally, we discuss symmetry-adapted pertubation theory and many-body perturbation theory in Sects. 2.6 and 2.7. 23 2.2 The Quantum Mechanical Theory of Intermolecular In- teractions In the Born-Oppenheimer approximation, the time-independent electronic Schrodinger equation is HI‘I’kl = Ekl‘I’kl- (43) In Eq. (43), H is the Hamiltonian for the system, Nu.) is the exact electronic wavefunction for the kth state of the system, and E], is the exact energy for the kth state of the system. If the system consists of two interacting molecules A and B, then Eq. (43) becomes qulkAB> ”—— EkAqujkAB>3 (44) where \IlkAB and Elena are the exact wavefunction and energy for the kth state of the interacting system. In Eq. (44), the overall Hamiltonian H is H=HA+HB+V, (45) where H A and H B are the Hamiltonians for molecules A and B when they are isolated from one another. The Hamiltonians H X are given by H. = {am-:23:- iEX iEX 06X 1 ”Z. .Tz'j 2,36X,z<] where X = A for molecule A, and X = B for molecule B. Indices i and j run over all electrons in X, and Oz runs over all nuclei in X. Also, (i) V? is the kinetic energy operator for the ith electron in molecule X, Z0 is the charge on nucleus 0 of molecule X, and Tia is the distance between the ith electron and nucleus (1 in molecule X. Additionally, T25 is the distance between the ith and jth electrons in molecule X. The Hamiltonians H A and H B satisfy the time-independent electronic Schrédinger equation Hxlq’zx) = szl‘llzx), (47) with X = A for molecule A, and X = B for molecule B. In Eq. (47), [\Ilgx) is the exact wavefunction for the lth state of molecule X , and E1 X is the corresponding energy of that state. Finally, in Eq. (45), V is the intermolecular 24 interaction operator, which is =;:::Z 36—2:— 76A 6E8 nEB 7€A1 2 25;— + 2 2 -—,. (48> mEA (SEBT 7716.4 7268 mn Indices ’7 and 5 run over all nuclei in A and B, respectively, and m and 77. run over all electrons in A and B. Also, Z7 is the charge on nucleus 7 in molecule A, and Z5 is the charge on nucleus 5 in molecule B. We also use 7'75 to denote the distance between nucleus '7 in A and nucleus 5 in B, rm to denote the th distance between nucleus 7 in A and the n electron in B, and rm; to denote the distance between nucleus 5 in B and the mth th electron in A. Here, Tmn is th the distance between the m electron in A and the n electron in B. When we combine Eqs. (44) and (45), we have (HA + H8 + V) I‘ljkAB) = EkABl‘IJk/IB)‘ (49) Eq. (49) can only be solved exactly for the interaction between a hydrogen atom and a proton. The energy of interaction between two larger systems can be obtained by solving Eq. (49) approximately, using either perturbation theory or variational theory.280 Although variational methods have successfully been used to calculate in- termolecular interaction energies,280 these methods will not be discussed in this work. For the remainder of this chapter, we will briefly discuss various perturbative schemes for solving Eq. (49). For more detailed descriptions of each of the methods mentioned - 9 here, we refer the reader to several rev1ews.7°_73w75 2.3 The Polarization Approximation 2.3.1 Introduction In Rayleigh-Schrédinger perturbation theory, the Hamiltonian for any perturbed atomic or molecular system is H = H0 + v, (50) where H 0 is the Hamiltonian for the unperturbed system, and V is the term that describes the perturbation which is being applied to the system. If we assume that 25 the Hamiltonian in Eq. (49) has the form of Eq. (50), then H A + H B = H 0 in Eq. (49) and we can solve Eq. (49) with perturbation theory. This specific partitioning of the Hamiltonian in Eq. (49) is known as the polarization approximation (PA).69’76’70 In this formulation of Eq. (49), V is the potential of interaction between A and B. When A and B are infinitely far apart, V = 0 and H = H 0 , since there is no interaction between A and B when they are isolated from one another. Let us consider only the ground—state Schrodinger equation for the interacting system. In this case, Eq. (49) becomes (HA + H8 + V) IqIOAB> : EOAquIOAB>' (51) Now, let us derive expressions for the exact ground-state wavefunction and energy of the interacting system. Let us introduce an ordering parameter A into the expression for the Hamiltonian of the interacting system, so that H becomes H =.- H0 + AV. (52) Then, let us expand both ‘I’OAB and E0 A B in a power series in A . When we do this, ‘I’OAB becomes \IJOAB -_- 2 mg, (53) where (n) _1<9"‘I’0 ‘11 11.0... 51—7” M and, E0 A 8 becomes E0... = 2 ”Eli; (55) In Eq. (53), W83; is the nth-order correction to the exact wavefunction for the interacting system, \IJOAB . Similarly, in Eq. (55), E6313 is the nth -order correction to the exact energy for the interacting system, EOAB . Now, let us impose the intermediate normalization condition, so that 011‘“ lWo.3>— —— 1 <56) 0.43 Then, substituting Eq. (53) )for I‘I’OAB) in Eq. (56), we obtain Eva/f owl MAL) =0. (57) n=1 26 Since A 75 0 , Eq. (57) simplifies to 00 201’ 323M219: 0. (58) n=1 If we substitute Eqs. (53) and (55) into Eq. (51) and combine terms of the same order in A , we obtain a system of equations of infinite order. The general form of an equation in this system for a given n is (HA + H8) “1101) > + VI‘IIUL 1)) : EéglJ‘Ifln) >E(1) |\Il(n 1)>+ 0A3 0A3 0A8 EOAB DAB 1 0 + E0123)I‘I’OA)B>+E0A)B|‘I’E)A)B>a (59) (0) where n = 1,2, ...00 . If we multiply each term in Eq. (59) by (\IIOABI and use Eq. (54), we obtain Efnl = (@(0) 0A8 0A8 WWW”). (60) 0A8 The nth -order energy E33; is known as the nth -order polarization energy. The ground state energy for the interacting system is the sum of the nth-order polarization energies for all possible values of n , that is, EOAB: ”2:0 E0203 (61) Also, the n h -order polarization wavefunction (1,01) Bis calculated recursively from (n) n 1) (MG ‘11(n—— k) ‘1’0A3=‘GV‘I’0AB +:Z:::EOBG \IIOAB , (62) where G is the reduced resolvent given by Eq. (19) in Chap. 1. The 1‘“, 2nd and 3rd -order polarization energies have been studied extensively, and their physical interpretations are well understood. In the next section of this chapter, we will present the equations for each of these energies and briefly discuss their physical interpretations. 27 2.3.2 The First-, Second-, and Third-Order Polarization Energies The 13t-order polarization energy is obtained by letting n = 1 in Eq. (60), E‘” =< ‘0) IVIWJL.) (63) 0A3 0A8 We approximate W82; by the product of the exact ground-state wavefunctions \IJOA and ‘IJOB of A and B, so that \Ilffim— _ \IJOAQIOB. (64) Using Eq. (64) in Eq. (63), we obtain EDA):B (66) Using Eqs. (64) and (62) in Eq. (66), we obtain Elli); : —<\IJOA\IJOBIVGV|‘IIOA\IIOB>‘ (67) If we allow excitations of A or B only in Eq. (67), we obtain the induction con- tribution to E323 . The term that arises from exc1tations 1n A can be physrcally 28 interpreted as the polarization of molecule A due to the static electric field produced by B. Similarly, the term that arises from excitations in B can be interpreted as the polarization of molecule B due to the static electric field produced by A. It is important to note that the induction energy does not account for intermonomer elec- tron correlation, that is, the correlation of the motion of the electrons in A with the motion of the electrons in B. When the distance between A and B is such that in- teraction energy is asymptotically approaching zero, the induction energies of A and B can be calculated using the permanent multipole moments and static multipole polarizabilities of A and B. At shorter distances, where the charge distributions of A and B overlap, the polarization propagatorsg‘l’97 of A and B are also needed to calculate E833 . Equations that express the second-order induction energy in terms of polarization propagators are given in references 95 and 187. Distributed multi- pole moments and polarizabilities are often used in calculations of induction energies generated by the interaction of two larger molecules.98“100 However, because the po— larizabilities used in these calculations are non-unique, these calculations are often inaccurate.100 Angyan et. al. have improved these types of calculations by defining distributed multipole polarizabilities so that they are basis set independent, and have also used these polarizabilities to calculate induction energies. 1‘” We obtain the 3rd—order polarization energy by letting n = 3 in Eq. (60), 3 0 2 E5). = (\PSALIVI‘I’EALl (68) Using Eqs. (64) and (62) in Eq. (68), We obtain E631; = (‘I’OA‘I’OBIVGVGVI‘I’OA‘I’OBX (69) where V = V - (\IIOAWOBIVIWOAWOB). We obtain the 3rd-order induction energy in the same way that we obtain the 2nd-order induction energy. When we allow excitations in states of A or B in Eq. (69), we obtain the 3rd-order induction energy as a sum of four terms. The first two terms represent the polarization of molecule B due to the static electric field produced by A and vice versa. The second 29 two terms represent the mutual polarization of A and B by the fields of B and A, respectively. As was the case for the 2nd-order induction energy, the 3rd-order induction energy can also be calculated using the permanent multipole moments and static multipole polarizabilities at large intermonomer distances. At distances where the charge-densities of A and B overlap, the static polarization propagators of A and B are also needed to calculate the 3rd-order induction energy. Moszynski et. al. has derived an expression for the 3’d-order induction energy that expresses this energy in terms of the static polarization propagators of A and B,187 including the quadratic polarization prOpagatorsQ7"1°2‘105 of A and B. We have discussed the terms that arise in the expressions for E3333 and E323 when we allow excitations in A or B only. If we allow simultaneous excitations of A and B in the expressions for E52; and E323, we obtain the dispersion contributions to these energies. The dispersion energy appearing in E533 can be physically interpreted as a consequence of the correlation of the motion of the electrons in A with the motion of the electrons in B. At large intermonomer distances, the 2nd E(2,disp) OAB -order dispersion energy can be calculated from the dynamic multipole polarizabilities of A and B .106 At distances where charge overlap is important, the polarization propagators of 2,d' _. . . A and B are also needed to calculate ESABZSP) .95'107 109 The 3rd -order polarization energy contains terms corresponding to a combined induction-dispersion effect as well as terms corresponding to a pure dispersion effect. Moszynski et. al. have derived an . . . . ' ' 3a. d‘d equation Wthh expresses the induction-dispersmn energy E6142” 23”) in terms of the electron densities and polarization propagators of A and 8.187 In this work, the p) . . 3,d" . . dispersmn energy EéAst is expressed 1n terms of frequency-dependent monomer susceptibilities for the first time. It should be noted, however, that our result is ‘correct only for large distances between A and B, where exchange can be neglected. . ,d' Prev10us attempts to express EéiBzSp) by Chan et. 01.110 in terms of monomer properties were made 30 2.3.3 The Convergence of the Polarization Expansion The convergence of the polarization expansion has been thoroughly studied.1“_125 The polarization expansions for the interaction energies of H-H+ and H-H systems converge. According to studies performed by Chalanski et. al., Jeziorski et. al., and others, the polarization expansion for the H-H+ interaction energy slowly converges to the energy of the 1509 ground state of the system at large H-H+ distances. Addi- tionally, at small intermonomer distances, calculations of the polarization expansion for the interaction energy of two ground-state He atoms carried to high order show that the series is convergent. However, in general, the polarization expansions for the interaction energy of other many—electron systems either converge to energies of unphysical states or diverge. 2.3.4 Summary There are two major advantages to using the polarization approximation to study intermolecular interactions. The first advantage is that the polarization approxima- tion is conceptually simple, relative to other perturbative methods for calculating intermolecular interactions.280 The second advantage, which is more important than the first, is that the energetic expressions which result from these calculations have physically meaningful interpretations, as discussed earlier in this chapter.280 However, there are also several drawbacks to using the polarization approximation to study in- termolecular interactions. One major problem with the polarization approximation is that the unperturbed Hamiltonian H 0 has the wrong symmetry with respect to elec- tron exchange. Although H 0 is symmetric with respect to the exchange of electrons within molecule A or B, H 0 is not symmetric with respect to electron exchange between A and B.72 As a result, the polarization approximation does not account for exchange effects.280 The inability of the polarization approximation to account for exchange effects inspired the development of symmetry-adapted perturbation theory, which will be discussed later in this chapter. 31 2.4 The Multipole Approximation 2.4.1 Introduction Another common method for calculating intermolecular interaction energies is known as the multipole approximation. In the multipole approximation, we express both the intermolecular interaction operator and interaction energy as infinite series in inverse powers of RAB , where RAB is defined as the distance between the centers of mass of A and B. The multipole expansion for the intermolecular interaction operator V in an arbitrary space-fixed coordinate system is 00 Vn V = —'fi, 70 ":2; (RAB) ( ) where Vn is given by280 n—l Vn = Z: Wm—l—l- (71) [=0 In turn, V1,n_1_1 describes the interaction between the 21 instantaneous moment on A with the 2714—1 instantaneous moment on B. When we express the inter- molecular interaction operator V as a multipole expansion in powers of —1— , we RAB can write the interaction energy of A and B as282’284v283 (6.4.03.1?) (12.43)" In Eq. (72), C X (X = A for monomer A and X = B for monomer B) is the Emt (RABa CA, (3,131) N i C" n=1 (7?) Euler angle that describes the rotation of a coordinate system fixed on X with respect to the spaced-fixed coordinate system in which V and Eint (R A B, CA, (3, R) are defined. Also, R = (0, ¢) are the polar angles that indicate the orientations of the molecular axes of A and B with respect to the space-fixed coordinate system. The functions 0,, (CA, (3, R) appearing in Eq. (72) contains coefficients that are called van der Waals constants. In the following sections, we will discuss various formulations of the intermolecular interaction operator, van der Waals constants, and intermolecular interaction energy 32 in the multipole approximation. Finally, we will discuss the convergence prOperties of many of the expansions that we will discuss. 2.4.2 The Cartesian and Spherical Formulations of the Intermolecular Interaction Operator in the Multipole Approximation We can write the multipole expansion of the intermolecular interaction operator as described by Eqs. (70) and (71) in terms of irreducible sphericalm'136 or Cartesian tensorslzil"145 of the multipole moments on monomers A and B. First, we will write the multipole expansion of the intermolecular interaction operator in terms of the irreducible spherical tensors. Let us begin by noting that we will refer to the operator Vn,n_1-1 in the following presentations as a specific form of V1 A1 3 , with L4 = n and l B = n — l — I. The quantities l A and l B refer to multipole moments on monomers A and B, respectively. In the spherical tensor formalism, V; A) B is IA+IB VIAJB = XIA.IB(RAB)_1A_IB_1 Z (-1)m 1731301) fll=—fA—IB X [MIA ® MlBlZ-HB' (73) where X1“ 8 is a constant, and the equation for this constant is Xm. = (—1>’BIISH%. (74) where S is given by S = 2L4 + 2Z3 (75) 21,, In Eq. (73), we also have that 011213 (R) are complex spherical harmonics which are often replaced by real tesseral harmonics.144 We note that equations for the real tesseral harmonics are given in reference 145. The quantities M1 A = m m {MIAA,mA = -lA, ..., +lA} and M13 = {MIBB,mB = —lB, ..., +l3} are multipole moment tensors on A and B, respectively. The M 1:1" and M5328 com- ponents of the multipole moment tensors M1,, and M13 on A and B are given by M133" = 2: 2,7?ch (fp) (76) pEX 33 where X = A for monomer A and X = B for monomer B. In Eq. (76), p runs over all nuclei and electrons in monomer X, Zp is the charge of the pth particle in X ,and Clrzx (fp) is a spherical harmonic. Finally, the tensor product [MIA ® MIBllAHB is [M1A®M,B]}" :5: Z MgAMgBuA,mA;zB,mB|z,m), (77) mA=—1A m3=—IB where (l A, m A; lg, m Bll , m) is a Clebsch-Gordon coefficient, and where we have let lA + l3 2 l.143 Now, let us write the multipole expansion of the intermolecular interaction oper- ator as given in Eqs. (70) and (71) in terms of Cartesian multipole moment tensors on A and B. In the Cartesian formalism, V; A 13 is a l l ,3 V1,, 1...: Z Z M { ”($731M } (78) {a} {5} Here, the M [{Aa} and M123} components of the multipole moment tensors on A and B are M127} : Z Zprp.i1rp.72'-'Tpmxa (79) pEX where X = A and ”y = Oz for monomer A, and X = B and ’7 = B for monomer B. As in Eq. (76), p runs over all nuclei and electrons in monomer X, and Zp is the charge on the pth particle in X. Also, Tp 71,7}, ,2...Tp,.,,x are the Cartesian coordinates of particle 19. In Eq. (78), the tensor T{[l 1:5; is given by TllA-HBl _ (R )1A+lB+1(—1)IA (V V V V v v ) {a},{3} — AB lA!lB! 01 02'” 011A .31 .32'“ .318 x (51;) . (80) Mulder et. al. give general expressions for TE: } Hg; for l A + I}; S 6 in reference 142, and Isnard and co-workers give specific expressions for T{[ AYES; for tetrahedral and linear molecules in reference 246. One can convert between the spherical and Cartesian formulas for V; A.) B using equations derived by Coope et. al.145-148 and Stone 149,150 2.4.3 The van der Waals Constants In this section, we will discuss various methods for calculating the van der Waals functions 0,, CA, (3,11) . We obtain the first expression for 0,, (CA, (3, R by solving the chrodinger equation for the energy of interaction of A and B in Rayleigh-Schrodinger perturbation theory with the normalized Hamiltonian H N , which is H” = H0 + V”. (81) In Eq. (81), VN is a truncated form of the multipole expansion that is given by N Vn V” ZZW’ ‘82) with N = N A + N B , where N A and N B are the total number of electrons in n=1 monomers A and B, respectively. The operator Vn appearing in Eq. (82) is defined in Eq. ( 71). When the Schrodinger equation containing H N is solved, we obtain an asymptotic expansion for the energies of the AB dimer which is expressed in powers of Bi; and contains the van der Waals functions 0'” (CA, (B: R) .112 According to Ahlrichs,160 one can calculate the van der Waals functions 0,, (CA, (3, R) re- cursively. Jeziorski et. al. give the equations needed to perform these calculations in reference 280. We obtain another expression for the van der Waals coefficients by asymptotically expanding the polarization energies E32; as 00 7(3) , ,‘ E12; (......) ~20 5:35?) m=1 (83) Then, each van der Waals coefficient Cm (CA, (3, R) is obtained from Cm (CA, (3,11) = i1: 07)?) (CA, CB, R) a (84) 11:1 where M is an integer whose value depends on whether the interacting molecules A and B are neutral or charged.”0 35 We can also use the standard Rayleigh-Schrodinger perturbation equations of the polarization approximation to write expressions for the C1)? ) coefficients. One obtains these expressions by substituting Eq. (82) for the intermolecular interaction operator into the standard RSPT equations of the polarization approximation. In this approximation, 05,1) (CA,CB,R) and C13,?) (CA,CB,R) are 0.),(CACB, R): <.‘1.IV.I\II.1.> (85> and280 05.?) (CA,CB,R) = 201’ OABleGABVn- kl‘I’ow) (86) kzx where G A B is the reduced resolvent for the AB complex. The expression for G A B is given by Eq. (19) with index K replaced by k, ‘11 K replaced by \I’kAB , EK replaced by EkAB , and E0 replaced by EOAB' Finally, if the interaction energy is known, then the van der Waals coefficients can be computed from 01 (no.3) = jigwR.BE.... (RAM/143.1%.) (87) and 0. (4.. <3, R) = 1. £1300 (12.43)" (E... (RAB, (A, <3, R) n-10.(c.,<3, R) ["1 (88) :1 R(AB) 2.4.4 Removing the Angular Dependence from the Multipole Expansion for the Interaction Energy The irreducible spherical and Cartesian expressions for the interaction energy pre- sented in Sect. 2.4.2, as well as the equations for the van der Waals constants pre— sented in Sect. 2.4.3, are very useful. However, since all of these expressions depend on the Euler and polar angles (A, (B, R , they need to be re—evaluated every time the geometry of the AB dimer is changed. Fortunately, we can also write an expression for the interaction energy in the multipole approximation which separates the depen- dence on (A, (B, R from the rest of the expression for the interaction energy. In this 36 equation, the non-angular part of the interaction energy (which contains the van der Waals constants) depends only on the distance R A B between the centers of mass of A and B, so that this portion of the interaction energy only needs to be re—computed if the distance between monomers is changed. In the polarization approximation, the th equation for the n -order correction to the energy of the interacting system which separates the angular and radial components of the intermolecular interaction energy is A E01132? }€(() )B(RAB) AM) (CA: (3.11) . (89) {A} In Eq. (89), {A}( 507: )B(RAB) is the radial expansion coefficient which depends on the intermonomer distance R AB . Additionally, A{ A} (CA, CB, R) is a function containing the angular dependence of E ( )3 .The equation for this function is L LA LB A{A}(CA,CB,R) = Z Z Z SA'ILDJICfA,KA(CA)* MAL=—LA MB=—L3 M=—L x DMB, BKB(CB) CL (R), (90) where _ LA LB L SML — (MA MB M) (91) is a 3 J symbol,143 Cit/I (R) is a complex spherical harmonic, and Di}: ,KA ((A)* and DiliKe (C3)“ are elements of the Wigner rotation matrix as functions of the orientation angles of monomers A and B.143 References 247, 248, 133-135 and 249 also contain derivations of equations (89) and (90). To obtain this energy in the multipole approximation, we replace the intermolecular interaction operator that ap- pears in the equation for the radial expansion coefficients {Mama (R A B) with the multipole expansion of the intermolecular operator, as given by Eqs. (70) and (71). When we do this, we can write approximations for the radial expansion coefficients {“5823 (R A B) that are determined by the irreducible spherical tensors of the po— larizabilities and multipole moments of A and B33032 Van der Avoird et. al. have 37 reviewed these derivations in reference 75. We will present the equations for the elec- trostatic, second-order induction, and second-order dispersion radial expansion coeffi- cients in the multipole approximation. Note that we will denote these approximations to the exact radial expansion coefficients {“583 (R A B) by {A}(-:0“ )A(R B). The electrostatic radial expansion coefficient8 1n the multipole approximation is {A} (1) _ _ LA (2LA+2LB+1)! EOAB (RAB) — ( 1) 6LA+LBAL (211A)! (2L3)! QK Ang LALA+BB+1° (92) (RAB) In Eq. (92), f: and Q22: are the spherical portions of the 21’" and 2L3 multipole moments on A and B. The equations for Q5: and Q5: are Q5): 5 (‘I’OAIMLAA I‘I’OA) (93) and QK§= — (‘I’OBIMKB B-l‘I’osl (94) In Eqs. (93) and (94), MI}: and Mg: are multipole moment operators of A and B, as defined in their respective molecular coordinate systems. The second-order induction radial expansion coefficient in the multipole approxi- mation i3130,132—135 {A}e( 0.2ind)A):(RB _l§:i§: $32131 21A=1l54=113=0 (RAB) C {A}, {A},md;B (95) 22,0, (RAB) where {A} is a set of indices given by {A} = {L4, :4, [3, 1’3} , and 3?le 00 ’3=0 00 ll 8:1 fi:‘M8 IIM8~ n=lA+lA+lB+l’B+2. (96) Also, C { A} m d A and C { A} m d— B are long-range induction coefficients, where 0"“ is {A}, ind— A {A} L L L OK K C{A},ind—A: €1Ai' 1:13, 00:11.)“ (0) [Q13 ® nglLZ- (97) 38 The long-range induction coefficient for B is given by Eq. (97) with A and B K interchanged. The irreducible product [Q13 ® Q13] L: is given by Eq. (77) with MIA = Q18, M13 2 Ql’Ba m = KB , and 1: LB . The quantity ELALBL 1,151,313; is a constant, given by SLALBL = (_1)lA+l:q (21A + 2Z3 +1)!(2l’A+ 2l’B +1)! §lA (111131;; (2b,)! (213)! (21:4)! (2123)! B x [(2104 'l' 1) (2L3 + 1) (2L + 1)}% x (IA + lB,O; l’A + l’B,0|L, 0). (98) where 1A I; LA I” = ’B 1’3 LB (99) lA+lBliq+123 L is a 9j symbol,143 and (l A + l3, 0; lg + liBi 0|L, 0) is a Clebsh-Gordan coefficient. Finally, 052114) LA (0) is the irreducible spherical tensor portion of the frequency- dependent polarizability on A, 2(E —E ) K H 0A “(113mm (w) = :(E "E 2 2 ”750 nA_ 0A) —w ... .. KA x [(WOAIMIAI‘I’M®<‘I’nA|Mz:,|‘I’oA>]LA (100) with the frequency w = 0. In this equation, WM and EM are the nth excited-state wavefunction and energy of A, respectively. The irreducible product .. ... KA [(WOAIMIAIWnA) <8) (wnAlMlquIOAflL is given by Eq. (77) with MIA = A (\I/oAleAlqlnA), M13 = (\I’nAIMlquloA), m = KA, l = LA. We obtain the equation for the irreducible spherical component of the frequency-dependent polariz- ability on B by replacing A with B in Eq. (100). The second-order dispersion radial expansion coefficient in the multipole approx- 130,132—135 {Me-:33?“ (RAB) = - Z Z Z Z —' imation is (101) with {A} _ 1 L L L K K C{/\},disp — gngigzizg/aufmm (W)a(1§1;3)LB(W)dW- (102) 0 Van der Avoird and co-workers281 have reviewed the calculations of the electrostatic, second-order induction, and second-order dispersion radial expansion coefficients. Since the electrostatic and induction coefficients are determined only by the multipole moments and static polarizabilities of the monomers, it is relatively straightforward to calculate these coefficients.280 However, because the second-order radial dispersion coefficients are determined by the polarizabilities of the monomers at imaginary fre- quency, calculating these coefficients is relatively difficult. To date, these coefficients have been calculated with several different methods, including many-body pertur- 236,251,237,238,240,239 the second- bation theory, order polarization propagator approach (SOPPA),250 and the multiconfigurational time-dependent Hartree-Fock (MCTDHF) 259—2‘” Other methods that have been used to calculate these coefficients technique. are the limited CI technique,244’252 the random-phase approximation (RPA), or the time-dependent coupled Hartee—Fock (TDCHF) approach.2‘“343353354342 2.4.5 The Convergence of the Multipole Expansions of the Intermolecular Interaction Operator and Interaction Energy In general, the multipole expansion of the intermolecular interaction operator as de- fined by Eqs. (70) and (71) is divergent. However, there is a small region of configura- tion space where the multipole expansion of V is convergent. The exact specifications of this region are given in reference 151.230 Like the multipole expansion of the intermolecular interaction operator V , the multipole expansion of the interaction energy is also divergent. Although the divergence of this expansion has only been proven for the H; system,154_156 it is expected that the expansion will also diverge for multi-electron systems. Additionally, Damburg et. (11.158 and Cizek and co-workers159 have shown that Eq. (72) is not 40 summable for H"; using conventional summation techniques,157 so it is also expected that the expansion will not be summable for any multi-electron complexes. Some of the methods used to define and calculate the van der Waals constants also have divergent expansions of the intermolecular interaction energy.280 For example, the multipole expansion of the intermolecular interaction energy that is produced when the Schrodinger equation is solved using RSPT with H N and VN (as defined in Eqs. (81) and (82)) is divergent.280 This divergence results from the fact that VN cannot be treated as a small perturbation, which is a direct consequence of the fact that the spectrum of H N is continuous. The convergence properties of the asymptotic expansion given by Eq. (72) are not well understood. Although researchers have studied the convergence properties of the expansions for the first- and second-order polarization energies, no one has investigated the convergence properties of the expansions for higher-order polarization energies. Jeziorski et. al. have studied the convergence prOperties of the asymptotic 209 and Berns and expansion for the electrostatic energy E61; for the water dimer, co-workers have studied the convergence properties of the same expansion for the N2 dimer.262 The expansions of E3114; for both the water dimer and the N2 dimer converge. However, neither expansion converges to the correct physical value of the electrostatic energy for the appropriate system. Vigné—Maeder et. al have shown that in general, the asymptotic expansion of the electrostatic energy is convergent for any system when Gaussian functions are used to approximate the unperturbed charge distributions of the monomers.263 Again, however, the expansion does not converge to the physical ground-state electrostatic energy of the system of interest. Several researchers‘“‘“"267 have studied the convergence properties of the asymptotic expansion for the electrostatic energy for each of various large molecules using the distributed multipole analysis. Stone has reviewed this method in reference 98. Dalgarno et. 01.268 have studied the convergence properties of the asymptotic expansion for the 2nd-order polarization energy of H; Specifically, they showed that the asymptotic 41 expansion for the 2nd-order induction energy of H; is divergent. Young269 studied the convergence properties of the asymptotic expansion for the 2nd-order polarization energy of the H2 molecule. The author showed that the asymptotic expansion for the 2nd-order dispersion energy of H2 is divergent. We should also mention that neither Dalgarno’s final expression for the 2nd-order induction energy of H; nor Young’s final expression for the 2nd-order dispersion energy of H2 are Borel or Pade summable.157 One might be able to use distributed polarizabilitiesgwm"272 to make these series convergent. To date, however, no one has done these studies. 2.4.6 The Multipole Approximation and Nonadditive Interactions Stogryn273,274 was the first to use the multipole approximation in the study of nonad- ditive intermolecular interactions. Piecuch275 has derived equations in the spherical tensor formalism for the interaction energy of M molecules to any order of pertu- bation theory. These equations are based on Wormer’s perturbation equations in the spherical tensor formalism for the energy of interaction of two molecules.130’132 Piecuch has also derived an expression for the anisotropic induction energy of M molecules through third-order in perturbation theory.63 The author has also used his equations to derive expressions for the isotropic interaction energy65 and anisotropic dispersion energy64 of M molecules through third-order in perturbation theory. Fol- lowing this work, the author derived expressions for the induction energies of M molecules through fourth-order in pertubation theory.276’277 Finally, Piecuch used the equations presented in reference 275 to calculate the nonadditive induction energies of the Arg-HF and Ar2-HC1 systems. We refer the reader to reference 278 for a review of these derivations and calculations. 2.4.7 Summary There are significant advantages and disadvantages of using the multipole approxi- mation to calculate intermolecular interaction energies. Probably the most significant 42 advantage of using the multipole approximation to calculate intermolecular interac- tion energies is that it is easier to evaluate multipole interaction energies than it is to evaluate the corresponding polarization energies. This is because the expression for any particular polarization correction must be completely re—evaluated any time the Euler or polar angles between monomers are changed, while only part of the cor- responding expression in the multipole approximation needs to be re—evaluated when these angles are changed. As discussed in Sect. 2.4.4, we can write the multipole expansion of the intermolecular interaction energy as a product of radial expansion coefficients and angular functions. When one changes the Euler or polar angles be- tween monomers, only the angular functions need to be re-evaluated. Although the multipole expansion of the interaction energy is easier to evaluate than the corresponding energy in the polarization approximation, there are also signif- icant disadvantages of using the multipole approximation to calculate intermolecular interaction energies. The most significant disadvantage of using the multipole ap- proximation to calculate intermolecular interaction energies is that by definition, the multipole expansion does not account for charge-overlap effects. Charge-overlap ef- fects are contributions to the intermolecular interaction energy that are caused by the overlap of the electron density on A with the electron density on B, and these effects are largest when the intermonomer distance is near or below the van der Waals minimum for the dimer. There is another method for calculating intermolec- ular interaction energies that has the many of the same advantages as the multipole approximation, and also accounts for charge-overlap effects. This method is known as the bipolar expansion, and this method is the subject of the next section. 2.5 The Bipolar Expansion 2.5.1 Introduction Another method for calculating intermolecular interaction energies involves using the bipolar expansion for the intermolecular interaction operator. There are several ad- 43 vantages to using this method to calculate intermolecular interaction energies. Like the multipole expansion, the bipolar expansion of the intermolecular interaction en- ergy can be separated into a radial component and an angular component. Also, intermolecular interaction energies computed using the bipolar expansion of the in- termolecular interaction operator include contributions from charge-overlap effects. 2.5.2 The Bipolar Expansion of Buehler and Hirschfelder The exact bipolar expansion of the intermolecular interaction operator proposed by Buehler and Hirschfelder is255v256 00 1< —1— = Z Z .1)ng (r1,7‘2, RAB) Y1? (61, <51) Y,;’" (0342) - (103) mg 1,1,113=0m=—-l< In Eq. (103), T12 is the distance between particles 1 and 2, where particle 1 belongs to monomer A, and particle 2 belongs to monomer B. Also, l< = l A if I A < l B ,and l< = l3 if l3 < (A . The quantities 7‘1, 51, $1 and T2, ég, (52 are polar coordinates of particles 1 and 2, respectively. Finally YIT (81,651) and Ylgm (62, 432) are spherical harmonics defined with respect to particles 1 and 2, respectively. Buehler and Hirschfelder255’256 derived Eq. (103) after assigning coordinate sys— tems to monomers A and B. The coordinate systems that they assigned to A and B have their origins at the centers of mass of A and B, and their z axes are co—aligned. Also, the a: and y axes of the system on A are parallel to the :1: and y axes of the system on B. The :12, y , and z axes in both of these coordinate systems are parallel to the corresponding axes of an arbitrarily selected spaced-fixed coordinate system. Note that we have written Eq. (103) with the notation used by Meath and co—workers in reference 257. Note also that although N g at. (11.257 use Jlljllg (7‘1,7‘2, RAB) in place of the B IIZIIIB (7‘1,7‘2, R A B) quantities used by Buehler and Hirschfelder, these functions are proportional to each other. There are four different expressions for .7);le (7‘1,7‘2, RAB), and the form of 44 this function that we use in Eq. (103) depends on the intermonomer distances of interest. Specifically, the form of J )3; (7‘1,7‘2, RAB) depends on whether we are interested in calculating intermolecular interaction energies for R A B > 7‘1 + 7‘2 , T1> RAB + 7‘2, 7‘2 > RAB + T1, or l7‘1 — 7‘2' S RAB S |T1+ 7‘2'. For RAB > 7‘1 + 7‘2, 7‘1 > RAB + T2, and 7‘2 > RAB + 7‘1, the equations for JIIZL (7‘1,7‘2, RAB) are combinatorial expressions containing l A and [3. Each of these combinatorial expressions also consists of a product of powers of R A 3, 7‘1, and 7‘2, and this product is also multiplied by m. For [7'1 — 7‘2] S RAB S In + ml, the equation for 17):}; (7'1, T2, RAB) is a finite sum of different powers of R A B, 7‘1, and 7‘2. The exact expressions for J 1 A1; (7‘1,’r2, RAB) are given in reference 257. If we neglect the contribution of the JIIA1|B(7‘1,7'2,RAB) functions to i when T1> RAB +7‘2, 7‘2 > RAB +7‘1, l7‘1 — 7'2] S RAB S [7'1 +T‘2I, then i:- reduces to the multipole expansion. 2.5.3 The Fourier Integral Formulation of the Bipolar Expansion We can also express the bipolar expansion of the intermolecular interaction opera- tor in terms of a Fourier transform. In this formulation of the bipolar expansion, 1/7‘12 i8258 i = 1 d3 keik R e—ik-f‘leik-I‘z (104) 7'12 271'2 [(32 Kay and co-workers258 assigned the same coordinate systems to monomers A and B as Buehler and Hirschfelder assigned to A and B. Kay et. al.258 also chose the same laboratory frame as chosen by Buehler and Hirschfelder. In Eq. (104), eik'R, eikrl , and 621°?“ , are given by l A “=2 2 2' %;)—"C“m (k) q;" (k, 1“), (105) with f‘ = R for eik'R, f‘ = fl for 1‘3“"f1 ,and i" = T2 for (and:2 . Note that the equation for eik'f is expressed in terms of the arbitrarily selected spaced-fixed coordinate system. In Eq. (105), the unit vector k = % , and its orientation angles 45 are 6k and (bk . Also, Cl-‘m (R) is a Racah spherical harmonic, and it is given byl43 4w % Ci" (k)-—- (2, +1) Y. (61,0). (106) Finally, the k-dependent multipole operator qlm (10,?) is m .. 2l+1 . q. (k, r>=-(-—— 2),.)01’" (r) 1020. (107) The j) (197‘) quantity contained 1n Eq. (107) is a spherical Bessel function. If we substitute Eq. (105) into the Fourier integral given by Eq. (104) and integrate over 91: and ¢k ,we obtain 1 . - . _ = Z ZlA-lB-J (2] + 1) 21A+18+1 T 12 (MB j kAkB lA!lB! kAL B A x7r(2lA)! (2113!) JAB/41,13]- (CAaCBaR) 00 x fdkj,()kRAqu/1,(k r1)qu (1,12), (108) 0 where we have expressed :1; in terms of the coordinate systems centered on A and B. Also lA l3 ' JAB=(O 0 (3)) (109) The quantity Am};- (C A (B, R) is given by Eq. (90) with {A} = {lA, kA, l3, k3, j} . If we select a space-fixed coordinate system that has R along 2 and replace V in Eq. (60) with Eq. (108), we obtain an expres- sion for the nth-order correction to the energy of interaction of A and B where the angular and radial components are completely separate from each other. 2.6 Symmetry-Adapted Perturbation Theory 2.6.1 Introduction Although polarization theory lends itself to physically meaningful interpretations of each term in the interaction energy of A and B, it cannot be used to obtain quan- titatively correct interaction energies. This is because polarization theory does not 46 account for the exchange of electrons between monomers. This, in turn, is because the . . . 0 . zeroth-order approx1mat10n to the exact ground-state wavefunction W023 v101ates the Pauli-exclusion principle. This problem can be overcome by using A‘Ilggg rather O . . . than @328 as the zeroth-order approx1mat10n to the exact ground-state wavefunct1on of the AB complex, where .A is the antisymmetrizing operator for the system, defined as __ NA!NB! — (NA '1” NB)! In Eq. (110), AA and A3 are the antisymmetrizing Operators for monomers A A AAAB (1 +73). (110) and B. Also, ’P represents the sum of all possible permutations which exchange an electron between A and B, where the appropriate sign factors have been assigned to all permutations. However, since A‘I’gg . is not an eigenfunction of H O = H A + H B , this wavefunction cannot be used as the zeroth—order approximation to the exact ground—state wavefunction in conventional Rayleigh-Schrodinger Perturbation Theory. This problem has lead to the development of several new symmetry-adapted perturbation theories which maintain the definition of H 0 used in polarization (0) 0A8 theory and use A‘I/ as the zeroth—order approximation to the exact ground- state wavefunction of the system. The first formulation of symmetry-adapted perturbation theory (SAPT) was published in 1930 by Eisenschitz and London.161 Other foundational works in this field include those of Murrell, Randic, and Williams;162 Hirschfelder and Sibley;163 Hirschfelder;76'164 van der Avoird;165—168 Murrell and Shaw;169 Musher and Amos;170 Kirtman;172 and Carr.171 We will summarize the most important features of these works here. We refer the reader to several reviews for thorough discussions of these works.72’73’12011731174 In general, there are two classes of symmetry-adapted perturbation theories. The first class of symmetry-adapted perturbation theories include those theories which were developed using weak symmetry forcingm"173 The energy expressions resulting from the development of these theories contain the antisymmetrizing operator A 47 However, the equations used to derive these energy expressions do not contain the antisymmetrizing operator. These theories have been used to calculate interac- tion energies between one-electron as well as many—electron monomers.280 The second class of symmetry-adapted perturbation theories contains those theories which were developed using strong symmetry forcing.175*173 In these theories, the equations used to derive the energy of the system contain the antisymmetrizing operator A . These theories have only been used to calculate interaction energies between one— or two— electron monomers.280 2.6.2 Weak Symmetry Forcing: Symmetrized Perturbation Theories The first kind of SAPT that employs weak symmetry forcing which we will discuss is called symmetrized Rayleigh- Schrodinger (SRS) perturbation theory. 175 In SRS theory, the exact ground-state energy of the interacting system E 5 R3 is the sum of all nth-order SRS energies E011 5 RS) , ESRS (12,8 SR3) Ema-1:: E0 (111) n=0 e e Eéjj‘RS) is given by175’176 ,we) (72 1))-1 (0) ((Jn,SRS) ___ (‘1’ OABIV'AI‘IIOABQ E0,“ SR)S (Howl/“ll 01(3)) (112) AB (1,0)) (0)) AB (1,0)) (0) (‘1’ oABIAI‘I’oAB) (‘1’ oABIAl‘I’oAQ It can also be shown that the nt h-order SRS energy is the sum of the corresponding nth-order polarization energy E6”; and an exchange term EOn’B SR5 cub) ,th at is, ('n,SRS') (,——nSRS arch) EOAB =on8 + EOA’B (113) E(n, ,SRS—exch) The exchange term 0A3 included in Eq. (113) represents the energy resulting from intermonomer electron exchange. The energy resulting from intra- monomer electron exchange is included in E62; . The generalized Heitler-London method IS another weak symmetry forcing method th which expresses the 71 -order perturbation exchange energy in terms of the wave- 48 functions of polarization theory.193 Cwiok and co—workers176 have shown that the generalized Heitler-London energies are equivalent to the SRS energies. The next weak symmetry forcing symmetry-adapted method that we will discuss is called Murrell-Shaw, Musher-Amos (MSMA).169170164 Jeziorski and co-workers17 have shown that the nt h-order correction to the exact ground-state energy Eon’B MSMA) of the interacting system in MSMA theory can be written as E53151...) : (‘1’ 0A)B|A|‘I’0AB> _ 53113634511114)(W3?B|¢:)lnggk'AISM/q)> (114) k=1 (‘I’OABI-AI‘I’OAB) The first- and second-order corrections to the exact ground-state energy of the in- teracting system in MSMA theory are equivalent to the corresponding corrections in SRS theory.280 Higher-order MSMA corrections are not equivalent to the correspond- ing corrections in SRS theory) because the MSMA energies EéjfilSMA) rather than the polarization energies E6: Bare used 1n calculating ‘14)... 2.6.3 Strong Symmetry Forcing: Hirschfelder-Silbey Perturbation The- ory There are two categories of theories that employ strong symmetry forcing. The first category contains what are known as one-state theories,161’16""1‘3‘3‘181’19“_198 and the second category contains what are known as multi-state theories.16‘°’*130’174'1”1199—204 In one-state theories, only one state is included in the perturbation equations in order to account for intermonomer electron exchange and that state is included via the antisymmetrizing Operator $1.280 In multi-state theories, such as Hirschfelder-Silbey (HS) theory,163 all possible states that can be produced by intermonomer electron exchange are included in the perturbation equations.280 Each state is accounted for by the inclusion of the specific permutation operator that gen- erates the state.280 Although one-state theories are significantly less complicated than multi-state theories, one—state theories do not have the correct asymptotic behavior 49 in the intermonomer distance R A B- Speficially, several calculations carried out on H; have shown that energies resulting from one-state calculations do not reduce to the apprOpriate polarization energies at large R A 3.181117312021205fio" 2.6.4 The First and Second-Order Energies in Symmetrized Rayleigh- Schrodinger Perturbation Theory In this section, we will write the specific expressions for the first- and second-order corrections to the exact ground-state energy of the interacting system in SRS per- turbation theory. Then, we will discuss the physical origin of each term in these expressions. If we let n = 1 in Eq. (112), we obtain E(1,SRS) _ (‘1’ 0,31,)IVAI‘IzoAL). (115) 0A8 '— (‘I’OAAIAI‘I’OAB> Then, using Eq. (110) in Eq. (115), we can show that (1, SRS) (1) (ISRS— erch). EOA’B =E0AB +E0A’B (116) In Eq. (116), the exchange term Eg::RS_euh) is given by 011‘” I (V — V) PIW‘O) > E51,]? ,SRS— ezch)_ _ 0A3 0,43 (117) (0) (0) ’ 1+ (‘I’OABIPI‘I’OAB> .(117) represents the largest component of the total exchange energy in SRS theory. Specifically, at the van der Waals minimum, EOI’B SRS exCh) comprises at least 90 percent of the total exchange energy for many molecules.280 Eq. (117) corresponds to the expectation value of the Hamiltonian for the interacting system over the wavefunction “(“1100)” , where AlligB is the wavefunction which accounts for electron exchange between A and B. Jeziorski and co-workers have developed a method for calculating exact values f E(1, ,SRS— —exch) 211 DAB Additionally, by restricting the types of electron exchanges to include single exchanges only, Jeziorski et. al. and Williams and co-workers have (1, h written an equation which approximates E0113 SR5 we ) .2112” Moszynski et. al. 1,SRS— h . . have rewritten the approximation to E's/1,3 we ) 1n terms of the propert1es 50 of monomers A and 3.186 Specifically, they have rewritten the approximation to E(l, ,SRS—exch) 0A3 in terms of the one- and two-particle density matrices of A and B. E(1,B ,SRS— catch) The resulting equations have been used to calculate for various systems.186’73’80 If we let n = 2 in Eq. (112), we obtain the second-order correction to the exact ground-state energy of the interacting system in SRS theory. The expression for this energy is (0 1 E31335): _ Balsam 12.1.4111}; (118) 0) A 0) ' ““3 B (ZSRS) . . . 2 We can separate E0 AB into the second-order polar1zation energy E828 and (2 S RS I an exchange component EOA’B we ”230 (2.5RS) (2, SRS—erch) EOAB =E0j3+ EOAB (119) ‘ ~ (2 S RS ) . . 280 Also, the second-order exchange energy EDA n SRS theory 18 given by (2,—SRS exch) (2,SRS—exch—ind)+ (2 SRS— erch— disp) EOAB ZEOAB +EOAB (120) E(2, ,SRS—exch—ind) 0A8 is the induction contribution to the second-order ex- E32, ,SRS—exch-disp) AB where change energy, and is the dispersion contribution to the second- order exchange energy.280 The exchange—induction contribution Eé2’SRS_exCh—ind) to the second-order exchange energy in SRS theory corresponds to the induction energy that arises when electrons are exchanged between monomers A and 8.280 Williams and co—workers have shown that the second-order induction-exchange en- ergy in SRS theory is a significant portion of the overall induction energy, especially at intermonomer distances R A 3 which are smaller than the van der Waals minimum.78 (2 535— h— (1 Due to the complexity of the expression for EOA’B we in ) , the second- order exchange-induction energy in SRS theory is also difficult to evaluate. How- ever, Chalasinski et. al. have derived an equation which is an approximation to the second-order exchange-induction energy E023 SR3 ”Ch ind) .214 They obtained this approximation by 1gnoring the energetic contributions of higher than single-electron 51 (,——2SRS exch— —2'nd) exchanges to the second-order induction-exchange energy E043 .Chalasin— ski and co-workers have shown that this approximation is valid at and around the van der Waals minimum for the helium dimer.213 Similar calculations need to be per- formed on larger systems in order to determine whether this approximation is valid in a general sense. (,—-2SRS exch— —d23p) The exchange-dispersion contribution E023 to the second-order exchange energy in SRS theory corresponds to the dispersion energy that arises when electrons are exchanged between monomers A and B280 This energy, how- ever, is not a significant portion of the overall dispersion energy. Specifically, the E(2, S RS —exch—d2'sp) magnitude of 0A8 comprises only about a few percent of the . . . . (2 h— d overall d1sper81on energy.280 L1ke the exact express1on for EOA’B SR3 8“ in ) E32, ,SRS—exch—disp) AB 3 the exact expression for is also very complicated and diffi- cult to evaluate. Chalasinski and Jeziorski have also derived an approximation to E(2, ,-—SRS exch— dzsp) 214 DAR They obtained this expression by making the same assump- 2, S RS h— d tion that they made when deriving the approximation to EéA'B we in ). In other words, they ignored the energetic contribution of greater than single-electron 2, S RS h— d . exchanges to E623 “C 1810) .Unfortunately, however, even the evaluat1on of E(2, ,SRS—exch—disp) 0A3 is difficult. This is because the wave- " - - . . 2, SRS— h-d ' functlon used 1n calculatmg the approx1mat10n to E6“ 6“ 13p ) the approximation to must contain charge-transfer terms, 15and it is also because the approximation cannot be simplified so that it depends only on the properties of A and 8.280 2.6.5 The Convergence of the Symmetrized Rayleigh-Schrodinger and Hirschfelder-Silbey Perturbation Theories Several researchers have studied the convergence properties of the SR8 and HS symmetry-adapted pertubation theories. In particular, these groups have studied the convergence properties of SRS and HS expansions for several states and intermolecu- lar distances of H22+ 311,112,175 H2,176’208 and H82.285 The calculations of the convergence 52 properties of H2 and H82 were performed with very large basis sets. Therefore, it is very likely that the results of these calculations are close to the results that would be obtained if an infinite basis set were used. In general, both the SRS and HS perturbation expansions for H; , H2, and H82 converge rapidly.280 However, according to the results of the calculations performed on H; and H2, the convergence of the HS expansion is better than the convergence of the SRS expansion. Also, because the convergence radii for the HS expansions of 208,285 H2 and H82 are similar, it is likely that the HS convergence for H82 will also be better than the corresponding SRS convergence for H82 when expansions are carried out to high order in 72.280 The most important difference between the convergence properties of the SRS and HS theories is that the two expansions converge to different energies.280 While the HS expansion converges to the physically correct energy of the system, the SRS expansion does not.280 If we subtract the energy that the SRS expansion converges to from the correct physical energy of the system, we obtain what is known as the residual exchange energy.‘“"*175 However, according to Jeziorski et. al, the residual exchange energy is so small that it does not affect the accuracy of the SRS method.280 2.7 Many-Body Perturbation Theory 2.7.1 Introduction The polarization approximation, the multipole expansion, and symmetry—adapted perturbation theory are useful theories for calculating intermolecular interaction en- ergies and determining the physical origins of each term in the equations for these energies. If the full configuration interaction (FCI) wavefunctions of monomers A and B are used in the polarization approximation expressions for the interaction energies, the intramonomer correlation effects are accounted for in these energies. However, these wavefunctions are rarely used when calculating these energies. This is because the sizes of these wavefunctions increase very quickly as the corresponding system 53 sizes increase, so that these wavefunctions are impractical to work with for systems in which monomers A and B have more than two electrons. Instead, the wavefunctions of monomers A and B are usually approximated by their corresponding Hartree—Fock determinants. However, if the HartreeFock determinants are used to calculate the in— teraction energies of the system within the polarization approximation, the multipole expansion, or SAPT, then the effects of intramonomer correlation are not accounted for. A new theory has been developed which accounts for intramonomer correlation. This theory is known as many-body perturbation theory (MBPT) or double pertur- bation theory?“218 In double perturbation theory, we assume that there are two perturbations acting on monomers A and B. The first perturbation is the inter- molecular interaction, and the second is the intramonomer correlation. We use the intermolecular interaction operator V which is given by Eq. (48) in the double per- turbation theory equations to represent the intermolecular interaction perturbation. Additionally, we represent the intramolecular correlation perturbation with a second perturbation operator W , where W is given by W = WA + WB. (121) In Eq. (121), WA represents the intramolecular correlation in A, and WB represents the intramolecular correlation in B. In this formulation, the Hamiltonian for unperturbed monomer X is183 HX = FX + WX, (122) where Ex is the Fock Operator for monomer X . To obtain the equations for H A and H B ,we let X = A and X = B in Eq. (122), respectively. Using Eq. (122), with X = A and with X = B in Eq. (45), we obtain H=F“+W“+FB+WB+V 0%) In the polarization approximation, we partition Eq. (123) so that FA + F B = H 0 . Letting FA + FB = F and WA + W8 = W in Eq. (123), we have that H=F+W+V (HQ Now, let us introduce the ordering parameters C and A into the overall Hamiltonian for the interacting system, which is given by Eq. (124). When we do this, H 54 becomes H = F+ = EOABI‘I’OAel (126) If we expand both ‘IJOAB and EOAB in powers of C and A and collect terms of the same power in A , we obtain the following double perturbation theory expressions for the nth -order corrections to the ground-state wavefunction and energy of the AB complex in the polarization approximation,182 \IISAL— _Z \IIOIXB (127) and E532- — 2 E61113. (128) 220 In Eq. (127), @822 is the nth~order correction in V and the ith—order correction in W to the exact ground-state wavefunction of the interacting system. Also, in Eq. (128), E62: is the nth -order correction in V and the ith-order correction in W to the exact ground-state wavefunction of the interacting system. Similarly, we obtain the SRS energy of the interacting system by introducing the ordering parameter C into Eq. (112), expanding this expression in powers of C and A, and collecting terms of the same order in A. When this is done, we find that the nth-order correction in V to the SRS energy is given by178 00 (n, SRS) (n2 SRS) EOAB =2 EOAB . (129) 2:0 In Eq. (129), EéZZSRS) ° 1sthe nth -order correction in V and the ith-order correc- tion in W to the exact ground— state energy of the interacting system in SRS theory. SRS Each E0213 m ) has a polarization contribution EA: m; and an exchange contribution E0722, ,SRS— BexCh)S othat (2 SRS) 2 ) n SRS— I). E0; =on; + E03 ’ “Cl (130) 55 th The total exchange energy for the 72 -order correction to the energy of the inter- acting system is 0,43 0.48 ’ E(n,SRS—exch): _ZE E(m', SRS—exch) (131) ',SRS- h w}... E33; 6“) th- order in V and ith-order in W. is the contribution to the overall exchange energy which is 71.2) Reference 280 reviews the evaluation of the MBPT expressions for EOAB and \I/(ni) in detail.280 The procedures for evaluating these expressions were originally developed by Szalewicz and co-workers182 and also by Tachikawa et. al.219 The eval- E(n2’, ,SRS-exch) 0A8 5 much more difficult than the nation of the exchange energies evaluation of the corresponding polarization energies because the MBPT expressions ' — h . . for EészSRS we ) contam 1ntegrals formed by the overlap of nonorthogonal or- bitals. Therefore, MBPT exchange energies E (m’SRS-—8uh) 0A8 have only been evalu- ated under the assumption that intramonomer correlation has been neglected (that . - . . ',S S— I 1s, 2 = 0 1n MBPT express10ns for E33; R ex“) . 10, S RS I order exchange energy EéAB’ 8“ 1) 211220 (20, SRS— exch— —2nd) 214 Specifically, the first- the second-order exchange—induction energy EOAB and the second-order exchange-dispersion energy 2 ch— d7 . . . . ESAZSRS ex 181)) 214 have all been computed 1n this approx1mat10n. Hi) OAB If we write diagrammatic expressions for the MBPT equations for E( and E(n2', ,SRS—exch) 0.43 , we see that these expressions include disconnected terms. As a result, these expressions scale improperly with the size of the interacting system. By manipulating these equations, one can eventually cancel the disconnected terms. . . 10 IOB,SRS— h Usmg thlS procedure, researchers have calculated E6118)?” E ( we )3“ EOAB E 0A8 ’ EOA ’ EOAB Ema—5123 exch)214 0A8 and It is difficult to manipulate the diagrammatic expressions for the MBPT equa- (122') and E(n2, SRS—exch) tlons for EOAB 0A8 in order to remove the disconnected terms that these expressions contain. Therefore, in order to avoid having to perform these ma- 56 nipulations, several researchers have used CC theory““7’218’223“230 to rewrite the di- agrammatic expressions for the MBPT formulations of the RS and SRS perturba- tion equations.177_179’216 Specifically, Rybak and co—workers have written CC equa— tions for the MBPT formulation of the RS perturbation equations in the polarization approximation.177 Additionally, Moszynski et. al. have derived CC equations that contain only connected diagrams for the first-order exchange energy in the MBPT formulation of SRS theory.178 These authors used the connected CC expansion of the expectation value232 and the single-exchange operator 'P1 to obtain the connected CC expression for the first-order exchange energy. Also, when deriving these equa- tions, they also ignored the contribution of higher than single electron exchanges to the total exchange energym’zm’288 Finally, they used the CC equations for the MBPT (lO,SRS—-e:rch) E(11,SRS—exch) first-order exchange energy to calculate EOAB , 0A8 , and 12’ R _ h - - 1,SR — h E ((321138 S we ) 2 and they used a CC approx1mat10n to calculate E6118 3 exc ).178 Other symmetry-adapted MBPT CC equations have been used to write orbital ex- 10) E611) 12 A3, A8 , and E6213) ,177 and a symmetry-adapted MBPT coupled- (2adi3P) 135 OAB ' Many-body perturbation theory can also be used to derive equations for vari- pressions for E6 cluster approximation has been used to derive a similar expression for E ous components of the interaction energies that express these energies in terms of the polarization propagators and electron densities of monomers A and B. Moszyn- ski and co—workers184 and Moszynski et. al.77 have both derived MBPT equations for the electrostatic energy of interaction in terms of the electron densities and po- larization propagators of A and B. Also, Moszynski, Cybulski, and Chalasinski187 have written MBPT equations for the induction energy of interaction in terms of the electron densities and polarization propagators of A and B, and Moszynski et. al. have derived MBPT equations for the exchange energy in terms of the same properties of the interacting monomers.186 These MBPT equations for the electro- static energy, the induction energy, and the exchange energy can be formulated in terms of Maller-Plesset expansions for the polarization propagators and electron densities 232.287.96.97,102,192 If these components of the total interaction energy are for- mulated in terms of the Moller-Plesset expansions for the polarization prOpagators and interaction energies, then the resulting energetic expressions are called nonrelaxed 57 expansions.280 The MBPT electrostatic, induction, and exchange energies can also be formulated in terms of what are known as relaxed expansions for the polarization propagators and electron densities. The expressions for these energies are called re— laxed expansions.280 In general, for a relaxed expansion of any particular polarization component of the interaction energy in MBPT, Eq. (128) is E(n A,resp) =: Eéjgresp) (132) In Eq. (132), E(n’B Hes}, is the total nth-order relaxed correction in V to the 122,1‘63 . p) 13 the nth-order specified component of the interaction energy, and EOAB relaxed correction in V and the 2t h-order correction in W to the specified component of the interaction energy. 2.7.2 The Electrostatic Energy in Many-Body Perturbation Theory The MBPT expressions for the electrostatic energy in the polarization approximation and in SAPT contain contributions from the intramonomer correlation energies of monomers A and B. Rybak, Jeziorski and Szalewicz have derived an equation for the second-order intramonomer correlation correction E323) to the electrostatic energy in the polarization approximation.177 Also, Moszynski et. al. have derived expres- sions for the third-order and fourth-order intramonomer correlation corrections to the electrostatic energy (given by E3343; and E83 , respectively) in the polarization approximation," given in terms of the nonrelaxed expansions for the polarization propagators and electron densities.96381974023921232 Moszynski and co—workers184 have derived an equation for the second-order relaxed intramonomer correlation correction l2, . . . E321 Brew ) to the electrostat1c energy. Reference 77 also gives equat1ons for the re- E(13, reap) and laxed third- and fourth-order intramonomer correlation corrections OAB E(14,resp) 0A8 derivations of the equations for Eéilga nd E31: r881) ) ,where k S 4 .280 to the electrostatic energy.77 Jeziorski and co-workers briefly review the The same researchers who derived the equations for these intramonomer correla- tion corrections to the electrostatic energy have also used these equations to calculate 58 numerical values of these energies for several different dimers. They have used the results of their calculations to compare the magnitude of the intramonomer corre- lation correction to the electrostatic energy of the dimer to the magnitudes of the electrostatic energy and total interaction of the dimer. Rybak et. al. have used their equation for E512; to calculate the second-order intramonomer correlation correction to the electrostatic energy of the water dimer and of the hydrogen fluoride dimer.177 The results of these calculations show that at or near the van der Waals (12) minima of the dimers, the second-order intramonomer correlation correction EOAB to the electrostatic energy is up to 10 percent of the total interaction energy. This indicates that for these dimers and at these distances, the intramonomer correlation energy is significant, and that one cannot neglect intramonomer correlation when trying to calculate the interaction energies of these dimers. Williams and co-workers have also calculated the 2nd-order intramonomer correla- tion correction E533) to the electrostatic energy of the water and hydrogen fluoride dimers.286 They have also calculated the third-order intramonomer correlation cor- rection E652 to the electrostatic energy of the same dimers.286 Then, by adding E5312; and E523 together, they obtained slightly more accurate estimates of the total intramonomer correlation energy of each dimer. The results of these calculations show that at intermonomer distances which are larger than the van der Waals min- (12) 0A3 18 a much smaller ima, the second-order intramonomer correlation correction E component of the interaction energy for each dimer. Specifically, at the intermonomer distances specified in their work, the total intramonomer correlation energy was only two percent of the electrostatic energy of the water dimer, and five percent of the electrostatic energy of the hydrogen fluoride dimer. Although the intramonomer cor- relation energy of each dimer is a smaller portion of the corresponding total interaction energy at larger distances, intramonomer correlation is still a significant part of the total interaction energy. The authors of this work also computed the relaxed first-, ' - . . 12, 13, th1rd-, and fourth-order intramonomer correlatlon correctlons EéABreSp), ((,ABreSp), 59 (14 ,)resp and EOAB ,for the water and hydrogen fluoride dimers, and they provided an- (12 ,resp) other estimate of the total intramonomer correlation energy by adding EOAB , E(13, ,resp) 0A8 and EOABZTGSP) for each dimer. The results of these calculations were very similar to the results of the calculations of the nonrelaxed energies. Other groups performed similar calculations on the helium dimer and on (H2)2. Specifically, Moszynski and co-workers calculated the second- order intramonomer cor- relation correction Eéllj: and the corresponding relaxed correction E01: Twp) for the (H2)2 dimer.184 They performed these calculations 1n order to determine the con- vergence behavior of the nonrelaxed and relaxed MBPT expansions for the intra- monomer correlation contributions to the electrostatic energy, which are given by Eqs. (128) and (132). They determined how quickly these equations (with n = l ) converge by comparing the values of E623) and Eéizéresm with the electrostatic energy of the dimer as calculated with the FCI wavefunction. According to their calculations, the second-order intramonomer correlation corrections contain only be— tween 50 percent and 70 percent of the FCI correlation energy. Therefore, higher-order intramonomer correlation corrections are large enough that they cannot be ignored in accurate calculations of the intramonomer correlation energy. Moszynski et. al. have also calculated E833) and E011 ’pr for (H2)2.77 However, they have also calculated higher-order intramonomer correlation corrections for this system, includ- ing E033), E612, E833 “Sp dB“: “3”) .77 Additionally, they have calculated Eéilgan dEéilzreSp) where n S 4 for the helium dimer. Then, for each dimer, they computed the sum of Egg) for k S 4 and of EU: Twp) for k S 4 , where the former sum is given by 1 (12 63,33 (4): E0”) + E033) + E0143), (133) and the latter sum is given by 63:21:31)) (4) : Eéliresm+ Eéiiiresp) + E014 resp) . (134) In Eqs. (133) and (134), 6838 (4) and 6(l,resp) (4) denote the sums given in each 0.48 equation. In order to determine the convergence of both MBPT expansions for the intramonomer correlation contribution to the electrostatic energy of each dimer, they (1) compared 60/13 (4) for each dimer to the corresponding total electrostatic-correlation energy. They also compared 6811:8819 ) (4) for each dimer to the corresponding to- tal relaxed electrostatic-correlation energy. The total electrostatic-correlation energy 60 6828 (F C I ) is given by 4,” (F01): —EO“’> (135) EDA)B AB’ 1 . . . . . where E323 IS the electrostat1c energy of the dimer computed Wlth 1ts FCI wave- . 1 . . . . function, and E612 15 the electrostatlc energy of the dlmer 1n the Hartree—Fock (HF) approximation. The total relaxed electrostatic-correlation energy 6(1’r83p) (F01) DAB is given by 6,(1 resp) E(l ,resp) (10.1‘esp) 60,13 (FCI)= EOAB —E0AB , (136) where EOI’B resin) and E0“: Twp) are the same quantities as E323 and E83: , respectively, except that EDA contain relaxed expansions for (,lresp) and E(:0,resp) the polarization propagators and electron densities. When they compared the sum through the fourth-order of the intramonomer correlation correction 61(11):; (4) to the total electrostatic-correlation energy 681,33 (F C I ) for the dimer, they determined that over 90 percent of the total intramonomer correlation energy is included in 6823 (4) . They obtained similar results when they compared 63228810) (4) to 6(1, resp) €0.43 (FCI) for each dimer. These results indicate that the MBPT expansions for the intramonomer correlation contributions to the electrostatic energies of (H2)2 1 and He,» converge quickly, and that for both dimers, 6012(4) an nd €(A’ gap) (4) are very good approximations to the total electrostatic-correlation energies 6012(1'701) and 68:28”) (FCI)77 . 2.7.3 The First-Order Exchange Energy in Many-Body Perturbation The- ory There are two methods for computing the intramonomer correlation contribution to the first-order exchange energy in SRS theory.280 The first method involves using E(l, ,SRS—exch) the approximation to 0.48 developed in reference 73, which is given in terms of the one- and two-particle density matrices of monomers A and B. In order to account for the intramonomer correlation contribution to the first-order exchange energy, the one- and two—particle density matrices originally included in the expression 61 for E(1,SRS—-e:rch) 0A8 in reference 73 are expanded in powers of (.186 The equations for these expansions are given in reference 280. The second method for calculating the intramonomer correlation contribution to the first-order exchange energy in SRS theory is a coupled-cluster singles and dou- bles (CCSD) technique which involves infinite-order summation methods that are nonperturbative.178'235 Jeziorski et. al. briefly review this method in reference 280. Moszynski and co—workers have used the expressions which give the approxima- . (LSRS-exch) tion for EOAB in powers of /\ to calculate the first- and second-order intramonomer correlation . 11,SRS— h 12,SRS— . h. corrections EéAB we ) and E51,; 3 en ) to the first—order exchange en- ergy of H82, (H2)2, He-HF, and Ar-Hg.186 Then, for each dimer, they added these two g::RS_exCh) (2) . In order to determine the convergence of the MBPT expansion for the intramonomer corre— in terms of one- and two-particle density matrices expanded corrections. We will denote the sum of these corrections 6 lation contribution to the lat-order exchange energy of each dimer, they compared _ h . - ' (I’SRS 8x6 ) (2) for each dlmer to the correspondlng total exchange-correlation 0.48 energy eéthS-exch) (F C I ) , which is given by (1,3RS—exch) (1,5RS—erch) (lO,SRS-e:l:ch) 60,3 (FCI) = E,” — E0” . (137) 1,3RS—erch) AB In Eq. (137), E5 is the total 13‘-order exchange energy of the dimer, as 10,SRS—e:rch) computed with its FCI wavefunction, and E3143 is the exchange energy of the dimer as calculated with its Hartree—Fock determinant. Moszynski, Jeziorski, and Szalewicz have calculated the intramonomer correlation correction to the first-order exchange energy in the CCSD approximation for H82, (H2)2, He—HF, and Ar-Hg.178 Jeziorski et. al. list and briefly discuss the results of these calculations. According to the analysis of the convergence properties of the MBPT expan- sion (for the intramonomer correlation contribution to the first-order exchange en- ergy), the convergence of the MBPT expansion is relatively slow. For example, for H62, the sum of the first- and second-order intramonomer correlation corrections €(1,SRS—exch) 0A8 (2) to the first-order exchange energy constitutes only 50 percent of . . l, —, .h the corresponding total exchange-correlation energy 66.1sz e“ ) (FCI) .186 For 62 the H2 dimer, egigRS—exch) (2) is 25 percent larger than the corresponding total (1,3RS-exch) 0A8 exchange-correlation energy 6 (F01) . However, for each dimer, the intramonomer correlation contribution to the lst-order exchange energy computed in the CCSD approximation is around 98 percent of the total exchange-correlation energy 68::RS_exCh) (FCI) . Therefore, the CCSD-based method for comput- ing the intramonomer correlation contribution to the first-order exchange energy is much more accurate than the corresponding MBPT method for computing the same quantity. 2.7.4 The Second-Order Induction Energy in Many-Body Perturbation Theory Moszynski and co—workers have derived an equation for the induction energy that in- cludes an MBPT expansion for the intramonomer correlation energy and depends on the polarization propagators and electron densities of the unperturbed monomers A and 318712321287 This equation for the induction energy can also be written in terms of the relaxed expansions of the polarization propagators and electron (2,2nd) densities.103‘1051188-1‘m’233’234 The induction-correlation energy 60/13 is given by (2.2'nd) _ (2,2'nd) (20.17211) 60” — EOAB EOAB . (138) In Eq. (138), Eggnd) is the exact second-order induction energy, and Eéii’md) is the second-order induction energy in the Hartree—Fock approximation. Similarly, (2,resp-z'nd) the relaxed induction-correlation energy 60” is given by (2,resp—ind) _ (2,resp—ind) (20,7‘esp—ind) 0.3 — Ed... — EDA, , (139) 2, -' d where EéAgeSP m ) (20,1'esp—ind) EOAB proximation. Sadlej has shown that each intramonomer correlation correction E(2l,ind) OAB 191 is the exact second-order relaxed induction energy, and is the second-order relaxed induction energy in the Hartree-Fock ap- (which is second-order in V and lth ~order in W ) can be written as E(2l,ind) : E(2l,ind—a) + Eé2l,ind—t). (140) OAB 0A8 AB In Eq. (140), EWnd") DAB 2(,’ d 21,' d— . . . EéABm ) . Also, E81432" a) is what 18 called the apparent intramonomer is what is called the true intramonomer correlation por- tion 63 . . 21," d . correlation portion of EéABm. ) 191 One can calculate the apparent intramonomer E(2l, ,—2'nd a) (21 d) , ' OAB of EOAB m by usmg the random-phase approx}- . . 2l,'nd in the expresswn for E5“: ) correlation portion 280 mation (RPA) propagator . Jeziorski, Moszynski, and Szalewicz (and references therein) discuss the apparent and true intramonomer correlation contributions to the second-order induction energy in more detail.280 In (2,resp-—ind) summary of their discussion, the relaxed induction-correlation energy €0.43 is a more accurate representation of the second—order induction-correlation energy (2,2'nd) than the corresponding nonrelaxed induction-correlation energy 60.43 Moszynski, Cybulski, and Chalasinski as well as Moszynski et. al. have calculated #227624“) and Eozzares” W” for the He—K+, He-F‘, (H20)2, and He—HCI OAB dimers. 187'“ Note that they did not calculate the first-order relaxed intramonomer 2(1 (1 . . . . correlation energy EOAB reSp m ) because this contribution 18 equal to zero by the Brillouin theorem.280 According to the results of these calculations, the magnitude of E(22, ,resp—ind) 0.43 is very different for each of the different dimers. For dimers . . . . 22, __ d containing a rare gas atom and an ion, the magnitude of E ( "3317 m ) 0A8 is relatively E(22, ,resp— ind) . large. For example, for the He-F‘ dimer, OAB 1S about 10 percent of the 20 d . . . size of E6113 “Sp in ) at or near the van der Waals minimum of the dimer. For 22 d . . dimers containing two polar molecules, Ell/13 res!) m ) is even larger, relative to the E.(20, ,—resp ind) (22 ,——resp ind) OAB EOAB size of .For the water dimer, is about 30 percent 20 d . . . of the size of EéAB res!) in ) at or near the van der Waals minimum of the dimer. Although the authors of references 74 and 93 did not calculate E02: ”Sp and) (22, resp— EOAB and ind . . . ) for any dimers containing a rare gas atom and a nonpolar molecule, E(22, ,resp—ind) Jeziorski et. al. mention that OAB is so small for these types of dimers - - . . 2, d that it can usually be ignored in calculations of E64268!) m ) 64 2.7.5 The Second-Order Dispersion Energy in Many-Body Perturbation Theory In general, there are two ways of writing MBPT expansions for the intramonomer correlation contribution to the second-order dispersion energy in the polarization approximation.280 Rybak and co-workers177 have written completely connected CC equations for the first-order intramonomer correlation correction Eéill’gdiSp) to the second-order dispersion energy. Additionally, Jaszunski et. al. have written the original expression for the second-order dispersion energy in the polarization approx- imation as an MBPT expansion in the intramonomer correlation.231 They did this by replacing the polarization propagators in the original expression for the second-order dispersion energy with MBPT expansions for these propagators. One can also compute the second-order dispersion energy at large R A B if the intermolecular interaction operator V is replaced with the multipole expansion in the MBPT perturbation equations for the dispersion energy. Recall from Sect. 2.4.4 that in the multipole approximation, the second-order dispersion energy is de- termined by the reciprocal of the distance RA B between monomers and the van der Waals constants. In turn, the van der Waals constants are determined by the frequency-dependent polarizabilities of the monomers in the multipole approxima- tion. Jeziorski and co-workers obtained a MBPT expansion for the lth-order intra- . . 2l,dis monomer correlation correction E ( p) 0.48 to the second-order dispersion energy by substituting the expressions for the polarizabilities with the Moller-Plesset expan- sions for these quantities.280 Specifically, Wormer et. al.236_238’240'239 have derived diagrammatic MBPT equations for correlated frequency-dependent polarizabilities, and they have deveIOped another MBPT method for calculating correlated van der Waals constants. Moszynski, Jeziorski, and Szalewicz have developed a method for approximating the long-range second-order correlation-dispersion energy which is known as the ring approximation (RA).185 One obtains the second-order correlation-dispersion energy 65 (2 (1 RA . . . . . . . EOA’B 23p ) in the ring approx1mat10n by replacmg the expressmns for the polariz- abilities in the equation for the second-order dispersion energy with the expressions for the polarizabilities in the random-phase approximation.24434312441242 If one writes the equation for the dispersion energy in the ring approximation in diagrammatic form, the resulting expression that he or she obtains will contain ring diagrams only.185 One can obtain the diagrammatic expression for the dispersion-correlation energy 0A8 in the ring approximation by summing the ring diagrams included 21, d ' ( stp) over all l.185 Note that one can also obtain the (2 ,disp— RA) in each expression for EOA second-order dispersion-correlation energy EOA’B in the ring approximation E52Bld1319) by replacing the polarization propagators in the expression for n the polarization approximation with the expressions for the polarization propagators in the random-phase approximation. 279345 Finally, one can use CC equations derived by (2,d RA Moszynski, Jeziorski, and Szalewicz to calculate E023 23p ) 185 Moszynski et. al. have used CC equations derived in the polarization approxima- (20 dzsp) ,E(21 disp), and E(228 disp) fOI' H82, (H2)2, and (HF)2.185 0.48 Then, for each dimer, they used these results to calculate 653:1”) (2) , which is the tion to calculate EOAB sum of the intramonomer correlation contributions to the second-order dispersion energy through second-order in W. They also calculated the E (22 (kw—RA) and th 0A8 I -order intramonomer correlation corrections where l _>_ 3 to the sum of all the second-order dispersion energy in the ring approximation, which we will denote ' - A . . . 68:28}? R ) (3 -> 00). The equation for this sum is 6(2,disp—RA)(3 __) 00) _2 E021, ,disp— RA). (141) 0.48 According to the results of these calculations, the MBPT expansion for the intra- monomer correlation contribution to the second-order dispersion energy converges rel- (2, disp— RA)( atively quickly. Specifically, for each dimer, the magnitude of 60 3 —+ 00) (2, disp) (2) is very small in comparison to the value of 60 , which indicates that most of the intramonomer correlation energy in included in the first-, second-, and third-order corrections to the total intramonomer correlation energy. 66 3 The Second-Order Correction to the Energy of Two Interacting Molecules A and B This chapter provides a review of known results for the second-order intermolecular interaction energies in the polarization approximation, which is valid when molecules A and B are separated by a distance R A B such that the overlap between their elec- tronic charge distributions can be ignored. If the electronic overlap is non-negligable but A and B interact noncovalently, then the interaction energy can be obtained from exchange perturbation theory. However, the current work is limited to the polariza- tion approximation. Then the second-order correction to the energy of interaction between the two molecules is AEm = (1139,;le G VAB (11(0) ), (142) OAB OAB where IWEBBB) denotes the ground-state wavefunction of the unperturbed system, which we approximate by the product of the ground-state wavefilnctions W833 and 1118:) of molecules A and B, 0 0 O 1111‘ ’ > = 1111511115.) (143) 0A8 In Eq. (142), VA8 is the interaction potential, and G is the reduced resolvent of H 0 = H A + H B , which was defined in Eq. (19) of Chap. 1. For the interaction between molecules A and B, G is a sum of three components, G = GA + G3 + 01423, (144) where (0) (0) (0) (0) GA 2 Z ”’23. ‘I’oall‘l’ja ‘I’oel (145) 0 0 0 0 ’ #0 (E12) + E62) — ( 6A) + E8) 0 0 0 0 0 0 0 0 ’ r790 (E62 + E7852) _ (E62 + E613) and (0) (0) (0) (0) l‘ij ‘Pra><‘1’j,, \Pral (147) GAGBB ___ Z 0 0 0 0 ' 1.1.10 (Egg + Egg) .. (Egg + Egg) 67 0 , . M) denotes the Jth exc1ted state of molecule A, and 4152,) denotes the Tth excited state of molecule B. Similarly, E39) , E53,) , In Eqs. (145), (146), and (147), \II(. E53), and E62) correspond to the energies of molecule A in excited state j , B in excited state 7‘ , A in its ground state, and B in its ground state. Eqs. (145), (146), and (147) are the reduced resolvents constructed when considering excitations in molecule A only, in B only, and in both A and B. In the following, we approximate V in terms of the dipole-dipole interaction and thus we have A AB ... A A B V = —,ua Tag 113, (148) The dipole propagator T03 is defined by l 3 Ra R -- 50 R2 Tag = VQV3E = 612.5 8 . In Eq. (149), Ra and R3 are the a and ,8 components of R, and Va and V3 denote derivatives of R with respect to a and fl , respectively. The full (149) polarization approximation can be recovered by expressing V in terms of polarization density Operators for the interacting molecules and a dipole propagator T (r, r’) integrated over all space with respect to r and I" . Using Eq. (142), (143), and Eqs. (144) - (147), we have A E552. = 4.511.. E (OAminé,OB'fl€lf’B>Wig,“(2‘:me 9'4““) (EL; + E08) - (EDA + E03) 1,11,, 2 <04|fi¢|0430€03mik~3>(mailer(gamma rméo (E0, + Eng) — (E0, + E03) —T76 Tax; 2: (OAllA‘filj/ifjfBlfiafBl(jAlligJO/i)(fofilfiglOBl’ jAJ‘BaéO (E), + Em) - (EDA + E03) (150) where we have let @823 = 0A, @823) = 03, ‘16-? = jA, and @533) = 7‘3, and we have replaced the first and second interaction operators with VAB = —ilf3 7175/1? and VAB = —fif Tap fig, respectively. Because (OAI/ZflOA) . «B B . #130, (OAlué‘IO/d = #240, (OBlfla I03) = #50, and (OBll‘gIOB) = 145° , A0 .7 where p , #240, 11,1530, and #50 are static dipole moments of molecules A and B, 68 we can write Eq. (150) as (0 | A'l | Al0 > 2) A #1 JA) (JA #6 A AEéAB— _ _TVA Tea" ”(1530”? Z< 7 (0) 3:19“) (Em jA —E0A) (OBIfiB ITB> (TBIILB I03) A0 2 6 ¢> 7‘37“) (ETB) — OB ) —T75T€¢ 0 0 37‘ 0 7" 0 x Z ( All/74 7|JA)O() BlfiiJ)B:_ _ T76 Ted) #601150 2 ’7 (0) _ JA9‘90 (E('()) —E0 ,4) 1 (oAmA IJA> _ T... T... #5011130 (2) z 1,, JA9£0 (EjA _EO 0)) 1 (0AM1 IJA>(JA|/1A IDA) — TAM/15011506) Z ( . (152) mm (EA-A -EoA) Interchanging the labels 6 with ’7 and (b with (5 in the second term on the right-hand side of Eq. (152) gives pf": <0A|fi7|JA> (JAMAIOA) O 0 (12.2 A.) 1 <0A|11A IJA>(J'A|fiAl0A> 80 BO 2 7 j/fiéo j _ 1 (DAIMIJAXJAlgA l0A> - T T75AAgOAAc1530 (5):: ) 7 jA7é0 (EjA —E((lA)) l = —T76 Tab M1530 #50 (5) 69 _ T76 Tab #60 (OAlfiflJAlUAlfiflofl Z (A? — E35?) (OAlfifileXjAl/‘y WA) .20 (E13) — Eat?) The bracketed quantity in Eq. (153) is the definition of the static polarizability a X (153) of molecule A. Therefore, we can write the first term in Eq. (151) as >: (OAIfiA lJA) — 796111113011?“ (2): (2A . (155) T3750 (E718) _EOB)) If we interchange 5 with (b and ’7 with 6 in the second term on the right—hand side of Eq. (155), then Eq. (155) becomes (OBIfiB I'rB) half '08) A0 ”A0 6 <15 _ - 7175716451”le E: (E(()) (0)) _ 7'87“) TB — 03 1 (OBI/13 |7‘B>(7‘B|fi§ |03> A0 A0 2 : TB 1 (OBI/AB |:B>(7‘B|;§|OB> _ T057176 #240 ”:10 (2) 2: ¢ 7B7“) (E718) — E03)) 70 1 = —T'76 T“? #240,130 (2) X Z (OBI/lgerXTBl/lglOB) Z (OBIAAAITBX'I'BIAAAWB) men ( E _E(0)) The bracketed quantity in Eq. (156) is the static polarizability (1215322 of molecule B. (156) Therefore, we can write the second term in Eq. (151) as (OBIHB ITB) >(7'Bl#¢ 103) "'T75 Ted) AA‘YOAAG A0 2 = _T75 Tf‘f’ “£0 “:10 (14212) x (é) a215,. (157) Therefore, from Eqs. (151),(154), and (157), the second order correction to the energy of two interacting molecules A and B is 2 l 4E11= — 2262211780115“ (2) 1 A0 A0 B — '75 71¢ #7 :U’e (2) add) — T76 Cred) 2: JA 78750 (OAlfi7 IJA>(OB|#§|TB>(JAI#A |0A> Letting a = (Egg) — E6?) and b 2 (Eg) — E8?) in Eq. (170) and using Eq. (167), we have (E) 7d“) (El-3) - E55?) (E13? — E3?) 2 2 -00 (Elm _ 530’) + 527.22 (E52) — Eff”) + 11%? JA A B = (1.)). 1 + 1 47F (BE? ——E§,‘j} +2710) (E)? —E§,‘jj final) —00 .7 X 1 + 1 (El? — Egg) + zfiw) (El? — Egg); — 2m) 1 = , (171) (Eé-f? — E32?) + (B? — E532) which is essentially Eq. (159). To complete the proof, we will evaluate f du (a/ (a2 + 712)) (b/ (b2 + 712)) C for the case with a = b . Then f (u) is f (u) = (a2 + u?) (a2 + u2)’ (172) and the two singular points for f (u) are u = :taz . However, 0.7 is the only singular point within contour C. Therefore, by the residue theorem, we have a a d = / u<0BIfi§ITB) jATB¢0 _ap >< (JAlfie |0A> X 1 + 1 (0) (0)_ (0) (0) _(E, —E0 zfiw) (EM — EDA +271») 1 1 x + . (180) _ (E3? — E32) — zfiw) (E32) — E32) + zhw) 1 Let us consider the third term in Eq. (180). Rearranging the components of this term allows us to write +00 h A o A _ 1,61... 23 (7;) / dw jAa7'87é0 - «A «B X (JAM |0A>(7‘B|u¢ I08) 1 1 X + L(B33) —E3°— ) m) (133? B—30)+zm) 1 1 + (Em) — E32) — zfiw) (E32) — E3? + zhw) _ 76 +00 ’1 = _T,3:l}3 (47) /dwz J'A7'50 (oimg‘lm'imfloa (orlnfiljmilmoi) 0 O 0 0 (E3) — E3) — zfiw) (EL) — E32 + my) Z <08|fi§|TB> (OBlfifererglOB) (181) .310 (E32) — E3? —zfiw) (E3?) -—E3‘;) +zfiw) Since 0’74, fig, [1? ,and [15 are Hermitian and IOA), I03), IjA) and ITB) are real, (OAlfliflJ'A) = (JAlllfiloA), (OAlfiflJ'A) = (JAIMIOA), (Oslflfer) = (TBIfiflOB), and (Oglfiglrg) = (TBIfigIOB). Using these relationships in Eq. (181) gives +00 71 . . A — T1572) 2 (E) /dw<0A|H§1|JA> JAJBS‘O . «A *3 X (JAIHeIOA> 1 1 x + (0) (0) (0) (O) _(EjA — EDA — 271w) (EM — EDA +zhw)J x 1 + 1 0 0 L (E7)? — E32) — zfiw) (E38) — E38) + zfiw) _ +00 h : _T75Tw5 (Z7?) fab”: -00 jxfiéo (OAlfiflJ'AHJ'AIfifIOA) (OAlflfilJ'AHJAIMIO/i) o o o 0 (E3) — E32 — me) (E( l — E33 + 2211.)) JA 2 (OBlfiferXTB 115103) (OBIfiEIT‘BXTBIfiaBIOB) 38710 (E32 — 3: — zfiw) (E32) — E3? + inw) (182) 77 In order to complete our analysis of the second-order correction to the energy of interaction between A and B, we need to derive expressions for the frequency— dependent polarizabilities (1’74E (w) and 015, (w) of molecules A and B. According to Orr and Ward,61 the first—order polarization P” of an isolated molecule in the presence of an applied field of frequency w is we: (0|P|n> (OIH'wlnManlO) E30) — E30) — hw E30) — E30) + fiw (183) 11790 if damping is neglected. In Eq. (183) In) is an excited (state and I0) is the ground state of the unperturbed molecule, with energies E730) and E (0) .,Also P is a polarization Operator, and H w is the perturbation due to the applied field offrequency w. Ifwe let w— — w, H“) = H’AW = +2417?” and P— — [17, then <11 A>ee _ FA ,3, Z (DAV?4 IJ'A> (J‘Alile |0A> (DAM? IJ'A> (Oelfiglre>] (0)_ (0) (0) TB¢0 ‘_'OBE ZBLU ETB - E08 '1‘ 2% B, (178 B, B with (0) = I03), In) = mg), E30) .—. E32} ,and E3“) = E32,) . Therefore, according to Eqs. (184) and (185), (CAI/LA IJA> 031001) = Z 07 (0)_ mm Eli) EDA h“ (OAl/ie le) E30)— E30) + zhw (186) 78 and (OBlfigerXTBl/lglOB) r3750 EA? — E323) -— zhw (OBlfifer> EB _ Egg; + A. l ' Using Eqs. (186) and (187) in Eq. (182), we have +00 ’1 A . A — TAT... Z (E)/dw<0A|/1§‘IJA> jAJ'BS‘éO (187) X (JAlllflOAXTBl/lgIOB) r - 1 1 E(0) E(0) ’10.} + E(0) E(0) m ( JA — 0A —Z ) ( JA _ 0 +2 )J A +00 11 = _T’75 Tab (21;) [dwafie (w) (1333., (w) (188) Finally, using Eqs. (180) and (188), we can write AEbiL 1 2 ABS/1);; = _ T76 Ted) #630 #50 (5) age 1 .. Te 1;, e30 17:10 (2) e38, f}, +00 — T75 T€¢ (II—7;) / do.) 0;: (W) 05,) (2(4)) . (1.89) The first two terms in AEéi; give the induction energy due to the polarization of each molecule by the field of the permanent dipole of the other (within linear response, and neglecting effects due to the non-uniformity of the field). The third term gives the dispersion energy. 79 4 The Third-Order Correction to the Energy of Two Weakly Interacting Molecules In this chapter, the third-order interaction energy of a pair of moleculesis derived within the polarization approximation. Results for the induction, hyperpolarization, and induction-dispersion energies agree with earlier work, but the third-order disper- sion energy is derived in a new form, as an integral of nonlinear response tensors over imaginary frequencies. 4.1 Non-Zero Contributions to AEéi; Again, we consider two molecules A and B, separated by a distance R such that the overlap between their electronic charge distributions can be ignored. The third-order correction to the emery of interaction between the two molecules is magi; = (xi/(0)3 IVAB G V Bo VA3 130”) (190) O . where ”1828 denotes the ground-state wavefunction of the unperturbed system, which we approximate by the product of the ground-state wavefunctions W823 and A LAB @823) of molecules A and B. In Eq. (190), VA8 is the interaction potential, V is defined by A V B = VAB will IVABhI/(O) ) (191) 0A8 OAB’ and G is the reduced resolvent, given by Eq. (19) in Chap. 1. We split G into a sum of three terms, one with excitation in molecule A only (GA), one with excitations in molecule B only (GB), and one with excitations in both A and B (GA®B), as in Eqs. (145) — (147) of Chap. 3. Here we consider only the dipole—dipole contribution to the interaction potential, which was given in Eq. (148) of Chap. 3. We also have LAB A A O 0 A A 0 O V 2 _HQ T03 H? + (‘I’hA‘I’ ) ‘I’cgglflg T03 #3 mg): @813) (192) Furthermore, since 0 0 A WWI/3:33.31 T 351%,. Web: T 3:3" 350, (193) then . AB V =—il€3 T33 #5 + T33 ufi” #50 (194) 80 In Eq. (194), #20 and [1.50 are the permanent dipole moments of molecules A and B in the a and 5 directions, where the total permanent dipole moments [LA0 and ”BO of molecules A and B are A0 A0“ A0“ A0“ [1 = #2: X ‘I’ fly 3’ ‘I' ”z Z BO 30“ BO“ 80“ 3 = 33X+3yy+3zz (195) and , 5’, and 2 are unit vectors in the x,y and Z directions. If we define -“—_«A_ A0 d;B_AB_ BO #0 _' “a ”a an #6 - ”(B “3 a ‘A—AB A0 V = mTaflfig_ EilTaBI‘BO _ ”a T033113 (196) Using Eqs. (144) - (147) from Chap. 3 for G and Eq. (196) for TA/JB , we transform Eq. (190) into a sum of 27 terms, 15 of which are nonzero. Table 1 contains a list of the non-zero terms and the order of u A0 and H BO in each of those terms. 4.2 Higher-Order Induction: Terms of First-Order in Both ”A0 and I180 The static polarizability 03:}; of molecule A is A _ Z (0.33. I33><33I35AI03> +2 «333. 33333. I03 0.5 ‘ 0) 0) (0) (0 (197) 3.30 E( —E( 3.30 Eh —E0> where IkA) = ‘I’S: is the kth excited state of molecule A. Similarly, for molecule 3, B Z (OBIfivltB>+Z (OBIfi3BItBWBIlivBIOB) - , (198) 0 (0 0 3330 33(3) E(B ) “#0 E(B > _E(B ) 0‘76 — where ItB) denotes the tth unperturbed excited state of B; then (12% GEE is A B _ 056 0’73 _ Z (EME(0)— E(O))1(Et(2)— Em) 0 kg, “3760 [(OAIlte IkA> (CAI/16 IkA> (OAIfi34IkAIIkAIMe IOAIIOBIMBB ItB>I - (199) 81 +++>< Now, let us evaluate each of the (1,1) terms listed in Table 1. From Eq. (148) for the left-hand perturbation operator VAB, VAB = —[2A Tab [Lg , and Eqs. (145), 6 (146), and (147) from Chap. 3, the (1,1) terms 1, 4, 5, 7, 12, and 14 are “ ;A ;B “ — (OAOBIVAB GA 1% T33 #3 GB VABIOAOB> = - Z T03 T75 T63 #530 #240 jAJ'B9éO (OAI/lfiIjA> (jAI/lgIOA> (OBIBSIM (TBIfigIOB> (Elm — E323) (E592 — E3?) ’ JA A 200) — (OAOBIVAB GA #30 T05 fig GAGE VABIOAOB) = " 22 T08 T75 THIS #30 #530 jAJ’B7é0 <03I3§Irs> (OAIfiélIJ'AXJ'AIflfloA) 0 0 0 0 0 0 ’ [(EJIA) — E33) + (E5...) — E33] (E12,) — E62) — (OAOBIVAB GB 32:11.5 35 GA VABlvoB) = A0 80 — X T03 T76 Ted) #7 #3 rBajA¢0 (OBIfl§ITB>UAIfi§I0A> 0 0 0 0 ’ (EIB) — 33;) (E): — E31) A ;A A A _ (OAOBIVAB GB 0 TaB #50 GAmB VABIOAOB> = - X T33 T,5 Ted) #330 111,40 TBJA#0 <03|3§|33><33|3§|03><03l323|jA> (32 — 5:) [(32 - 3:) + (Es-r — 301’ A ;.A A — (0A033VAB 0333 3.. Tag 350 GB VAB|0A03) = — X T333 511,, T... 35" 3f“ jAaTBfi‘éO A 201) (202) (203) 82 (GAMMA)(Ml/130A)(OBIfigerWBIfifIOB) a (204) 0 0 0 0 [(32 — 32) + <32 — 33>] (32> — 3) and A LB ‘ _ (OAOBIVAB GAG”? 33" T0333 0" VABIOAOBI = _ X T03 T75 T605 #30 #31530 jAs'rB9é0 (OAIfifIJ'A)(J'AI/lfIOA)<08Ififlr3> (205) (0) (0) (0) (0) (0 (0) ' (E3 —B.,.,) [(133 ‘E03) + (3... " 03)I Since a, H, ’y, (5, 6, and (15 are dummy variables, we can rename them. If we convert Eto Oz, qb to fi,,3to’7,d to 03,7 to €,and a to 5,termlfrom Eq. (200) becomes — 0,103 VABG'AfiATagfiBGB VAB|0A03 = a [3 — X T67 T60) T03 “(15:0 [1:140 jAaTB9éO (OAIfiijA>(jAI/lglIOAXOBIfifITB)(TBIflgIOB> (0) (0) (0) (0) (EjA - EDA ) (E773 _ E03) In term4 from Eq. (201), we convert (5 to (15,) to 6, 6 to (5 ,and 05 to ’7 (206) to give A L8 513 A — (OAOBIVAB GA #20 Tag/13 GAVE VABIOAOB) = - X T33 Tm T67 #330 #50 J'AJ‘B790 (OBIfigITBXTBI/lflOB)(OAIfifIJ'AlUAI/lisqloxi) (0) (0) <0) (0) (0) (0) ' [(3, - E03) + (E... - 33)] (E3 - E03) Similarly, in term 5 from Eq. (202), we convert ”y to a, 5 to 5, B to ’7, and (207) a to 5 which gives A _“_A AB A — (0A03|VAB GB 3,, Tag 35 GA VAB|0A03) = - X T37 T33 T33 #530 #50 TB .jA7éO 83 <03|3§|r3><33|3§l03>(00334000332403) 0 0 0 0 (E33) — E32) (E32 — E32) When we convert 7to,a, (Ito H, (b to ’7, B to (b, a to 6, and 6 to 5 in term 7 from Eq. (203) we have (208) _ (OAOBIVAB GB 4: Tafi “£330 GAEBB VABIOAOB> = — Z T... T3 T3 350 3:30 TBJA¢0 <03I33I1~B><33I3§I03>0332403033303 0 0 0 0 0 0 ' <3: - 3:) [<32 — 3:) + (Es-2 — 32)] In term 12 from Eq. (204) we convert 6 to a, (b to )8, 5 to 7, B to (b , 03 to 6 and ’7 to 5 ,so that this term becomes (209) A 4A A _ (OAOBIVAB GAGBB #10 T03 #50 GB VABIOAOB> : BO A0 - 2 71.5713 71.33., 3.. 33.73750 (0033403)033003)<03|3§|r3> 0 0 0 0 0 0 ' [(32 — 32) + <32 - 33)] <3: - 3:) Finally, in term 14 from Eq. (205), interchanging (5 and 7 gives (210) _ (OAOBIVAB 0.4333 #20 T06 E133 GA VABIOAOB> = - X T03 T57 Tea“) #20 #31230 jAfl‘BS‘O (0333030333103<03|35I7~B> (0) (0) (0) (0) (0) (0) ° (E3 - E3) [(3. - E3) + (E... - 33)] If we add terms 4 and 7 as specified by Eqs. (207) and (209), we have (211) A _"_B A _ (OAOBIVAB GA #2140 T00 #6 GAEBB VAB|0A03> A _,._A A — (0A03|VAB G330, Tag 350 GA“ VABIOAOB) = - X T03 T37 T63 #230 #50 3.343737“) 84 (OBIM3 ITB>(7‘BIM5 I0B><0AIM. IJ'A) A AA_A_B A (OAOBIVAB GAQBM ACT #3 GA VABIOAOB> ___ A B -Z T073 T677135 ”:0 [1:0 JA 73?“) (OAIMa IJAXJAIMEA IOAIIOBIMB ITBW‘BIM3 I08) (0) (0) ( ) (0) (E.- ... >32 3) B (213) If we replace [CA and t B with j A and 7‘3 in Eq. (199) and then use Eqs. (199), (206), (208), (212), and (213), we can replace the sum of terms 1, 4, 5, 7, 12, and 14 with A0 B00 B SI : _ 0123 T57 71¢ ”a ”’45 066 0’75 (214) Physically, this sum represents a higher-order induction effect: The permanent dipole of molecule A sets up a field that polarizes molecule B, producing a reaction field that acts back on molecule A. Molecule A is polarized by the reaction field due to B; the polarization of A creates a field acting on B, which alters the energy of the pair due to the permanent dipole of B (and similarly, with the roles of A and B interchanged). 4.3 Hyperpolarization: Terms of Third-Order in #30 or 3’40 The static hyperpolarizability 787016 of molecule A is 7‘... Z Z (E‘OI—JEEI:I)1(1~73?—E(°I) k. 1,.an x [(0.1331 13.) (3.13233033. (0.) (OAIMAIkA>(lAIM. IDA) (OAIMaIkAIIkAIM. IlAIIIAIM7 IOA) (DAIM7IkAIIkAIM. IIAIIIAIMCAIOAI +++ 85 A _"_A A + (0A AlkAl A ;A A + (0313241333313.11333133103], (215) where Wu) and HA) are the km and lth unperturbed excited states of term 3 in Table 1. When we evaluate term 3, we have If we convert Converting ’7 to 6, 6 to ’7, 5 to ¢,and (bto 5 in Eq. (217) gives If we convert a X a X (OAOBIVAB GAMA T03 M3 OGA VABIOAOB> = T03 T76 T73 M330 3230 35: Z <0A|M7IJA>(qA|M7 IDA) 3.4.3130 (Eli - E11,.) (E33 - 130,.) (217) (218) to ’7, ’7 to a, H to 5 , and 5 to B in Eq. (218), we have (OAOBIVAB GAHA T75 T/LBO GA VABIOAOB) = Tab T75 Tafi #50 MMO Mg: 2 <0A|M7 IJA> 0 0 JAJIAiéO (EL ) _E(() 21)) (E911)- E023) 86 (219) Converting e to 7, 7 to 6, 5 to 14,45 and (b to 5 in Eq. (219) gives — <0AOB|VABGAfif €¢pfOGAVAB|OAOB)= BO BO BO — 76Te¢TaBl16 #4, W} Z (014mg IJA>< l 0) 0) 0 ’ 334324950 (EjA) — E62) (ECSAL —E(() A?) also, converting a to ’7, ”y to 01, HA to 5 and 5 to fl in Eq. (220),we have —(0A03 IVAB GAfiA an? 00" VAB|0A03)= — Tag 71¢ 22",, u?” #530 #530 X Z (OM/12“ le> (Es? - 352) (E3? — 3?) If we multiply Eqs. (216) - (221) by 1/6, sum the results, and use Eq. (215), the result is (220) (221) 1 —<0AOB|VAB GAH: Tag #3 OGA VABIOAOB>— _ 80—67105 T75 Tap X #5 Ougoufofifae, (222) where we have replaced IkA), HA), Ella) and ES) in (215) with HA), I‘M), E39) and Egg) . Physically, Eq. (222) represents the change in energy due to the hyperpolarization of molecule A by the field from the permanent dipole of molecule B. A similar analysis allows us to write term 8 in terms of the static hyperpolarizability 553W, of molecule B. The static hyperpolarizability fig”) of molecule B is B _ 563(2) “ $21837“) (E§2)_E 30:1) E( 0)_E E(0)) X [ (Oalfifltal(talfifluBHuBlfiEIOw mangle)l . (223) +++++ 87 In Eq. (223), (153) and (21,13) are the tth‘ and um unperturbed excited states of molecule B with energies Egg) and E1303) . When term 8 is evaluated, the result rs — (voglV/‘B GB #30 To), if? GB VABIOAOB) = - afi T76 Teeuéoflfo #50 Z rmsméo (E53,) _ E3?) (Egg) — E5?) When we convert 5 to B, ,3 to (5, a to 'y, and ’7 to (1, Eq. (224) becomes — (OAOBIVAB GB #30 T,5 fif GB VAB|0A03) :- - T76 T as Tax» #30 #20 It?” (224) A LB A Z (OBIMEIT‘BXTBIMISBXSBIHEIOBl 0 o 0 0 73.83350 (EE'B) — E613) (EgB) _ E812) Converting a5 to 5, 5 to qb, 6 to ’7, and 7to 6 in Eq. (225) gives A _A_B A — (OAOBIVAB GB #er T“), [1,), GB VABIOAOB) = A0 A0 A0 _ 60511037175 “6 ”a [1,), Z <03I2§Ir3>(relfifIsBstmfloB) r3,83¢0 (Egg) " Ed?) (Egg) - E3?) If we set B to 6, 6 to B, a to 7, and 7 to a in Eq. (226), we have - (OAOBIVAB GB #50 T6,, fif GB VABIOAOB) = — Teas T75 T05 #410 #340 #30 Z <03I263Im> resaaéo (13(2) — Eli?) (El? - E3?) , and, converting 45 to 6, 6 to (b, e to 7, and 7 to e in Eq. (227) gives — (OAOBWAB GB “:30 T,5 fif GB VAB|OAOB) = — T,5 Teas Tag #340 #240 #20 (225) (226) (227) A ;B A Z (OBlflngB> (TBIW |33> who (Eli? — E62?) (E933 — E3?!) 88 (228) Finally, if we convert B to 5, 5 to B, a to 'y, and ’7 to a in Eq. (228), the result is A _“_B A — (0A03|VAEGE 23071,)”, GEVAE|0A03)= _ TaBTe¢T75II£O “:10 “£0 x Z (OBI/(2|?)=— a 71,, we?“ X Z (0AM,IJ:> (Tel/1,), l08> (E2‘3)E WK Em) E‘“)+ (Em Eé‘élll We can replace 1/ (E53) — E6?) + (El? — E620] in Eq. (231) with an integral over frequencies, (231) [(E(0)_((3))+1 (E(0)_ E320] : (g) +00 X / d“ (59>- 531(3+zhw) —OO 89 1 1 (E52) — E53) — zfiw) 5 (E732) — E52) + zhw) 1 0 0 ’ (E58) ‘ 33 " ml) so that term 2 (as expressed in Eq. (231)) becomes _ (OAOBIVAB GAfifi TaB/Jfi BGAEEB VABIOA OB): — TseTttflztp?°(:— 7)]me (0AM? lJ'A>(CMIJL12‘1 IDA) 0 0) (1352—195?) (E5, — E53 +zhw) + (232) JA QA TB¢0 (CAI/17 IJ'A>(JA|fis|qA><(JA|Ma|€1A><€1Alllié1 IDA) (E5?-- E3”) (E(.0 --E(0 Hm) (OM/11? IJA>(qA|fi€‘ IDA) (Egg? —E(O)) (11*.O ) — E03 — m) M (OBlfiferXTBl/lglow (OBlfiflT‘BX’I‘BIfigWB) (Big) _ E35: + m) (35.2) _ E33 _ 2m) ’ (235) where we have replaced (1A with j A in Eq. (232). Term 13 is _ <0A08|VAB GAeBfi-A “To ”500/1693 VABIOAOB>_ — Z Tag T76 Ta» #50 J'A.qA,r37é0 X (OAlfifIJA>(qufifl0A>(OBIfi?ITB> " [(EJ —Esi:>) + (E? — 32)] x 1 (236) [(1953 E3°))+ (E53? -E33’)]' We can use59 1/ { [(E‘fi-E Es") + (E52 - E326] X [(E‘f? -Eéi?)+ +(E5f22— Emu-_- e 72» 1 + 1 471' _00 (E£0)— E(0) + 2%) (Egg) _ Egg) _ 2m) 1 (133(0) EoA) +212») (Egg) —E0A +212») X 1 (Egon E“”— m) (E(0)— E53) flu) + (237) 91 to write Eq. (236) as _ (OAOB IVAB 0A®B“A ”a To; 3/150 GAGEB VABIOAOB> ___ — 1.105717511053360 h +00 X (a?) / ‘3". Z —oo JA QA TBJéO (0A|H7 |JA>3JA|Ha lqA> (35.?— E38 +zhw) (E3?- E33: + m) (E39,) — E33” + m) (OAIHé1 IJA>3JA|Ha lqA>3€1A|He |0A> (E33,? —E33A’A— 22w) (EV-2-131632%” (E33) — E33) + zhw) + ()0 (0) (0) (E332—13332—zfu) (EjAl— )zhw)— E33 — 3A find) 3 x (ma? Iowan? IrB> : — T0371¢T “yd/1(1) ( 7A,.)ZoodeZ 30A|He IJA>3JA|Ha(|;1A>303|HE|TB> (15:33” —E30)) (E33) —E3A +zfiw) (E33; — E30 +zfiw) JA (IA T3730 <0A|Hf IJA> O O (E E3.)— E32) (E E—33) E30) + zhw) (E33; — E33; —Zfiw) 92 (OAIHE |JA>3JA|Hn IqA>(qA|H7 |0A>303|H§|TB> (E3A — E33) (E32 — E33) —zhw) (E32,)— E30) +zfiw) 1 (E3.0 —E33A)) (E32) — E30) — m) (E732) — E332 — 2m) JA + A . . ;A A A x <07qu IJA>] «239) If we convert (15 to E, B to 05,01 to E and 6 to a in Eq. (238), the result is _ (OAOBIVAB GAEBBfi —A gTe (AugO GA$B VABIOAOB>— _ 71¢T76Ta,3/350(4'h_ 72)me‘2 <0A|H7 IJA><03|H§|m>(J‘BIHfi9 |03> (Em) —E(0) +zth) (E30) —E0A) +zhw1(EqA) —E0A) +zfiw) JA (IA 7‘33‘0 JA > <0A|H7 |JA>< + (E39, —E30) +zhw)A (E3O)E — E30 A—zhw) (E33 —E33A) —zhw) <0A|H7 IJA> (1~37.AE30)—E(37O flan) (E33) — E3A°+zriw) (E33) —E33A)+ziiw) 1 + (Eryn _ EM -777) (Egg _E03 -777) E59 -1339 -777) x <0A|H7 |JA>3 . (240) Expanding Eq. (235) and adding this to Eqs. (239) and (240) gives _ (OAOBIVAB GA HST Tafl Hf? GAoB VABIOAOB> _ (OAOBIVAB GAeaB-AcA-A T03 Hg BGA VABIOAOB> _ (OAOBIVAB GAeeB—A “a T (WAD GAEBB VABIOAOB)_ _ TaflT76R¢u<03IH§|TBI (E3I— E33”) (E32I— E3°I + m) (E733;I — E08 33” + and) 3A OAIHe IJA)3JAIHanA>3OBIH7§ITBXTBIH5 I03 OAIHA IJA><7“(BIH5 IOB 3 I (E3BAI— E33”) (E30I—E E3°I + zhw) (E33?— E38) + zfiw) OAIHA IJ'A>(JAIH:71 Iq AHQAIHA I0A>(OB|H7’5B ITB>3OBIH§ ITB>3€1AIHnI0AI3TBIH5 I03) E733I E3°I BA+zhw) (E33’I— E3AI— 5m) (E32I— 33II— 5m) (OAIH7 IJAI3OBIH§3ITB>3TBIH5 I03) < (EE (my. gym) (5E 55,: +55) (En gum) (° ( E32I— E3°I— 5m) (E33) — E3AI +5555) (E33I — E33) + 52255) 94 1 (E32 — E33AIAI — mu) (E33II — E3°I zfiw) (E333,I — E3°I zfiw) .3. JA A— A— A . . ;A A A A X 30AIH’74IJAI3JAIH5ICIA>3QAIH§I0A>3OBIH5ITB>3TBIHEIOB>3o 3241) Now we will show that Eq. (241) is equal to the product of the frequency-dependent hyperpolarizability 33476 (—w; w, 0) for molecule A and the frequency-dependent polarizability 013533 (w) for molecule B. We can use Eq. (187) from Chap. 3 with 45 converted to 78 to write the frequency-dependent polarizability 01% (w) of molecule B as QB (7w) : Z 3OBIH§3ITB>3TBIHEIOB> 55 Em) E3°I hw T3750 TB — 03 '—Z 3OBIH5|TBI3TBIH§IOB> E33;I — E33? + m (242) Orr and Ward61 have derived an expression for the second-order nonlinear polar- ization Pw" of an isolated molecule due to applied fields of frequencies cal and 3412, Pwa = K(—wa;w1,w2) 11.2 Z m,n7é0 <0IPIm> X (E3?) -— E3°I — m3) (E33II — E30) — 5551) + <0IH'AIm> (E3?) — 3‘” + m2) (E3‘II — E33II + m3) + 3OIH’B2ImI3mI-1-BIH) 3HIH’MI3I) (E333I — E3°I + M2) (E33II -— E30) — m1) = K (—wa;w1,w2) (—h)’2 2 m,n7€0 30|1BI7TE>3mIH7 In>3nIH’w1|0> (E3‘7II — E3°I — m3) (E33II — E33II — m1) 95 + (E(0)_ E(0)_ hug) (E310) _ E30) _ AM) + (OIH’AAImeIH’ |n> (E333I— E3°I + fiw 7) (E33II — E30) + mg) + (OIH’B‘ImeIH |n> (E3?) — E30I + 5551) (E30) - E3°I + hug) + <0IH'AIm> (243) (E39) — E3°I + m1) (E33II — E3°I — m) where wa = 0.)] + tag, and Im) is an unperturbed excited state of the molecule with energy 137(2) . In Eq. (243), K (—w0;w1,w2) is determined by K(—wa;w1,w2) = 2'" X D, (244) where m is the difference between the number of polarization frequencies and field- frequency labels in the set of frequencies w1,w2,..., excluding zero. Also, D is the number of times that the field-frequency labels can be arranged distinguishably, where +0) and —w are distinguishable for all w 75 0 . In addition, 11,2 indicates that a second term should be produced from each term in 13”” by permuting cal and (.02 , and 75 is defined by H=P—mmm. 9%) The quantities HA“ and HI”?- denote the perturbations due to the H11 and tag frequency components of the applied field, and A“) A w A w H’ = H’ — (OlH’ I0>- (246) If we let 13 = #2, col: 2w, L412 — 0 (therefore, wa— — 2w, —wa = w,) H'W— — IfI'AW = #35314”, H’wz = H“ = —5;3FA° H 1 = H ‘ =41, AFAW, and H 2 = -A—’A’0 A A A I . = -EA FAA’O, where H A” is the perturbation when the field FAB" 18 applied to 96 molecule A and IT“) is the perturbation when the field F (‘4'0 is applied to molecule A, then Eq. (243) becomes A E _ FAA“ FAA” (OAIHEIJAXJAlHelqu ”(“940 (Eu) —E0 J—zfiw) (qu1) —E0A) —zfiw) (OAIHE |JA><€1A|HE |0A> E ..Ew) (E593 ..Egg>) (OAIHE IJA>)(E _Ego ME) 0 (CAI/‘7 le>)<3IAllAalOA> (E33) _ E33: + 222:) (E3 3” — E33” + Em) (OAIHQ4 IJA>361A|He IDA) (E3°)— E30) +zhw) (E33 — E33?) Note that we have let K(—wa;w1,w2) = 1, Im) = IjA), In) = lqA), and I0) = |0A>- Now, let us calculate the product of the frequency-dependent (248) polarizability 61% (w) of molecule B with the frequency-dependent hyperpolar- izability £7: (—zw; 2w, 0) of molecule A. According to Eqs. (242) and (248), afflw) a76(- zw;zw,0) is 0133 (w) :3” (—zw;zw,0) = 2: JA GA 73750 (OAIHCA le>(7'BIH§ IOB> (E30) —E30)— 2m) (E39, —E30) flab) (E32) —E33;> ~2m) (OAIHSIJAXJAIH7 IqA>(OB|HE ITBWBIH5|03> 0 0 0 0 (E3A ) — E3A) — zfiw) (E3)— 3A 30))(E3‘; -E3A ) —zfiw) (DEIH:1 IJA>(qE|HaA I0A><03|H3B ITB> (E3°)— E30) (E33) — E30) +zfiw) (E33,; — E30) — Zhw) ( <0A|H7 IJE1>(JEIH:l | E30— E30)+zhw) (E30)— E3 Alarm) (E3; —E30 —zfiw) (OAIHA IJA> E3.°)— E30) (E3? —E30 —zfiw) (E32) —E30)—zhw) (DEIH7IJ'/1>(6114|H2‘1 |0A>3JA|HE lqA>3qA|H7 IOAl3OB|HE ITB)37‘B|HI33IOB> (E30)— E33?- 77w) (E39, —E30)— m) (E 3’) —E30)+zhw) OAIHA IJA>3JA|H7|qA (qAIHA |0EA>3OB|HE ITB)_ E(0)_ 3733) (#0313332) (Em) _E(o> +zfiw) 3 (Eu 30A|HA |JA>3JA|H7 lqA)3qA|Ha 30A)3OB|HE ITB>3TB|HE NE) (E 3’) —E33A’) (E3, E3” — E30 +zhw) (E32 —- E30) +zhw) 3 3 3 + JA 30A|H7 IJA>3JA|H24 IqA>3qAIHA |0A> E3fll— E30l+zhw) (E3? —E3 (2+2hw) (E3°— 3°l+zhw) + OAIHA IJA>3qA|H7 IOA)3TBIHB I03 > E3°)— E(0))(EAA Em) _E(0)_ WA) (E30l— Em)+ +hw) > 30AIH7IJA>3JA|HE7|qA>3€1A|H§1 IOA>3OB|HE ITB>3TB|H§A |OB (E33? — E3A +zfiw) (E39, - E3A) (E33; —E30) + zhw) . (249) Let us return to Eq. (241). If we convert a to ’7, B to 5, ’7 to Oz, and 5 to B in the first, second, sixth, eighth, tenth and twelfth terms in Eq. (241), the result is — (OAOBIVAB GAEA TaE E3 BGAAB VABIOAOB) — (OAOBIVAB GAABEA TOE E3 BGAV ”3|vo ) __ <0AOB|VAB (314633—"1/1’6 T (lb/ABC GAQBB VABIOAOB>_ — TaET7671¢H¢1730 (4h 71’) food“) 2 JA 731A 7‘87“) 30A|HA IJA>3JA|H7 lqA>3qA|Ha IOA>3OB|H¢1§3 ITB>3TBIHE |03) (E30)— E33”) (E30l— E30) +zfiw) (E32) — E33” +zfiw) 30AIHA IJA)3JA|H7|qA>3qA|HA IOA)3OB|HB ITB> (E(-0)-— E30)) (Eq E30) __ E03) +zhw) (E732) __ 30) —zfiw) 99 30A|HA IJA>3JAIHAIOqA>3JA|HanA>3qAIHA I0A>3OBIHE ITB)37'BIHB I03) (E30)_ E30)) (Eq EI—(O) E30) —zhw) (E(B 0)_ E30) _zm) 30A|HA IJEA>3JAIHE IqA>3qAIHA l0A>3qAIHAI0A>303IHA ITB>3TBIHAIOB> E(O)—-— (2+ zhw)A (E(O)— —E00) + zfiw) (E33) — (0) + zhw 30A|HA (:IJAXJAIHAICIAXCIAIHA I0A>303IHB ITB)<7‘BIHB I03) 3 (,7 < > (1232— J+H> < m) 30AIH7 IJA)3JAIHE ICIA)3C1AIH: IOA)3OBIHA3 ITB)37‘BIHE I08) E30)—-— E30— 7m) E3°)—15130l+zhw) E33 —E30)+zfiw JA .3. E3 —E3°— m)(3Efj) —El30)— mat)(E33 —E3°l— >< 30AIH27A|JA>(JAIH:1 IqA)3qA|H7 AIOAXOBIHAITBWBIHA IOB>3 (250) If we assume that the matrix elements of [Ag and [1? are real, then 3OBIH¢BITB) = 3TBIH — (voElvAB GAEBBE‘A TaE E3 BGA VAB|0AOB) _ (OAOBIVAB GA€BB —: T ¢fl¢0 GAGBB VABIOAOB>Z — TaETETAHEOQ-B— )fdwz 30A|HA IJA)3JAIHAI€IA)3(IAIHA IOA)3OBIHE ITB)37‘BIHB I08) (E30I _ E30I) (E32I- E30) + zhw) (E33,? — E33;I + m) JA JA (1A 7‘37“) 30A|HA IJA> (JAIHA IqA> (qAIHA IDA) (OBIHAITB> 3TBIHAIOB> (E30) — E33?) (E30) - E00) + zhw) (E732) — (3):) - zhw) 30A|HA IJA)3JAIHA IqA)3qAIHA IOA)3OBIHA ITBI3’I‘BIHAIOB) (E33II _ E33?) (E32I - E30) — 21w) (E33,;I— —E3°I +zfiw) 30A|HA IJA>3JAIHAIqA>3qAIHA I0A>3OBIHA ITB>3TBIHA I03) (E33II _ E3AI) (E333,I — E33II -- 2m) (E3? — E33,;I — 2m) A 30A|HA IJA>3JAIHanA>3qA(IHA I0A>3OBIHAITB>3TBIHA I03) (E33I E3) (E33II— E3A I+ 2m) (E333I— —E33II +2773») 30A|HA IJA)3JAIHAIqA>3qAIHA IOA)3OBIHAI7‘B)3TBIHB I03) (E3? —E3°I) (E30I — E3A) — 2m) (E33,? E—30I +zhw) 30A|HA IJA>3JAIHA IqA>3qAIHA IOA)3OBIHA ITB>3TBIHA I03) (E333,I —E3°I) (E30 I —E3AI +zhw) (E33,;I — E33;I — 2m) JA 30A|HA IJA)3JAIHAIC1A)3CIAIHA IOA)3OBIH5 ITB)37‘BIHAIOB) (E33I— E3 I) (E33:I — E3AI — 2m) (E33,;I — E33,:I — m) 101 <0A|fi7 IJA) (JAM-3 lqA> (013W? ITBXTBlfifloB) (E332, —E((,O)+zhw)A (E3ol—E33jj +3233) (E 3” E30)+zhw) (DAMS IJA)(JA|#.3|CIA><03|fingBXTB|fiB IOB) (E332- E33” BAHM) (E3.0 —E33]j —zhw) (E30—E E30) —zfiw) (OAII::( IOJA> (JAM lqA> (E32- 32—31233) (E33)— E33: +3133) (E33) —E30) +3133) 1 + (E3332— $32233) (E30— —E33:) —zhw) E30) -—E30)— 3223;) >< (DA/153 le>]. (252) Each term in Eq. (252) is identical to a term in Eq. (249). Therefore, we can write the sum of the (0,1) terms as _ (OAOBIVAB CAI—1*: T033 fifi BOA/638 VABIOAOB> _ (OAOBlVAB GAEBB/l: Tafl fig BGA VABIOAOB) _ (OAOB IVAB GAEBB—A #6 T ”HOG/1633 VABIOAOB>— — T33T73T333§°(4—h 7,) / mfm mm- 73330). (253) Now that we have derived the final expression for the sum of the (O, 1) terms, let us consider the (1,0) terms. When term 6 in Table 1 is evaluated, the result is A LA LB 33 (0303|VAB GB 30, T33 333 GA“ VAB|0303) = —Ta3 71,3 713, 335,30 A ;B . X Z (Oaluglraflralug ISBXSBWfIOBHOAlua |JA>3JAl/13 IDA) JA3TB3SB#0 1 (33 — 32>) [(3:02 - 33>) + (33 — 3377 Using Eq. (232) with qA replaced by J A and TB replaced by SB in Eq. (254) gives x (254) — (OAOBIVAB GB fif T33 71-? 013633 VAB|0303) = 102 h - T06 T75 Ta; H7 0(4—A) (OBIH5 ITBl (TBIHg ISBXSBIHfloBl X d“ (0) <0) (0) 3333;33330 (E8 —E0 3) (E3322 — E08 + 31333) (OBIHB lTB> — Z Tafi T75 Te: ”:10 JA37‘B3339‘90 A .23 A (OBIHcSBlTBXTBlflfl ISB>(SBIH§IOB)<0A|H7 lJA>(JA|Ha|0 A) 0) 0 0 0 [(E3 E‘ l) + (E53 -E5!)l (E33 $93) From Eqs. (232) (with CIA replaced by jA) and (256), .(256) _AT _ (OAOB IvAB GAEBBfi-a T:/3 #3 BGBV VABBIOAO >_ - TaHT75T6¢M240(4— :)Zoodcdtz (OBlHa ITBl (7‘8ng ISB> (JAlHa IOA) ( 0) 0 (EAA -— E3A +2133) (E3A—l E30)— zfiw) JA 7‘3 839390 103 = _ TaHTvéTerbeO('4_ 72)me2 (OBIH5 ITB>3TB|H5 |SB> (SBlH5 I03) 30A|H7 |JA> (JAIH3 IDA) (E3?) —E3 ) (E - E3A +2253) (E33) E—30) +3533) (OBIH5 |;B>3JAIH3 IOA) JA3 7'33 38750 + (E33 E—(O) E3)(E32)— E33 +sz E30)— E33) —zfiw) + (03 |H5 ITBWBIH§|83> 03lH¢|J3><5313315353133103><03|33 IJ3><33|3103>]<>257 Term 15 is 3 ;B 3 — (0303|VAB GAHB 330 T33 33 014393 VAB|03033 =3 _ Z T03 T75 Tab #30 JA3TB3SB#0 x 1 0 0 0 0 0 0 0 0 [(52 - 52> + <52 — 552)] [(5- > — 5:) + (5:: — 52>] 3 .;B A X (OBIHflTBWBIHa |SB><83|H3§|013)(031|H7|J'3) — 52)] 3 [(139—335) (33-3373: (3) _/m 3, 1 + 1 473 (E30— E33” +3533) (E33) —E33A) —zhw) 1 (2+ zfiw) (E32,) — E3? + zfiw) 104 1 + (E33; — 33A) —zhw) (E32) — E33? — 3533) 3 (259) we can write term 15 as _ (OAOBIVAB CA€BBAA AOT 5H3 6034353 VABIOAOB> = - T03T76T5¢H£0(4— JIM: (OBIH5 |TB> + (33>- 353333) “(35- 3 -333) (33g -330>_333) (OBIH5 ITB>383|H§IOB><0A|H7 |JA> X (OBIH5ITB><0A|H7|J'A>3 (260) Now, we will relabel the indices in Eqs. (255) and (260) so that the component of the static dipole moment of molecule A in Eqs. (255), (257), and (260) has the same index in all three equations. Converting ’7 to 6, E to 7, ¢ to 5, andd to (f) in Eq. (255) and expanding gives ,3 ;A _"_B A — (0303 IVAB GB 50 T33 53 03335 VABIOAOB) = _ TaBTech 763% 04(h 71..)Z00j2dw (OBIH5 ITB> (TBIH5 |SB> (SB|H§IOB>(0A|H3 |JA> (JAIH7 |0A> (E30)— E35?) (E33,? —E30) +3755) (E33 — E33? +3533) JA3 TB 389'“) 105 OBI/133ITB> 32>- -3332?” .33: + 33 33> 35,52 _ 333) < <03lfiflr3>(83513I03><03IH£ |JA> :,3.3,?(E—E31~333)(3,?—E33’—mw E3? —E33? +3133) E3 E33?) (E30 —E38— 3133) (E33? — E33? — m) X <08|fi3lTB>30A|H3§|JA>(JAIH’74IOA>] 3261) Converting 6 to 01, a to 6, (Z) to H and ,3 to (25 in Eq. (260), we have _ (OAOBIVAB GAeaB/L A0 T3 3H: GAeB VABIOAOB> : - 71¢T75T05H340(4h7r-)Zodwz (OBIH5 VB) (TBIH5 ISBXSBng IOB) 30A|H7 |JA> (JAlHa |0A> (E33? — E3 ?+zm) (E33; — E3 33? B+zfiw) (E33; — E3 BMW) JA3 T133889“) (OBIH5 (ITBXT‘BIHMSBXSBIHE IOBXOA|H7 IJA> : 106 TafiTeabT 76/33 04('h— 7r_)A:/:sz:dw J3A 7‘33 33790 (OBI/15ITBI:BIfi¢ IOBI<0AIH7 AIJAI<03I337 333333103] (263) Now we will show that Eq. (263) is equal to the product of the frequency-dependent hyperpolarizability 538633 (— -—;w w ,0) for molecule B and the frequency-dependent polarizability CIA (w) for molecule A. We can use Eq. (186) from Chap. 3 with 'y converted to Oz and 6 converted to ’y to write the frequency-dependent polarizability aA( 0’7 w) of molecule A as 30A|HA IJAI3JAIHA IOAI 02732”) Z Z (0) (0)_ ”#0 E-A —E0 zfiw 30A|H7 IJAI3JA|H33|0AI3 . 264 E33’—3’E +3333 ( ) At this point, we will use Eq. (243) to derive the frequency-dependent hyperpo- larizability 3,5363 (—zw;zw,0) of molecule B. If we let P— — pg, (311: w, (322:0 (therefore, wazzw, —wa=— w), H“1 =HIB’W =—[LBF5WB’ , ,3 , A , ,3 _"..’W1 ;'B3w A B 6.23% W = H3,” = —33 Ff”, H = H = :35 E33“, and H = -A—,B’0 A B A I H = —-]Z¢ F f ’0, where H BAA" is the perturbation when the field Ff’w is applied to molecule B and H [B ’0 is the perturbation when the field F f ’0 is applied to molecule B, then Eq. (243) becomes W _ FB’O F333 2 3OBIH3 ITBI37‘BIH5ISBI3SBIH5 IOBI B TB,SB¢0 (E53) — E62) '_ Iliad) (E83) _ Egg) — 73%) 4B ,3 3OBIH33I7'BI37'BIH6 ISBI 38BIH§I0BI (E33’— E33?— 3733;) (E33’ —E33?) 30BIH5I7‘BI37‘BIH3153ISBI35BIH3IOBI (E30I__ E30I) (E30I_ E30) +73%) 108 (OBI/15B IT‘BXTBlfi-e |SB> (E3? — E3: +zh:) (E3? — E30) + m) (OBIH5 |7°B>(7‘B|fig ISB> (SEW? IOB> (E3? — E3: ) (E30) — E3? — zfiw ) (OBlfiB ITBWBIIZelSBXSBlfiB |03) (E3? — E3: + zhw) (E§?E — 3‘?) = Ff’OFaB’wfi%¢(—w;w,0). (265) Therefore, from Eq. (265), the frequency-dependent hyperpolarizability of molecule Bis (OBIMEB ITB> — E30 — 21w) (E3? — E3‘? — zhw) [856(1) ("W3 W: 0) Z Z (EBB?) T333750 (Ogle? |;B> (E3‘?— E3?) (E3? — E38 — zfiw) + (OBll‘gerXTBll—ifiISB> (266) (E3? —E30 Hm) (E3 “’) —E3‘?) Note that we have let Im) = |7‘B), In) = [33), and l0) = I03). Now, let us calculate the product of the frequency-dependent polarizability 034,7 (w) of molecule A with the frequency-dependent hyperpolarizability 311396 46 (—zw; 2w, 0) of 109 molecule B. According to Eqs. (264) and (266), (1A3 (2w) B55365) (—zw; 5w, 0) is e27 fl535<—w:wa0> = Z JAJ‘B @3550 ;B A (OBlfie |TB><0A|H5 IJA) (Ml/1’731 |0A> (EB E(0)— E330 33—2111») (EB: — Em) — 275w) (E30) — E33) — zfiw) OBI/3B |7‘B)(:B|#5ISB)<0A|#5 |JA> 30A|fi5|JA33JA|fi7 IDA) E? —E3‘33 3) (E3? — E323 +5155) (E323 — E323 - zfiw) (OBlfigerWBlm |SB> (SBlugloBXOAl/Ie lJA> ;B 03|fl5 |TB> <0A|fi7 |JA> (E3‘? —E3‘333— z m)(E323—E323—zm) (E323 —E3 23+sz) ( 05mg |T3><0A|fl7 IJA>< (SBIHE I03) (OM/17 IJA) (SEW; ICE) 30Alfl7 IJAXJAIfie IDA) (E3? —E33‘33 + 555;) (E323 — E323 + zfiw) (E323 — E323 + 255;) 110 (OB |H5ITB3< 3 _ (OAOBIVAB GAGBB-lifi T053 fiflB BGB VABIOAOB> _ ____ _ TafiTe¢T75 “:10('4_ 72>]:de (OBIH5 ITB3 5,3»)(5 553-55 (553 533555 + (OB IH5 ITB3 _ (OAOBIVAE GAeB—fu T5571? 303 VAE|0A08> _ (OAOBIVAB (3751533324 ESGAeB VABIOAOB> : " T557155T76H240(4— 7:)()/oo:w_2 (OBIHBIT‘B337‘BIH5ISB3_5 55m -55 (55.5? 5533 55 0B 3OBIHB ITB>3TBIHZEISB>3ESBIH§ IOB330A IH 5IJA33JAIH7 I0A3 (E (2)—E(0))(E323 —zfiw (EBB—E E30) —zfiw 0BIH5BI7"B337‘BIH5ISB33E8B:IH,153I0B330AIH7IJA33JAIH5I0A E323— E323) (E323— E323 + 555 E‘23— (23+zhw OBIHB ITB33TBIH5 ISB33 0B330AIH gIJA3-333JAIH7 IOA 3 3 3 3 3 3 (E323— E323) (E323—E E323 +2552 3—555) 3 3 3 3 3 OBIHB I;B(337‘BIH5ISB3:BIH 5BIOB330 AIH7 IJA33JAIH5 I0A3 E323— E3‘333)(E323— —zfiw (E‘23— E323 +555 3 30B IH5 ITB337'BIH5 I8B338BIH5 I0B330A IH5IJA33JAIH7 I0A E5, “33 —E323) (E323 E323 — 5755; E“? — E323 — 555; 3 3OBIH5B I7'B3 7‘BIH5ISB33SBIHBIOB330AIH, IJA33JAIH§ I0A3 3A E3) E30) + zfiw) 8(E3g) — E32) + 231w) (E323—E (2+ zfiw 3 3° 3OBIH5 I7'B3 3"‘BIH5 I833 3SBIH5BIOB330AIHBIJA3 3JAIH5 I0A3 (E303 —E323 +5552) B(E323 - E323 - 555) (E323E — E323 —zhw 3 3 JA 3OBIHB ITB3 3TBIH5 ISBXSBIEBB IOB330AIH5 IJA3 3JAIH7 I0A3 E‘3 —3—E32 5555) E323— El,‘,‘333+2m) (E ‘33 E323+m) JA + 3 E‘—‘33E3‘33—zh5e) (E323-131323—2m) (E323— 323- 3 JA x 5515555555518555155IOB>55152555553105](270) Each term in Eq. (270) is identical to a term in Eq. (267). Therefore, we can write 113 the sum of the (1,0) terms as _ (OAOB “/1413 03%: Ta fiufi BGAEEB V:BI0AOB> — (0,403 IVAB GA‘BBJ ya Tag 57315 BG'BV ABIOAOB) _ (OAOBIVAB GAGBB I135 A0 n¢— #43) BGAQB VABIOAOB> = +00 ’1 '— T033 THH T75 ”:10 (In?) / dw 035117 (w) figd) (-290; w: 0) ' (271) 4.5 Third-Order Dispersion: Terms of Order Zero in Both #540 and “BO In this section, we derive a new expression for third-order dispersion energies as integrals of nonlinear response tensors over imaginary frequencies. When we evaluate term 11 in Table 1, the result is —30AOBIVAB GAEBBfi: T30 ’13 BGAQEB VABIOA083— " T03 T76 Tab :3 jAaQA57‘85337é0 1 [(5:2) - .55) + 55 - 55)) [(523 - A?) + (52> — 55)) X 30AIH7 IJA33JAIH5I€1A33QAIH5 I0A3 X (OBIfiaITB337'BIHBISB33SBIHL¢IOB3° 32723 Replacing q A with j A in Eq. (232) and using Eqs. (232) and (272), we have _ (OAOBlvABGAG9B—QTB a Bufi BGAEBBvABIOAOB)_ _ —Ta,’3 T75 cred) 1 X Z 0 0 0 JA59A TB SB¢0 [(E3/1) _E( A))+ (Ea: -E(() 12)] X 30AIH7 IJA33JAIH5 IqA33qAIH5 I0A33OBIH5 I7‘B337‘BIH5 I8B335BIH5 I0B3 +00 x (43) / dw 1 + 1 7‘ (E33-2) — E33) + zfiw) (E33-3) - E33) — zfiw) —OO 114 1 1 + (ESQ — 133? + zhw) (Efi? — E3?; — 2m) Replacing T3 with 83 in Eq. (232) and using Eq. (232) in Eq. (273) gives _ (OAOBIVAB GAGBBfia —AT Ta 3,1,3 BGAGBB VABIOA OB>_ _Taa T75 71¢ X Z (0AMIJ:>(JA|#a|qA)(qA|/1€ IDA) jA quJ‘BaSBSéO A ;B A X (OBlflgerXTBl/IgISB>(SB|/1§IOB> (273) +m I x (1679) fdw ZOO dw 1 1 X (0) (0) + (0) (0) _(EjA — EDA +zhw) (E3-A — EDA — zhw)‘ , - 1 1 X 0) (0) + (0) (0) (EfiB — E08 + m) (Em — E08 — zhw) F H 1 1 X 0) (0) + <0) (0) (E131 — EDA +zfiw’) (EM — EDA — mm) X 1 + 1 (Egg) — Egg) + my) (Egg? — Egg) — mm) = —Tafi T76 Ted) A . . ;A A Z J'A.QA.TB,SB¢0 A $.13 A X (OB|#§|TB><83|I£§|08> 1 X (16—7272)_Zo(1§dw E(,O)+zhw)(E§2)—Eé:)+zhw) 1 jo oodw(E(.°— E5 0)+zhw) (Efi2)—E3‘;)—zhw) 115 1 +OO_Z(E dw — E3?—m) (Efig)—E53)+zhw) 1 _Z(E dw —E00— m) (E72) —E(§:) —zfiw) A _fw dw’ 1 (E53 — .3) +zhw’) (ESQ — E33) +zhw’) 1 (__ZOdJO; (50) _E00 )+zfiw’) (E58) —E00)— zhw’) 1 +_/000:0E1dw,( ”7 —E<3— —zfiw’) (E 0) —E33)+zhw') 1 j. ..., (Em) — E00) A—zhw’) (ES) — Egg) —- zhw’) We can use the properties of the integrals in Eq. (274) to reduce the number of terms. (274) Inoo the integral f:dw1/[(EJ(-?—Eég)+zfiw) (E£2)—Eé:)+zfiw)] , let w = —77 and w=—m, 71.1 = 3+ zfiw) (E52 — E33) + zfiw) JA 1 +/00 (Em) — E33) -— zhn) (E723 — E62) — zhn) 1 _Z( dw E30“ —E33)— 2m) (E72’—E33’—zhw)' (275) 116 Similarly 7w 1 = -00 (E313) — E53) + #1.») (E53) — E33) - 277w) 1 dw . (276) .../o (El-3) - E63) - zfiw) (E72) — E33.) + W) This means that we can write the w-integrals in Eq. (274) as 1 _Z(E dw - O)+ zfiw) (E12) -— E33) + zhw) 1 + _Z( dw Egg)— E03) + zhw) (ESQ —E(§:) — zfiw) + / dw 1 (E3-3) —E(§3)— 2717.)) (Elm— E33)+zhw) 1 + _/ 01d.»(E(3_ —E33)—zhw) (El37—E53Lzhw) 1 = 2_/00( dw EJlO)- 0)+ zhw) (E72) — E33) + zfiw) 1 + 2 [(E dw . (277) —E03’ + m) (E13) — E33) — zhw) Similarly, we can write the sum of the w’ integrals as 777 1 (E(g)— Em) + zhw’) (ES. 0) —Eé:) + zfiw’) 1 (”_ZOOdwi (Em) — E0 (0) + zfiw’) (ES. 0) — E62) — zhw’) 117 1 + _/00 dwl(E537— E537 flax) (E..— 07— 537mm) + Z dw' 1 (E537— E537 — 27w) (E537 — E537 — 27w) 1 = 2 f... 7,7 _00 (E53)E — 0)+ zhw’) (EQ— 3:) + zhw’) + 2 / dw' 1 -00 (E537 — E537 + my) (E537 — E537 — 27w) Using Eqs. (274), (277), and (278), term 11 becomes (278) — (OAOBIVAB 07473 7‘2"T.,fi.3 074673 VABIOA 0.): —T.,T..T.. X E «147723 |7A><7A|7ta ICIA> jA,qA,TB.SB¢0 A 2.3 A X (OBlltfsBlTBWBl/tg ISB> 1 (4:2) _ZO( dw 3507 _E537 +271.) (E537—E537+zm) 1 + jo idw(E537- E537 + zhw) (E5. “77 —E537—zrw) / 77’ 1 _00 (E53) — E63) + zhw’) (EQ— E30) + zhw’) / 77’ 1 _oo (E537 — E537 + 271.7) (E537 — E537 — 27w) +00 7 —-:_>7dw 77>:de 118 JA (IA 7‘3 83750 30A|M71 IJA) (E337 — E337 + zfiw) (E337 — E337 + 27171;) A ;.B A (OBIMSBITBWBIMg I83) <88|M§|OB> X E337 — E337 + 27w) (E337 — E337 + 7777/) <07|M74lj7>(7'71IMQ|7177><7‘B|M73|5>‘B><7‘>‘7B|Mqli3 IOB> E337 —E337 +2777) A33(E7 —E337 —zhw’) 30A|M7 IJAXJAIMQ lqA> E337 — E337 + 27717) A(E337 — E337 + 27717) (DAIMA le> E337 — E337 + 271w) (E337 — E337 — 2m) (OBlMa ITB>3 I378) (E337 — E337 + 77717) (E337 — E337 -— 27w) (279) When factored, Eq. (279) is A LAT ;B 7 A _ (OAOBIVAB GAEBB“ T10!3 ”B GAEBB VABIOAOB> +w < 2777 7°72 (OAIMA IJA>+7)(72 - - 77) 253‘” 7 :73 7 7 37357 (Ml; _w0'9 w2) : 30A|Ma|JA73JA|M7 lqA73qA|M:A IOA7 00 go 0 17376 (7771; w2, —w0) = 30A|M7 |7A739A|H¢ 70717 (2817 Then M2377(- -wa;w1,w2) = b277—( wa;w1,w2)+b§‘70(-wa;w2,w1) 120 + b27377 (W1; —w0', LL12) + bayg (3‘01; W29 —LU0) + b17460 (7122; —wa, 7.721) + bf,“ (7172; w1, —w3) ,(282) Similarly M555 3—wa;w1,w27 = b37335 3—wo;w1,w27 + b5673(_w0;w27w1) + 175756771; —wa,w2) + b557, (7771; 7772, -wa) + ban (7172; —w0,w1) + b33333, (w2;w1, —wa) .(283) I If we let 77.71: 2712 —w and (712: w in Eq (282), then wa = wl +012 = w , and b: (wwr_w _WI) 2 Z 30A|M7|JA73JA|Ma|qA7 QC ’ 2 0 7,472,770 (E777) — E77,, + zhw) 3QA|M2A |0A7 (E33) — E03) + zfiw') (284) Similarly, when we let 011 = w —zw and 7712:qu for molecule B then 7170 = wl + (.722: w, and AB , 7 0 IABIT 737' I— IS 7 B . __ 3 B M5 8 B M B b53777 (”Aw ”AA—Aw) — Z (0) <0) r3.337é0 (ETB _ 08 +27%») 33377325703) (E337 ——E337+ zhw') (285) Comparison of bme (w; w), — 2w,— —zw’) with the A term in Eq. (280) indicates that the (O, 0) term, as specified by Eq. (280), contains b33106 (w); w, - w, —w'). Also, examination of bggq, (w; w, — w, —w ) in Eq. (285) and the first B term in Eq. (280) indicates that the (0,0) term contains bggé (2w; zed, — 2w, —zw') . If we let wl 2 —2w' — w and tag = w in b533, (w2;w1, —wa), then wa = —zw' and AB 0 IABIT 737‘ l_ 75 7 B . , , _ 3 8M5 B 3M5 B b57347 (“A—“‘3 _w’w) _ Z (0) <0) r3,33¢0 (Era " E08 +2501) 121 x 3SB|M7€3|07 . (286) (E337 — E32) — zhw') Inspection of Eqs. (280) and (286) indicates that b53377 (2w; —zw’ — W, 27.12,) is the second B term in Eq. (280). When we let an = 7712' + M and bag = —-zw in b35367 (7172; w1, —w0), then wa = w, and aB ’ 7 0 AB 7‘ T‘ — 3 777 (7272 +2.22) 2 E: < 77737 77071771 A 7.8958750 (ETB _ E08 _ 2’10!) <83|M§|037 (E32,) - E32) + zhw') (287) Examination of Eqs. (280) and (287) indicates that ()5?ch (—zw; w), + w, —zw') is the third B term in Eq. (280). When we let (.01 = w - 7,7,7), and 0.72 = -—zw in b333, (w2;w1, —wa), then tag 2 —2w' and A LB 3 7 7 303|M§3|TB73TB|M73 ISB7 A533" (_A‘A A” _ A” ’3’“) = Z (0) (0) rasméO (Era - E03 — 7’53“”) s O 3 BIMB l 7 3 (288) (E337 -E337 — 271717) which is the last B term in Eq. (280). Therefore, from Eq. (280), _ (OAOBIVABGAQB-LATO fifiBGAGBBf/ABIOA OB) ___ — 7107371767171) (Al—h” 2—2)Zood3ad -ZOObA(dCUI 706 (W;W,—W,—Zw’) x [b§5¢(w;zw— w—roouu) b533, (2w; —zw — 7,117,270,) +++ bffid, (—zw; 77.77, + 174—7717,) B 37537 ( —w; w —— 2w], AAA/)7 . (289) 122 Consequently, using Eqs. (214), (222), (230), (253), (271), and (289), we have 3 MS; +++ _ A0 30 all B _ T03 T57 71¢ #0 ”go acts 07,3 1 6 T03 T75 72¢ MEG/160M?) 31015 1 6 T03 T75 Tap Ma 0M7 0M6 A0 508 3gb T03T36Twp50(3_1h_ 7r.)Zodwa§3(zw) €a3(— 2w;zw,0) ’1 T03 T63, T35 #240 (_) ZOO dw a; (w) 3553, (—zw; zw, 0) Tax? T76 Ted) (4: :) fodw Zo'dw b3a€( 2w; 2w, — tug—2412') [b68603 (14mm — w, —w) b53333 (w); —zwl — w, w’) b35333 (—zw; w, + w, —zw’) bgw —zw; 2w — w’, WIN . (290) 123 5 Numerical Estimates of the Second- and Third- Order Corrections to the Interaction Energy of Two or Three Hydrogen Fluoride (HF) Molecules for Various Geometries 5.1 Leading Contribution to the Second-Order Correction to the Interaction Energy of Two Molecules According to Eq. (189) in Chap. 3, the second-order correction to the energy of interaction ABS/24; of molecules A and B is 2 1 ABS/RB Z _ T75 71¢ M1530 #50 (5) a; 1 — T75 Tab M340 M240 (5) 05p — Trim (5) 70cm a3: (Mama). (291) Let us write Eq. (291) as 25533 = Mg; (0,2) + 231351 (2,0) + AEéij (0, 0), (292) where AE”) (02) — —T T. 30 301- A 0A3 a — 76 642/16 Iu’q) 2 036 0,13 3 — ’75 EQHV #5 2 aria) h +00 2 AEéA)8(O,O) = —T3,5T€¢ (Z7?) [dwafiE (22100233 (w). (293) Eq. (291) (or Eqs. (292) and (293)) can be used to compute AEéi; for any choice of A and B and corresponding geometry. 124 5.1.1 The Second-Order Correction to the Interaction Energy of Two Colinear Molecules Let us derive AEéi; for a pair of colinear molecules whose internuclear axes are oriented along the z axis of the x, y, z laboratory frame, as shown in Fig. 12. In Fig. 12 x, y and 2 denote the axes of the the laboratory frame, and :c’, y’ and 2’ denote the axes of the molecular frames. The centers of mass of A and B are COM A and COMB, respectively. Also, the nuclei of A are A1 and A2, and the nuclei of B are BI and B2. Finally, R A B, is the center-of-mass to center—of-mass distance between A and B. It is important to mention that when we use the general formula for AEéiL from Sect. 5.1 to derive AEéi; for a specific A — B geometry, we carry out the derivation in the laboratory frame. The non-zero components of the dipole moments and polarizabilities of A and B, however, are given in terms of the coordinates of the molecular frame. Therefore, if the laboratory and molecular frames are not the same, we need to transform the non-zero components of the dipole moments and polarizabilities of A and B from the molecular frame to the laboratory frame. In Fig. 12, :L", y’, and z’ of the molecular frame are aligned with 1:, y, and z of the laboratory frame, so that the two coordinate systems are the same. Consequently, there is no need to transform the non-zero components of the relevant prOperties of A and B to the laboratory frame, and we can complete the derivation of [BESS/i; for this particular geometry in the laboratory frame. All quantities and equations in the remainder of this section will be given in terms of the coordinates of the laboratory frame. The center-of—mass to center—of-mass distance between molecules A and B in Fig. 12 is defined as RAB = RABIi + 12,4335! + RABzi, where RABI, 12,433 and RAB, are the :r, y and .2 components of R A 3. For this geometry, R A Ba: = RABy = 0, so that RAB = RABzi- To begin our derivation of AEéiRB for A and B arranged colinearly, we will determine the contributions of AEéiL (0, 2) and AE(2) (2, 0) 0A8 125 to AEéiL. Recall Eq. (149) in Chap. 3, 1 3R rag-5,, R2 T03=VOV5R= R5 3 , When we use Eq. (294) with R = RAB to evaluate Tag for all possible a and 3 where a and 3 can be I, y, or z, we find that (294) Txx = Tyy = Tzz = (RAB)31 (295) and T05— — 0 when a 7e 3. The expression for AEéi) B,(O 2) given in Eq. (293) simplifies to 1 AEéi; (0’2): - (2)Tm: Trait/150 “Boa; T Tyayufoufo 53y NIH BO BOO/12 $2: HTzzH Liza '8 BO Boa A nyl‘iE My Mata yx EH BO 800 Ay nyyy ”y ”ya Tyy 71223330335003 5. T2 Txxugoflfoan A BO BO A TzzTypypz yazy ml .... toll—I NIH [\DIH [\DIH NIH [\DIH VVVVVVV ,3? l ¢AAAAAA¢ )T (2..) In Eq. (296), we have omitted those terms that vanish because they contain Tag with a 75 ,3. Recall from Chap. 4 (Eq. (195)) that the permanent dipole moments 126 MA0 and p80 of molecules A and B are AO AOA AOA AOA = 9.. Hit, HA. 2 BO BOA BOA BOA u = uxx+uyy+uzz (297) For the colinear geometry of the dimer shown in Fig. 12, 113:0 = [1:0 = O and p50 = #50 = 0, so that ”A0 = 112402 and #30 = pfoi. Therefore, Eq. (296) reduces to (2) _ 1 BO BO A AEOAB (0, 2) — — (‘2‘) T22 T22 #2: Hz azz’ and similarly AEéi; (2, 0) reduces to 2 1 AEfLRB (210) = _ (E) T22 T22 #on #:1002132 When we substitute T22 = (Bi)? into Eq. (298), the result is AB 2 AEéii. (o. 2) = —- (R36) ,3 2.8%., and substituting into (299) gives 2 A1233). <2, 0) = — (R3,) 2:0 wag. (298) (299) (300) (301) Now, we need to derive an equation for AEéi; (0, O) in terms of R A B- From Eq. (293), h +00 AEéiL (0’ 0) Z _ (II—7F) / d“) [131"F TM? 0211‘ (201)053: (W) + Tm Tyy afiy (2w) afy (w) + Tm. T2,, a; (2(1))021.3 + Tyy Tm 05:1: (W) 05:1: (W) + Tyy Tyy ayAy (W) 0‘ + T33 T22 a; (w) a; (w) + Tzz Tm of; (w) a + Tzz Tyy a2, (w) (153 (w) + Tzz Tzz a: (W) 01.5.32 (20.1)] - Let us consider the imaginary-frequency polarizability a3: (w) of molecule A, which is given in Eq. (186) of Chap. 3. 0346 (w) = Z (029M);4 IJA>J . (303) E30) Em) + the In general, (13142.0) has nine components: (13:43 (no), 0:343 (2w), 03:42 (w), 0343 (w), 0343040), 0523(1)), (12430112), (12,/(w), and afz (2w). For any par- ticular molecule, however, some of these components may vanish, depending on the symmetry of the molecule. Let us determine which components of the imaginary- frequency polarizibility vanish for molecule A, where A belongs to the C00,, point group. Note that the components of the imaginary-frequency polarizability that van- ish for molecule A will also vanish for any other molecule with the same symmetry as A, and that the static and frequency-dependent polarizabilities have the same symmetry properties. Consider the product of matrix elements (0 Al )1 I ] A>< ] Al [1 IO A) contained in N A I” A Eq. (303). Using the fact that [1: = Z (32-Tia + Z: ZvRva, we can write the i=1 v=1 product of matrix elements as NA NA (OAleIJ'AHJAIMfIOA) = ZZeme,,(0A|r,,,3|jA)0,4334%) + 22%” (OAlrm7|]A> "m: + ZZZZmen<0AIRmIJA>919.40..) "Ii/737$: +2222 m=1 n=1 >< (OAIRmIJ'A> (jAIRnelOA>- (304) 128 The matrix elements of Rm vanish between orthogonal electronic states. The po- larizability components (13:13 (M), GA (2w), 0.31:3(ZLU), (152(201), azAx (w), and a”: (w) vanish by inversion symmetry with respect to the J: and y axes, but a; (w), CIA: (w), and (1A2 (w) are B,nonzero and a; (w) = 80343 (W). If molecule B also has Com, symmetry, then a3 3(zw), 0:8 5(zw), and (12,041)) are also nonzero, and (1535— — 0 if 5 74 (b. In this case, Eq. (302) reduces to 1'2 A1533), (0. 0) — (f5) / dw (T... T... a; (w) a5. (w) + Tny aA 00(zw)aB (w) 1‘19 yy yy + Tu Tu an (M) (15, (21.0)] . (305) Finally, because aA x(zw)- — aAy (2w), 01515.3:r (w) = of; (w), with (295), the total second-order correction to the energy of molecules A and B when they are aligned colinearly is magi; (0,2) + AEOle (2,0) + Ang} (0, 0) = 2 BO 800 A #2 #20 —(RAB6 ) +00 _ (L) #AO MAOCYzz B _ (i) [dw [zafix(w)afx(w) RAB6 z z 47r _ RA36 A + 4azz zw OB 2w (R:B6zz( )] . (306) 5.1.2 The Second-Order Correction to the Interaction Energy of Two Colinear HF Molecules Now, we will use the information in Sect. 5.1.1 to derive the second-order correction to the energy of two interacting HF molecules. If we assume that A = B =HF in Eqs. (300), (301), and (305) then we have (2) _ 2 HF,O H1200 HF AEOHF_HF(012) — — (m) Mz Mz 0122 , (307) 2 AEOJP HF (2,0) = — (m) MfF’WYOMfFO 2F, (308) 129 and AEOH)F HF (0,0) : _(4—H) _Zmdw [20 gRHF)— H:: (W) 40/” (191)04sz F090] + ZZ 309 RHF—HF6 ( ) Maroulis62 has recently used coupled cluster theory at the CCSD(T) level and finite- field perturbation theory to calculate the electric properties as well as the property derivatives of the X12+ state of HF as a function of bond length. Accord- ing to Maroulis, the most accurate values of these properties have been obtained using CCSD(T) theory and a (16s 11p 8d 4 f / 10.9 6p 3d 2 f) basis set. At the ex- perimentally measured value of the equilibrium bond length of HP, 7‘( H F)c = 1.7328 a.u., the CCSD(T) value of the permanent dipole moment pHF’O in the (16311p8d4 f / 1036p3d2 f ) basis is ”HR“ = 0.7043 a. u., and the corresponding value of the 22 component of the static polarizability of HF is aHF =6. 36 a. u. Recall that for the geometry shown in Fig. 12, ,uA0 — —/.I.’zA 0Z Fand ”BO — —u§ OZ, so pHFO— — ,uHFOZ. Substituting pH” = 0.7043 a. u. for pf 0and aHF— - 6. 36 a. u. for 01sz into Eqs. (307) and (308), we obtain 6.31 AEOIBF— HF (0’ 2): AE0H)F— HF (21 0) = — (m) ° (310) In order to obtain numerical estimates of A1303,” HF (0,0), we use the Unsiild ap- proximation with the average excitation energy approximated by the ionization po- tential Eff? of HF. Let us begin by considering the static polarizability of HF, as specified by Eq. (303), with w = 0 and A =HF. If we assume that the matrix el- ements in Eq. (303) are real, then (OHFI/lfyiFIjHF) = (ijlfigFIOHp) and (OHFIMe HFIJHF): (JHFIMHFloHFl ,and EQ- (303) reduces to (0 HF - AHFO )_2 Z (HFlMy IJHF> = 2 JHF¢0 We get the frequency-dependent polarizability of HF by letting A = HF in Eq. (303), a?!" (w) = Z: JHF¢0 (314) (OHFIMHFIJHFXJHFIMG FIOHF> E(0) —E(O) —zfiw JHF OHF (OHFIHFFUHF>(jHFlflgFIOHF>:| (315) (0) ° EJHF_ E0H)F + Zhw Setting (Ejn)p_ E62”) 91 Egg and using Eqs. (314) and (315) gives EHF 2 HF a??? (w) ( )a ale . (316) : [(EIPF2) +h2w2] Therefore, from Eq. (316) with ’y = 6 = as, ’7 = e = y, and ’y = 6 = z, we have 2 0:27(uu) __ (13HF3052F [(EIPF2) +h2w2] 2 aHF(zw) = (E11531?) a5?" yy HF 2 [(EIP) +h2w2] HF 2 HF aifiw) = (E’Pg) 0‘“ - (317) [(EEJF) +h2w2] 131 Using 033‘: Eq. (317), and Eq. (295) in Eq. (309) gives ayHyF’ 2 EHF 4 diff 2 h M=— (12.1-1.6) (...) XZOO dw [(EHF)2 12712002] 4(15‘IEF“)(a§;F)2 )1 +00 1 — 1;:1F-HF6 (Z7?) /w[(EfiDF)2+h2w2]2. (318) —00 In order to simplify Eq. (318), we need to evaluate the integral in this equation. If we let Eff = a and flu = :13, then dw = dx/h and the integral is _l d“ [(Efif)2l+ h2w2]2 = (H) _4 d1; (a2 +232)? (319) Since the integrand on the right-hand side of Eq. (319) is integrable from ~00 to +00 and it is an even function, G?) de(a2 : 3:2)2 = (:3) (200de +1.22)? (320) --00 According to the integral tables of Gradshteyn and Ryzhik,67 +00 1 (2n — 3)” 7r / ”Home" 2 <2n—2)z:a2n—v (321) 0 where (2n+l)ll=1-3---(2n+1) and (271)” = 2-4---(2n) . For 71:2, +00 1 7r [d1]? (a2 + $2)2 — 2—a3'. (322) 0 From Eqs. (320) and (322), 1 +00 1 7T (5) / d$(a2 + 1:2)2 — “Th, (323) 132 and +00 / dw 21 2 = 11:3 . (324) -00 [(Efif) + 7121122] [P h Using Eq. (324) in Eq. (318), 131931)-“ (0, 0) = _ 355(03): _ EfivF(aZF):_ 2(RHF—HF) (RHF-HF) When we let of?" = 6.36 a.u., aflp = 0%!" = 5.22 a.u. (as calculated by Marouli862) and EH! = 0.5896 a.u. in Eq. (325), the result is“8 (325) 31.9 . . AE33F_HF (0, 0) = — a u 6. (326) (RHF—HF) - AF”) 2 0 AF”) 0 2 AE(2) 0 0 - Addlng OHF—HF( , ), 0HF_HF( , ), and OHF—HF( , )g1ves the total second-order correction to the interaction energy of two colinear HF molecules, 44.5 a.u. AEH) = — . (327) OHF—HF (RHF—HF)6 5.1.3 The Second-Order Correction to the Interaction Energy of Two Parallel Molecules At this point, we will derive an expression for the second-order correction to the energy [SE/"((33 of two interacting molecules A and B whose internuclear axes are parallel to each other and to the x axis of the 2:, y, z laboratory frame. This particular arrangement of molecules A and B is shown in Fig. 13. In Fig. 13, x’, y’, and z’ are the axes for the molecular frame (A and B have the same molecular frame), A1 and A2 are the nuclei of molecule A, and 81 and B2 are the nuclei of molecule B. Also, COM ,4 and COM 3 are the centers-of-mass of molecules A and B, respectively. We have denoted the vector extending from the center of mass of A to the center of mass of B by RAB. Let us compare the geometry of A and B in Fig. 12 with the geometry of A and B in Fig. 13. The internuclear axes of A and B are designated as the z’ axis of 133 the z’, y’, 2’ molecular frames. Whereas the :r’, y’, 2’ molecular and x, y, z laboratory frames are the same in Fig. 12, these frames are not the same in Fig. 13. Rather, the x’, y’, 2’ molecular frame in Fig. 13 is rotated 90° counterclockwise from its position in Fig. 12. Consequently, we need to rotate the non-zero components of the relevent properties of A and B for the geometry shown in Fig. 13 from the molecular frame to the laboratory frame. While deriving AEéi; for the colinear arrangement of A and B shown in Fig. 12 (see Sect. 5.1.1), we determined that the non-zero components of the dipole moments and the static polarizabilities of A and B in the molecular frame are [1:10 , [1530 , A A A B B 2:232 yy) 221 arr, ayy’ 01 01 Oz and 01:32 T.hese components have the same values 1n the molecular frames of Fig. 13. We can rotate these components from the molecular frame of Fig. 13 to the corresponding laboratory frame by interchanging the roles of :1: and 2. Therefore, we have “214,0: #201 #280 — "MEO, afixr = 02:, 024,2, = 0133;) (.153, = a2, and (132, = 02131 . Recall Eq. (296) from Sect. 5.1.1. Because [.130 = #50 for the current geometry, Eq. (296) reduces to BO [1800! A AEéi’. <0, 2) = — (g) T ”T. u. a... (328) Similarly 2 A0 ”A00 B AEHLRB (2’ O) = — (2) T1171? TILE #2: am (329) In Sect. 5.1. 1, AE E033 (0, 0) is given by Eq. (305). Since we have (1:7,: C232 , 01242 = (lg/m), 01m: 052;, and a2 = 051., for the current geometry, we can also use Eq. (305) to write AEéiL (0, 0) for the geometry of A and B in Fig. 13. When A and B are parallel to each other and to the :1: axis of the laboratory frame, the total second-order correction to the interaction energy energy of A and B is AE”) = AEOij, 2) +AEOi)B(2,0)+AE EH) (0, 0) OAB 0A8 = _(;)TxxTxfoO/J;BBOQTA$- (2)TxxTrx/1£O%Aoafx 134 +00 5 A B _ (47:) /dw[Tm Tm 02,2, (w) an, (2w) Tyy Tyy 01A (W) QB (W) yy yy — Tu Tu a331, (2w) a331, (2w)] . (330) 5.1.4 The Second-Order Correction to the Interaction Energy of Two Parallel HF molecules Now, we will use the information in Sects. 5.1.1 - 5.1.3 to derive the second-order correction to the energy of two parallel interacting HF molecules. If we assume that A = B =HF in Eq. (330), the result is 2 2 2 2 AEéHL—HF : AEéJF-HF (0’ 2) + AEéI-BF-HF (2’ 0) + AEéH)F-HF (0’ O) = _Txa: Tm: (#:IF)2 0gp h +00 HF 2 _ (Z7?) fdw {Tu Tu [an (zw)] 2 _ Tyy Tyy [015? (21.0)] _ T22 T22 [afle (W)]2} ° (331) According to Eq. (295), Tm, Tyy and T22 for the colinear arrangement of A and B are —1 Tm: : T = W (RAB)3 2 22 -——3, (332) (RAB) Using these equations with A = B =HF in Eq. (330), we have 2 2 2 2 AEéH)F—HF : AEéI-BF—HF (0’ 2) + AEéIBF—HF (2’ O) + AE(()H)F—HF (0’ 0) 1 HF 2 HF : _ #27: am (RHF—HF)6 ( ) — (Elf—i7?) (RHF1_HF)6_ZOdw [agp(w)]2 135 ’ (In?) (Rnimfzdw [05? M2 h 1 +00 2 — — dw [ozHF (2111)] (333) (7’) (RHF—HF) 22 -—00 where we have also distributed the integral over (.12. According to Eq. (317) in Sect. w) aHF(zw), andafz F(zw) can 5. 1. 2, the frequency-dependent polarizabilities aHF ( , W be approximated by 2 OzHF (2(1)) 2 7 (EIHF) Gigi [(Efi; F2) + hsz] 2 aHF (2w) : (EHF) as)? W [(Efigp)2 + hzwz] aHF (W) : (EEDF)2O:IZF (334) [(13552 + 1121.12] ’ From Eqs. (333) and (334), we have AEOH)F— HF = AEOIBF— HF (0’ 2) + AEOHF- HF (2’ O) + AEéfB—F HF (0’ O) 1 HF 2 HF : _ ”a: 0151' (RHF—HF)6 6( ) (21%) (13;:)F((111;):HF)6)2_/;w[(EHF)21+h2w2]2 — (£7?) (13::)F% HF) i/wdw[(EHF) 21+ h2w2l2 _ (g) (1:11;:HF)6)2_/:dw[(EHF)1,302]? (335) 136 The integrals in Eq. (335) were evaluated in Sect. 5.1.2. According to Eq. (324) in Sect. 5.1.2, +00 1 / d1.) 2 2 = ”:3 . (336) -00 [(Efif) + M122] [P h From Eqs. (336) and (335), 2 2 2 2 A3,)... = wt)... (02) +333),_,, (2,0) +AE6.’.-.. (0.0) 2 2 ___ (Him) 33;; _ (E55) (05‘2") (RHF-HF)6 4(RHF-HF)6 (E3333)? _ (E33335? (337, 4(RHF-—HF)6 (RHF—HF)6 Recall that in the calculation of AE3:)F_HF for two colinear HF molecules that we took pi”: = 0.7043 a.u., Efif = 0.5896 a.u., 0gp = off = 5.22 a.u., and off = 6.36 a.u. Because we have interchanged a: and z for the current geometry, we have #:F = 0.7043 a.u., of: = agf = 5.22 a.u., and of: = 6.36 a.u.. Using these values in Eq. (337), we obtain (2) _ (2) (2) (2) AEOHF—HF _ AEOHF—HF (0’ 2) + AEOHF—HF (2’ 0) + AEOHF-HF (0’ 0) 29.2 . . = — a u 6. (338) (RHF—HF) 5.1.5 The Second-Order Correction to the Interaction Energy of Two Perpendicular Molecules In Fig. 14, the internuclear axis of molecule A lies along the z axis of the 2:, y, z laboratory frame, and the internuclear axis of molecule B lies along the x axis of the 1:,y, z laboratory frame, making these two molecules perpendicular to one another. The nuclei of molecules A and B in Fig. 14 are labeled A1, A2 and BI, 32, respectively, and the centers-of-mass of A and B are COM A and COM 3. Also, RAB denotes the vector extending from COM A to COMB. 137 Let us call the molecular frame of molecule A in Fig. 14 the LL", y’, 2’ frame, and the molecular frame of molecule B the :12”, y”, 2” frame. The internuclear axis of molecule A lies along the z’ axis of its molecular frame, and the internuclear axis of molecule B lies along the z” axis of its molecular frame. Because the internuclear axis of A lies along 2 and z’, the molecular frame of A is the same as the laboratory frame. Therefore, we do not have to rotate the non-zero components of the relevant properties of A, and we can specify these properties in the laboratory frame. However, because the internuclear axis of molecule B lies along 2” and x, we need to rotate the non-zero components of the relevant properties of B. The :12”, y”, 2” frame is rotated 90° from Ex ‘2 03%", and (15y 2’ ai = affix”. From the properties of A and B and Eq. (293), we have the 23,31, z frame. Thus #50 = p39, Oz 1 1319339 (0,2) = _ (5) Tm Tm (359)23fix, (339) (2) 1 A0 2 B AEOAB (2, 0) = — (‘2') T33 Tzz (Hz ) axtrxn, (340) and +00 (2) h A B AEOAB(0,0) = — Tm TM (47?) [dwam(zw)azuzu(zw) fi —+oo — Tyy Tyy (21;) / d0) (lg/4y (2&2) (1513/11 (20.)) )1 _+00 _ TzZ Tzz (47f) /d¢uafz (3w) dag/3,4212). (341) -00 Letting A = B =HF in Eqs. (339), (340), and (341) gives 2 1 HF, 2 AEéH)F—HF (0, 2) = — ('2’) TIIXI: T333 (#2,, 0) agF, (342) 1 AE3:)F_HF (2,0) = _ (5)71. Tu (#5502353 (343) 138 and +00 2 h AEéJF— up (010) = " Tara: Tan: (1;) /d“dafo (2w) 01:1”; (W) -oo h +00 — Tyy Tyy (4;) diuagF(w)afi,§~(zw) h — Tzz Tzz '— (4.) +00 x / dwagp (magi. (w). (344) 5.2 The 2'” -Order Correction to the Interaction Energy of Three Molecules In Sect. 5.1, we wrote the second-order correction AEéilA to the interaction energy of molecules A and B (see Eq. 292) as AEOAA— _ 3123340, 2) + AE” 8(2, 0) + AEO2)B (0,0). (345) If we have three molecules, which we will denote A, B, and C, we can write the total second-order correction to the energy of interaction AEéiLC of these molecules as the sum of the second-order, two-body corrections due to the interactions of A and B, A and C, and B and C, AE(i:C= AEOAB + 435,336 + AE02) (345) BC’ and an irreducible three-body energy) of second- order, AEOABZI' The second-order, (2) is two-body energy of interaction AEOA)B of A and B is given in Eq. (345), AE given by Eq. (345) with B replaced by C, EOACS Ang’fC: 435,33 (0,2) + AEoi) (2, 0) + 4353; (0, 0) , (347) and AESQC is given by Eq. (347) with A replaced by B, AEOBcz Ang; (0, 2) + AE(B 2’ (2,0) + AEOBC (0, 0) . (343) 139 The irreducible three-body energy A5133: is a sum of three contributions, AEéi’B) , AE(2 B3), and AE(:’ 3) ,where 131332 3 - “03,3 Ta7(RAB) #50 Tfi6(RAC) 1U? 0- (349) The full nonadditive second-order correction to the energy AEéigé 2, 3) nEgAAC = _ a5, Tannin) n50 Tamra) a?” - 055 Ta'7(RAB) #30 T36(RBC) #600 - c223 Ta7(RAC) #30 T36(RBC) 141530. (350) Therefore, using Eqs. (346), (345), (347), and (348), we obtain an equation for AEOA)BC’ ABM)” = 1:530:13 (0:2)+AE(:)i:e(2 0) + EoA:B(030) :E02)C (0 2) + :E0::C (2»O)+ AEoiLw ,0) + EOE},(O,2)+AEO2B)C (2,0) + EOB)C(O,O) AEOABC. (351) We will use Eq. (351) and the results of the derivation of AEOHC_ CC in Sect. 5.1.2 to derive and equation for AEOJAL HF_ HA. 5.2.1 The Second-Order Correction to the Interaction Energy of Three HF molecules, Arranged Colinearly Fig. 15 shows three colinear HF molecules which have their internuclear axes on the z’ axis of the :c’ , y’, 2’ molecular frame. Their internuclear axes are also aligned with the :r, y, z‘laboratory frame. Note that the molecular and laboratory coordinate systems are the same, as in Fig. 12. In Fig. 15, we have labeled the HF molecules HP 1, HF2, and HF3. Also, H1, H2 and H3 denote the hydrogen atoms in HFI, HF2, and HF3; and F1, F2 and F3 denote the fluorine atoms in HE, HF2, and HF3, respectively. The HR, HFg, and HR», molecules have centers-of-mass COMHF“ COMHFZ, and COMHFa, respectively. We have let RHFl-Hth RHFl—HF31 and RHFz—HF3 be the vectors between HFl and HFg, HFI and HF3, and HF2 and HF3. If we let A z 140 HF1,B = H172, and C = HF3 in Eq. (351), we have AEéi)p,_na_ar3 = AEéi’CCHFA(0,2)+AE(§:)F,_HF (20) + AEéffCCHFC (0,0) +AE33.)F,_HF (0’2) + Angij HF, (20) +AE3?F,_HF, (040) + AE32,)CC_,,,A(0,2)+4311?” (240) + AEéijC an. (0,0) +AE3§:3_HF,-HF, _ (2) (2) (2) _ AEOHFl—HFQ + AEOHFl—HFg + AEOHF2—HF3 (2.3) + AEonF,_na_ur3- (352) Recall Eq. (327) from Sect. 5.1.2, which gives AEé:)F_HF for two colinear HF molecules 44.5 a.u. AE<2) = . 353 OHF—HF (RHF—HF)6 ( ) Using Eqs. (352) and (353), we have (2) 44.5 a.u. 44.5 a.u. 44.5 a.u. AEOHFl-HFg—HF}; : — 6 — 6 — 6 (RHFi—HF2) (RHFr—HFe) (RHF2—HF3) (2.3) + AEOHp1—HF2_HF3' (354) From Eq. (350), the irreducible three-body energy for this geometry is 2,3 _ AEéAB; = _ a; Tzz(RAB) #23 Tzz (RAC) “S '— CéZTLAJKAB)MfQQAIiBC)HS — OS; T22(RAC) l1? Tzz(RBC) ”28- (355) and, letting A =HF1, B =HF2, and C = HF3 in Eq. (355), we have 2,3 AE(() ) = — Gin TZZ(RHF1-HF2) [A513 TZZ(RHF1—HF3) [1st HFl—HFg—HF3 _ 0.52% T22 (RHF1_HF2) ”EB T22 (RHFz-HFs) ”5”}; - 0‘th Tzz(RHF1—HF3) Him] >< T22(RHF2-HF3) ”gm, (356) 141 5.2.2 The Second-Order Correction to the Interaction Energy of Three Parallel HF molecules Fig. 16 shows three parallel HF molecules which have their internuclear axes aligned with the z’ axis of the :r’,y’, z’ molecular frame, and with the :1: axis of the any, z laboratory frame. In Fig. 16, we have labeled the HF molecules HFl, HFg, and HF 3. Also, H1, H2 and H3 denote the hydrogen atoms in HFI, HF2, and HF3; and F1, F 2 and F3 denote the fluorine atoms in HF], HFg, and HF3, respectively. The HFI, HFg, and HF3 molecules have centers-of-mass COM Hp” COMHF2, and COMHFC, respectively. We have let RHFl—HFQ) RHFl—HFg , and RHFQ—HFg be the vectors between HF} and HF2, HFI and HF3, and HF2 and HF3. The relationship between the molecular and laboratory frames in Fig. 16 is iden- tical to the relationship between these two coordinate systems in Fig. 13. Therefore, we can use the equation for AE(2) 2 OHF—HF Sect. 5.1.4 to write AEéA)C_,,C Eq. (352) in sect. 5.2.1, AE”) OHFl—HFQ—HF3 derived for two parallel HF molecules in for each pair of molecules in Fig. 16. According to is AEéi).,_n.~,-nr, = AES:)F,-HF, (0, 2) + ”5%“, (2, 0) + AEéi)FA_HFA (0. 0) + AES:’.,-..~, (0, 2) + AE3:)C1_,,FC (2. 0) + AEéi)n,_nr, (0’ 0) + Milan... (0. 2) + 4E8; (10) + 4193122-“, (0. 0) + AEéi’if_....-nn, = AEéi)Cl_HCA + AEéi).~,_nn, + AE3:)r,_nn, + AEéi’if-nr,_n.,- (357) Recall Eq. (338) from Sect. 5.1.4, which gives AEé:)F_HF for two HF molecules that are parallel to each other and to the x axis, 2) _ 29.2 a.u. HF—HF — (RHF—HF)6. 4E5 (358) 142 Using Eqs. (357) and (358), we have AE(2) _ 29.2 a.u. 29.2 a.u. 29.2 a.u. 0 — — --— .... HFl- HF2- HF3 (RHFI— HF2)6 (RHFl—HF3)6 (RHF2—HF3)6 (2,3) + AEOHF1——HF2—HF°3 (359) From Eq. (350), the irreducible three-body energy for this geometry is 2, 3 AEéABL— — _ O‘A' WEAR/(B) RAC)#C Tm( — Q§JIT12(RAB)3(RBC)H7I — arz’ Tum/10) #2 M(RBC)B - (350) and, letting A =HF1, B =HF2, and C =HF3 in Eq. (360), we have __ HFI HF] HF3 1315613,- —HF2-HF3 — — 012,2, Txx(RHF1-HF2)#ZI Txa:(RHF1-HF3)MZI - eff? sz(RHFr-HF2) 14521 Ramadan) #5172 — 0553 Tm(RHFr—HF3) #52 X Trr(RHF2—HF3)#:iF2. (361) 5.3 The Third-Order Correction to the Energy of Interaction of A and B According to Eq. (290) 1n Chap. 4, the third- order correction ABC? Bto the energy of two interacting molecules A and B 1S 3 A AESAL = — T05 T57 7161) #040 (15000.3 Aa'fi? 1 - gTea T75 Tee #50 #3 0145?” 3“... 1 _. -6—TO,A3 T76 71¢ ”00/170”er 36,30 _ T03T75Teaugo(zh- 7K)Zodwaw(w) fiCm(— w;zw,0) h _ T03 T64) T75 ”:10 (4;) [00 dw 0323, (w) @1354) (—zw; 2w, 0) —00 143 — T03 T76 Te¢(%’ —:-)/oodw fmdw' 7C,C( (zw;zwI—w,-zw’) X [bfw (w; w — 2w, —zw) + 123,, (w; —zw' — w, 7412’) + bggd, (—ud; w, + w, —zw') + The individual terms in AE(3 ) AEB) 0A8 AE‘2’) 0A8 E02113 3 4E6). AE(3) 0A8 AE(3) 0A8 [#53346 (—w; w — 741),, 74.12)] . are 0.48 (1 1) Z _ 01/3715”) TE¢H£OH§§30 066055 1 (37 0) = —6 0113 T75 Tm) [1’20 “gm/1:10 186,133) 1 (0 3) = -6Tad T76 71314501430145” 33. h (0,1) = J11,3 71“,, TC, ago (47?) foo dang, (2w -oo x C3,, (—zw;2w,0) h +00 (1’0) 2 “7111371357176”? (a) [@0127 (W x 5535C» (—zw;zw, 0) (0,0) = -TafiTyéTcd)(% —:)/oodeOdw' A . I I x me (2w,zw —- 2w, —sz0) x [bfw (2w; 3w, — 2w, —zw') + 5%,, (M; —quI — 2w, 7.5),) + (253C, (—zw; w, + w, —zw’) 144 (362) + (253$ (—zw; 2w — w], 3111)] . (363) We can use Eq. (362) or (363) to derive expressions for AEéi; as a function of RAB for various geometries of A and B. 5.3.1 The Third-Order Correction to the Interaction Energy of Two Co- linear Molecules Let us derive an expression for AEéiZC as a function of R A B for the colinear geometry of A and B in Fig. 12. To begin, let us derive an expression for the AEéiL (1, 1) term in Eq. (363) as a function of RAB. Recall from the derivation of AEéi: a function of RAB for this geometry that the molecular and laboratory axes are the same, so there is no need to rotate the non-zero components of the properties of A and B before deriving A1333; in terms of the laboratory coordinates. While deriving AEéi; for this geometry, we also determined that Tm = Tyy 75 O, Tzz 75 0, and T03 = 0 when a 31$ 3. In the colinear configuration of A and B shown in Fig. 12, pfio = 11on = 0 and pf” = pf” = 0. Therefore, AEéi; (I, 1) = — Tzz me T22 #1240 ”280 Q2435 afz — T... Ty, T... a?“ u?“ at; 0:52. _ T22 Tzz Tzz #240 ”£30 05:12 0282' (364) Finally, since 0405 = 0 if a 75 ,3, AEEEB (1,1) = —TZ,z Tu Ta 11:10 #230 or“; 05,. (365) Recall Eq. (295) from Sect. 5.1.1, —1 Tm: : T = _— 2 AB Using Eq. (366) in Eq. (365) gives A0 BO A B (3) _ 8/4.. 14. area... AEOAB (1,1) _ (RAB)9 . (367) 145 Now, let us derive an equation for AEéi; (0,3) for this geometry. According to Eq. (363), AEéi’B (0,3) is 3 1 ABS). (0, 3) = 7311;) :13, T.) 35077530735?“ 34:... (368) Since Tm = TW 79 0, T2; 74 0, and T03 = 0 when a # ,8, and ,ufo = #50 = 0, 1 AEéiL (0, 3) = 77;. T2. T... u§°u§°uf° 2‘; (369) Using Eq. (366) in Eq. (369) gives 3 AE(3) 4015.30) fizz. 3(RAB)9 0.48 (0,3) = — (370) Similarly, according to Eq. (363), AEéi; (3,0) for A and B as arranged in Fig. 12 is AEéiL(3,0) = —% asTslaTeiuéoufi°uf°fi£as (371) and AEéiL<30> = —%T..T..T.. (324°? .3 (372) Using Eq. (366) in Eq. (372) gives Mg; (3,0) = —4(”?0)3 :3 (373) 3(RAB) At this point, we are ready to calculate AEéi; (0, 1) and AEéi; (1, O) for A and B as arranged in Fig. 12. According to Eq. (363) in Sect. 5.3, AE(3) (0, 1) 0A8 15 +00 ’5. AEéiL (0,1) = —Tag T76 Tecb #50 (21;) / dw fig” (—zw; zw, 0) X c7533 (2w) . (374) 146 Since a) T,m 2 TM 75 0, Tu 75 O, and T03 = 0 when a # B, b) pf,” = )1on = O and c) 070,3 = 0 when a 31$ B (for HF), +00 AEéiL(0,1)= — T..T..T..u§°(4%) fdw 3...(— w w 0) >< aim) “0° _ T T Tzuz(4h 7K)Zodwfi,yy( —zwzw0) x aijw) +00 h _ Tzz T22 T22 #50 (a) f d“) fiiz (_W; W) 0) x (if, (w). (375) In order to simplify Eq. (375), we need to determine which elements of the hy- perpolarizability B22117 are nonzero. For a Coo” molecule with its axis in the a: direction by reflection symmetry in the x2 and yz planes components of the [3 hy- perpolarizability tensor that are odd in either subscript a: or subscript y vanish. By rotational symmetry around the z axis, the non-zero components of the hyperpolar- izability ,Bfm of molecule A (with C00 00,, symmetry) are Bxxz— "" '— 2:23: £112: _ 551,2- - yAzy— — 22,3], and 324”. If we assume that molecule B also has Coo” sym- metry, then the non-zero components of the hyperpolarizability of molecule B are B _ B _ B _ B B (811)832—— szx — 2.72.7) — yyz — yzy — zyy’ and 222' NOte that the non- zero matrix elements of the static and frequency-dependent hyperpolarizabilities of molecules A and B will be the same. When we inspect Eq. (375), we see that it contains only non-zero matrix elements of the hyperpolarizability of molecule A. Therefore, we cannot eliminate any more terms from this equation for AEéiL (O, 1) . However, we can simplify the expres- sion for A518; (0, 1) by simplifying the expressions for the frequency-dependent hyperpolarizabilities contained in Eq. (375). Eq. (215) in Chap. 4 gives the static hyperpolarizability H705 of molecule A. From Eq. (215) with ’7 and 6 interchanged, 147 we have (33,: Z 1...)..70 (E,£E?— Eéf) (E :3 ES?) x [(0117). IkA> (0.4163(3))(3.116311361163103 (OAIIIQ lkA> (lAlflAIOA) (0.416.Alk.4>(k.4|fiflz.i)(1.4162(0)) )< > > > ) _:_A <0A|#7|kA kAlfls llA (lAlfialoA ;A (01163373377311 (1.416? (0.4 J. (376) As discussed in Sect. 5.1.2, we can use the Unséild approximation to write 1 1 (0) (0) g '7" (377) EkA — EOA 1P +++++ and 31(3) i E53) 2 3% (378) When we use Eqs. (377) and (378) in Eq. (376), the result is 5.0.7 A) 2:: [< 0AM. lkA> (kAlflallAWAlH7 |0A> (Erlp)2 1s,, 1,7730 (OAlltAlkAXkAl/te |1A><1AII17IOA> (oilfiémmmflzix A163 (0.4) (OAIfiAIk/i)(kAlfifllAXlAl/la IDA) (0.4172333)(kAlfifizA><1AIH7 IDA) —(oAI6A (3.1331162 IoA)<3AI6..6A IDA) kA (OAIMAIOAXOAIHQA 7|0A> (OM/12A lkA) (OAlfiéA |0A)<0AI#QIOA> >1 (OAlflAIOA (381) Similarly, since 2 IkA)( [CA] 2 1, [CA + X Z (CAI/12A lkA>= 1s,, 1,4760 (OAlfle'flafl AIDA) (0.1m? IDA) (0.116621036366071) ((OAIIICIOA) (0 (6210A)<0AI6A10A)) (332) Recall from Sect. 4.1 that $0 = [1:3 — [1230. When we use this equation in Eq. (382), the result is A ;A A Z (OAlfléAlkAXkAlua|1A> = kAJAsaéO 149 (OM. #3617 A|06> - (OM/12A |0A><0A|fiafiA|0A> - (OAIAAflaloA)<0A|/1A|0A> OAlfiA |0A><0A|HA|0A>(0A|#A |0A> OAlflAIOAMA 0(0A|0A>(0A|/1A|0A> ( < = (0A Ail/AIDA) < < 0A llu’e loj><0AlflauA|0A> OAII-le fiQIOA> A A A A A A + #6063067“ 13.06.7067” = (OAlfléA'flafiAIOA> — (OAIAA |0A><0AlflafiA|0A> — (0AI6A62I06)<06I6A10A). (333) Now, consider the sum over [CA and [A of (CAI/lg IkA) (kAlfifIIA) (lAlpA IOA) in Eq. (379). We can use Eq. (383) with 6 and a interchanged to write this quantity as Z (OAlfiA kAJAaéO <06I6A6f6AloA) — (oAI6AloA) = by61n the sum over 6,, and 1A of (oAmglkA) (M6364) (lAlfiAlOA) gives 2 (OAlflalkA)— — kAJAaéO (OAlflAfiAfiA|0A> - (oAI6AIoA> (lAlAAl0A> yields 2 <0AI624I6A><6AI636A>«Ammo/1 = 1971,7720 (OAIAAA7 AAIOA) '— (OAIAA |0A>(0A|AA;1§|OA) - <0A|fifAAI0A><0AI6£I0A> (386) We can also use Eq. (383) with 6 replaced by ’7, 7 replaced by a, and a replaced by 6 to write 2 (OAIAAII‘CA)(kAlAAllA>(lA|AA|0A> = 6,4,1A9eo <0A|A7 AA Aa AIDA) - (OAIAAIOA><0A|AAA AIDA) — (OAIAAAA IOAXOAIAAIOA) (387) Finally, interchanging ’7 and 6 in Eq. (383) allows us to write the last product of matrix elements (summed over all k A, l A 3A 0) in Eq. (379) as Z <0Al6r,‘ 16A><6AI626A><1A6£ 61,4): 16,1, lAaéO (OAIAAAAAAIOA) - (OAIAAIOAXOAIAAAAWA) — <0A|A7 AAIOAXOAIAA IDA) (388) Therefore, we can use Eqs. (379), (383), (384), (385), (386), (387), and (388) to write LA A ><0Alfla MAMA) A ;.AA A m — A [<0AIA5AQAAIOA>-<0A|AA|0A> + (OAIAaAe AAA|0A> (OAIAAIOAXOAIAAA A|0A>—<0A|AaAe AIOAXOAIAAKLA) 151 fl(Aory g <0A|M0M7MA|0A>— (DAIMQIOAXOAIMZMA AIDA) (OAlMaM7 |0A>(0A|MA |0A>+ +<0A|MA M7 AMAAIOA) <0AIAA10A><0A — <0A|AA A3|0A><0AIAA10A> <0A|A7AAAAI0A>—AA10A><0AIAAAA<0A> <0A IAAAA“ |0A><0AIAA10A>+ +<0AIAAA2AAI0A> <0AIA310A><0AIA2AAI0A> <0 AIAAA2<0A><0A|AA I0A>] . <380) Since the matrix elements in Eq. (389) are real, we can write Eq. (389) as 2 A ;A A A ;A A (E? PA) [<0AIAAAAAA > -— <0AIAAI0A><0A (GA IMfMa|0A><0A|M7|0A>+ +<0A|MaMfM74|0Al <0AIAAI0A><0AIA3A710—A> <0AIAAAAAI0A><0AIA7 I0A> < A3AAI0A>— <0AIAAI0A><0AIA7AAI0A> <0AIAAA7I0A><0A|AA |0A>] (300) Solving for the matrix elements in (390) gives W) «A 2 (E [<0AIAA AAAA10A>— <0AIAA I0A><0A <0A|MA Ma A|0A><0A|M7 |0A>+ +<0A|M§MA AM71|0A> (OAlfifiloAXOAlfi-efi 7|0A>- (OAlMaMA|0A><0A|M7|0A> <0A|M§M7MA|0A>- (OAIMA|0A>(0A|M7MA|0A> <0AIAAA710A><0AIAA AA] (391) _'~_A A Expansion of the matrix elements in Eq. (391) using pa = [1:3 — Mg (and similarly ;A _A_A for [LAY and [JG ) followed by comparison of terms shows that <0AIMA MaM7 AIDA) 152 —<0AIAA I0A><0AIAAAAI0A><0AIAAA£I0A><0AIAAI0A> = (OAIMAAMAM A—IOAl (OAlMaloAXOAIMAMAIOA) '(0AIMAAMA IOA)<0A|M7|0A) = <0A|M0M7MA IOA)— (DAIMAAIOAXOAIM7MA |0A> — (OAlMaM7l0A)<0A|MA|0A) (392) and therefore M53703 Apz) 6 A ;AA : [<0Al/J'? _IIQI’LAIOA)—<0AIH:1|OA> - <0A|MA AMA|0A>(qAIM7 IDA) E(.0— -E0A— zhw) (Eéol— E3 ‘33) A 607 (—zw; 2w, 0) <0A|M7 lJA) (JAlMa MA) (quMA MA) E(.°— —E03) (EA? —E(O) + AAA) Em (OAlMA IJA><9A|MA IDA) (EA — AA) (BA - AAA) MAAA7(- MMO) ’-—‘-’ Z JAqA¢0 (OAIMA IJA>(qA|M7 i0A> (EMP— zhw) EMF <0A|M7 |JA> EMF (EMF + zfiw) (OAIMA IJA>(JA|M7 IqA>(qA|MA iOA> (EAP + zhw) (EA [P + zhw) (DAIMA IJA>(qA|MA IDA) Ej‘ p(EAp- 2AA) (OAIMA IJA> (E1 IP + zhw) EMF + (396) Using Eqs. (383) - (388) with [6,4 = jA and 1A = qA in Eq. (396) gives A 507 (OAIMA M7 AMAIOA>— (OAIMA IOA)<0A|M7 AMA|0A> (EJAP — ZMW) (BAP - zMW) (OAIMAM 7|0A>(0A|MA|0A) (EA —mA> (EA AA) A A (DAIMAAMAMAIOAl— (OAlMA IOAHOAIMAMAIOA) (EIP zhw) EIP (OAlMA MA|0A><0A|M7 |0A) (EMPA — zhw) EMF <0A|M7 MAMA A—IOA> <0A|M7 IDAHOAIMAMA IDA) EMF (EIP + m“) (- -zw;zw,0) 154 <0A|M7 MQIOAXOAIMEA IDA) EEAP (EMF + 2h“) ALAA ;AA (OAlfiaM7MAIOA>- (DAIMCA |0A><0A|M7MA|0A> (EAP +zhw) (E;4 ,P + zhw) (OAIMQM AIOAXOAIMEA IDA) (Ea) + W) (Ea) + m») A ;AA (DAIMAME ”filo/1)"(OAIIA‘yIOAXOAI—fleA/AIAIOA) EMP(E1P - 25w) <0A|M7Me AIOAXOAIMA |0A> E1 P(E;AP— 2h“) (OAlMaMe AMA|0A)— (OAIMQ |0A><0A|Me AMAIOA) (EAP + 2h”) EIP (OAIMQME |0A><0A|M7 IDA) (EAP + zhw) EIP (397) Since the matrix elements in Eq. (397) are real, we obtain “2 A son A .LAA A ;AA [<0AIMQM7 MAID/1) - <0A|M2|0A><0A|M7 MAID/1) <0AI/22r1-13 |0A><0A|M2A Ion] ("w; w: 0) A 1 1 (E1 IP + :fiw) (EiAP + 2h“) + (BAP _ zfiw) (EiAP " 27%)] L<0A|Me MaM MA—|0A> (OAlMe |0A><0A|MaM 7|0A> (OAIMe Ma |0A> <0A|M7A|0A>] 1 1 L(EAP “ m”) EfAP + EiAP (EMF + 2h”) (OAlMAMe MAID/1) A _2.A A <0AméloA>— (OM/13m low/alumna] 155 1 1 + EiAP (EiAP - 2h“) (E3AI) + 2h“) EiAP Then, from Eqs. (392) and (398), N A LA A A _c.A A 2:7 (w; m0) = [<0AIuA uaufilon — <0Alqu0A><0A|uau¢I0A> A 2A A — <0A|ufiualoA>] x . (398) 2 2 x + EAP (BAP + 2m") EiAP (EIAP " Z’5‘") 1 1 + . (399) EfP -— zfiw) (EfP — 2%)] + A A (EIP + zht") (EIP + 2’7‘") ( Using Eq. (393) in Eq. (399) and combining the frequency-dependent denominators in Eq. (399), A can MA)“ + 2h2w2] 3(Ef‘P + 2m)2(E;1P — zruu)2 ' [BA (_w; 2w, 0) g 60:7 (400) Let us return to the calculation of AEéiL (0, 1) . We will use Eq. (400) with 6=z,a=a: and ’y=:1:;with e=z,a=y and ’y=y;andwith e=a=7=zinEq. (375) h AEéiL (0: 1) g _Tm Tm T22 ”:30 (—) 277 yaw/2A [3“ + (Emwwfi X P 3(EAP + zhw)A(Ef‘P ‘ zh’w)2 an; (W) —00 h _ T22 Tzz Tzz ”:30 (Z7?) +00 A A 4 A 2 2 2 fizu 3 E + E hw X /d‘*’ [(1,3) 2( ”3) Jam). (401) 3(Ef‘P+zhw) (EfP—zhw) Then, using Eq. (317) from Sect. 5.1.2 (with HF replaced by B) in Eq. (401), we find “‘00 AB“) (0,1) g —TmeTzzpB°(£) 0’43 z 27r 156 ll? HZ £13.73 7:14»); 2” [3(E1P)A + (EAPMEAWAJ (EMP)AOtB 3(EAP + z7i‘*’)A(EiAp-Z MA) [(Ef3P)2 + hsz] —00 T22 T22 TZZ/l’ 2804(h7r (LAW (E1?) (EA?) ’12 2] (EP) 2 3(Ef‘P + 2%)2 (EfP — zhw)2 [(EIBP)A +h2w2] "'00 h —Tm TxxTzz M? 0(a) E214 (EIP) )A(EIBP)AO 0:ch A 70dw [3E( EIPA'l’hAw )2] ) _OO [( (E)f1P +h2w2 J2 [(EP )A+h2w2] Tzz Tzz T22 MzB 0(—) 5A2(EIP)A (EIBP) 20:: [3(EIP)A + EA” 2] / dw 2 -00 [(EAP) 23112102] [( (Ego) +4thw2] -sz Tm Tz zz AAA)AAA_(A)1AAA(EIP) 4(EIBP)Aaxa: +00 / A A [(Efp) +h2w2] [(EFP) +5232] 3 Txx Txx T22 #280 (SA—71:) 32AM (Efp)2 (EIBP)2afx +00 / AAA 2 AAA 2 [(Efp) +W] [(EFP) +11%?) —00 h TA TA TA AP (4—) EAEAWM; 157 / A“ i 2 _00 [(EA) )2+h23w2] [(EIBP) +h2w2] _ Tzz Tzz Tzz ”:3 01h2( _) 18f22(EIP)2(EEP)aBazz (2)2 / dw 2 2 2 -00 [(Efp) +h2w2] [(EPP) +71%?) . (402) In order to simplify Eq. (402), we need to evaluate the integrals contained within this equation. From the Mathematica software package, +001 2 hid“) [( (Efp) +5222]? ((13,310? + W] 2h{[—3(E1P)2EFP + (E50)? x (E) Z + [3(Ei4P)2EIBP ’ (EIBP)3] 10g (E—fi;) + 2(EiqP)3 x (om—:3)— (E:— )l} x 4(E2AP)3EPP[ >2) [Am (E27 AZA “2 = [h2w2+ +(EAP )2] [h2w2+ (EBP2)] 7T A A B 2. (406) EIP (EIP + EIP) When we use Eqs. (403) and (406) in Eq. (402), the result is h AE(3) (0,1) g —Ta:x Txa: T22 ”2:30 ('27.?) 213EE4EPP205$D (EIAPa EIBP) 0A3 Txl‘ TIL‘IE T2 22 #223 O/Bzfgcxa ngI/‘P EIBP 12(E1p +EzBp) — T22 T22 Tzz ”:30 (4h 71') fizzzE‘I AP:EIBP2azB;D (EEP’ EFF) _ ngTzz Tull/£30 $201 aszIPEIP (407) 24(E,AP +E,B P)? ’ Now that we have derived AEéi) 3(0’ 1) for the colinear geometry A and B, let us derive AE(3) (1,0) for this geometry. We can obtain AEOA)B (1,0) by 0A8 interchanging B and A in Eq. (407), N 3h AEéi)3(110): _ TM TN? TZZ/A’fo (16) fmeIBPa 51134230 (EPPvEIP) 159 Tam: Tana: Tzzflfo Erma arrE?P(EIP)2 12(E}3,, + Ef‘ P2) " T22 T22 T22 ”:10 (%’62) fzzElBPasz(E1P1E1P) _ T22 TzszZ#zOIB§zzasz1:3P(EAP2) . (408) 12(E,BP +E, P)2 These results are equivalent to those obtained by Piecuch at the level of the Unsold approximation.63‘66 We are now ready to derive the expression for AEéi; (0, 0) for the colinear geometry of A and B. According to Eq. (363), AE(3) (0, 0) is 0A8 (3) ’72 AEOAB(0,0) = —TQ3T,3T,,, 472 lb . I I x [00th joobAdw ’706 (w,zw—uu,—zw) X [23,, (7:;zw — 2w, —w’) + b333,, (2w; —zw’ — zw, 2(1),) + b§3¢(— —;zw zw +zw, —zw) + b§3¢(— zw; zw— 2w WWI):| (409) w Recall from Eq. (284) that bA ( flu) — 2w, —zw') is 706 , , (OM/14‘ le>(0A|#A IOA> (EAP +zfiw) (EAP +2hw) (411) Recall Eq. (393), 185/1017 (EfP) 2 6 = (OAlue'flaflAAO/ii- (OAl/lflOAHOAI‘fla/lflClA) - (OAlfif/lal04> ,3 3310 (El? WE?) + 12412) (El? -— E35? + 71%) (414) If we let (422 = to), col = w, — 7,0.) , and 0.20 = w, in Eq. (414), the result is b§3¢ (2w; zw’ — 2w, —zw’) = Z (OBIILB lTB><83|fi§ ICE) 1'3 33760 (Ema) —E(()O) + 277-14)) (E83) _ E32,) + zm') (415) In order to simplify Eq. (415), we need an expression for molecule B which is analagous to Eq. (388) for molecule A, specifically A 2.3 A A .;BA 2 (OBI/igerXTBIHgISB> = (Oalufmuflma) 1'3,835£0 A ;B A - (Oalfi?IOB>- (OBlflgflgIOBHOBl/Igl03)o (416) 161 We also need to write the Unsold approximation to b for molecule B. Using Eq. (416) and the Unsold approximation for molecule B in Eq. (415) gives bgw (w; w, — 2w, —-zwl) 2 AB A (OBI/15 H5H§l08>— «)8le IOB> (EBP +zhw) (EBP +zhw) (OBIH? H§IOB>(OBIH§ |03> (EIBP +zhw)(EBP +zhw') (417) Thus the results are equivalent to those obtained by Piecuch, in the Unsold approximation.63’66 162 6 Summary, Concluding Remarks, and Future Per- spectives The charge-density susceptibility x(r, I"; w) of a molecule is defined as the change in the Lil—frequency component 5,06 (r, w) of the electronic charge density at a point r within a molecule, due to a perturbing potential ’08 (r’, w) of frequency w applied at r’ (within linear response), as given by Eq. (1). Several molecu- lar properties, including dipole- and higher-order polarizabilities, dielectric functions, and other properties mentioned in Chap. 1, depend on the charge-density suscepti- bility. We have derived an ab initio expression for the charge-density susceptibility x(r, r’;w) in CISD theory, developed an algorithm for calculating x(r, r’;w) which is based on this expression, and written a program which is based on this al- gorithm. Finally, we have used our program to calculate x(r, r’; w) of H2 as a function of r, r’ , and w in the aug-cc-pVDZ basis set and at the equilibrium bond length of the molecule. Since CISD is equivalent to full CI in a two-electron case, our results are exact within the aug-cc-pVDZ basis. The charge-density susceptibility can be calculated using the method described here, or it can be calculated using several other methods mentioned in Chap. 1. The advantage of the method presented in this work is that one can easily obtain the exact value of x(r, r’; w) for a molecule (in a given basis) at any frequency w. However, using one of the methods mentioned in Chap. 1, one can only obtain the exact value of x(r, I"; w) for a given molecule at limited number of frequencies. According to Eq. (20), the charge-density susceptibility x(r, r’;w) of H2 is finite at all energies hw 75 (E K — E0) . This is demonstrated in Fig. 1, which shows x(r,r’;w) of H2 as a function of y and z with :1: = 0, w = 0, and I" = (0,0, 0). In this case, he = 0, and x(r, r’; w) is small at all r and r’ . Eq. (20) suggests that x(r, r’; w) is singular at energies fiw = (E K - E0) . However, this is the case only for specific excited states \I'K. For example, triplet 163 excited states ‘11 K do not cause singularities in x(r, r’; w) at ha) = (E K — E0) . This is because \110 for H2 is a 129 state (recall the H2 has D00), symmetry), and [16(1‘) (fie (r’)) is spin-independent, so that matrix elements (\Ilolfie (r) Mix) and (\Il Kl fie (r) [\Ilo) (and the corresponding matrix elements of fie (r’)) are non- zero only for singlet excited states \I’ K . This is demonstrated, for example, by Fig. 2, which shows x(r, r’;w) of H2 as a function of y and z with :1: = 0, hw ~ (E1 — E0) ,and r’ = (O, 0, 0) . Although he) ~ (E1 — E0), x(r,r’;w) of H2 is small because W1 is a triplet state. In addition to the fact that x(r, I"; w) vanishes for triplet states, x(r, r’; w) also vanishes for many singlet states when r and r’ take specific values. We have determined which particular types of singlet states contribute to x(r, I"; w) for the H2 molecule. We did this by writing x(r, r’; w) as a sum of products of orbitals evaluated at r and r’ , and determining which types of orbitals are nonzero when evaluated at various r and r’ values. The states that contribute to x(r, r’; w) for particular r and r’ values are determined by the orbitals which are nonzero at those r and r’ . When r = (0, 0,0) or I" = (0, O, 0) ,only 0'9 -type orbitals and WK states with 129 symmetry contribute to x(r, r’;w) . This is because 09 orbitals are the only molecular orbitals of H2 that are nonzero at r = (0, 0,0) or at I" = (0,0, 0) . For example, this is demonstrated in Fig. 3, which shows x(r,r’;w) of H2 as a function of y and 2 with a: = 0, I" = (0,0, 0), and flu ~ (E4 — E0) . The charge-density susceptibility of H2 is singular here because \114 is a 129 state; x(r, r’; (.0) has the shape of a 09 orbital because 09 orbitals are the only nonzero orbitals at r = (0, 0, O) or I" = (0, 0,0) . If r or 1" lies along the molecular axis, 09- and (Tu-type orbitals and excited states ‘11 K with 129 and 12,, symmetries contribute to x(r, r’; w) for H2. This is because both the 09 and 0,) molecular orbitals of H2 are nonzero along the molecular axis. This is demonstrated by Fig. 5, which shows the charge- density susceptibility of H2 as a function of y and 2 with :L‘ = 0, M N (E3 — E0) , and r’ = (0, 0, 0.7) 164 . The charge-density susceptibility is singular because W3 is a 12,, state, and x(r, r’; w) has the shape of a an orbital because both 09 and 0,, orbitals contribute to x(r,r’;w) when r’ = (0, 0, 0.7) . Finally, if r or r’ is in the :L‘Z—plane, only 71'2 and 5x2_y2 orbitals and 1H,, and 1A332.“ states contribute to x(r,r’;w) for H2. To test our x(r, r’; w) calculations, we have used x(r, r’; w) to calculate the CISD polarizabilities an (w), ayy (w), and an (w) for H2 at w = 0 and at several other frequencies in the DZ, DZP, and aug—cc—pVDZ basis sets. We compared our static polarizabilities with the corresponding polarizabilities obtained in the finite field approximation using the MOLPRO17 quantum chemistry software package. The static polarizabilities calculated with the two methods are given in Table 2. There is excellent agreement between the polarizabilities calculated with the two methods. Note that as with the x(r,r’;w) calculations, all polarizability calculations were carried out at the equilibrium bond length of the H2 molecule. According to Eq. (30) in Chap. 1, the polarizability 0105 (w) is continuous when fiw 75 (E K — E0). Eq. (30) also indicates that aag (w) is singular when ha) = (EK — E0) . However, this is not the case for all excited states \11 K . Specifically, as with x(r, r’;w) , triplet states do not contribute to 01030.12). This is because \Ilo for H2 is a 129 state and ya and HH are spin-independent operators, so that matrix elements (‘I’OlHal‘I’K>, (WKIMQIWO), (‘I’OIHfiI‘I’K>, and (\leluglqlx) are nonzero only for singlet states \I/ K of H2. The frequency-dependent polarizability of H2 is also finite at a number of singlet- state transition energies. We determined which types of singlet states cause Clog (w) to be singular at (11.0 = (E K — E0) by determining which symmetries of the com- ponents of the matrix elements (@JIfiOICPJI) (and (CI) Jul [1ng J”’>) in Eq. (37) make the direct product of those symmetries contain the totally symmetric represen- tation of the D00), point group. Since ((PJI is a determinant in (WOI, (‘IIOI must have the same symmetry as ((PJI . Since IQJI) is in I‘IIK), Ill/K) must have 165 the same symmetry as |Jr) . Therefore, we determined the allowable symmetries of (WM and I‘I’K) from MM] and [(1) J!) . Using this analysis, we determined that an (ad) would be singular for singlet \IJ K states with 2: symmetry. Figs. 6 and 7 demonstrate this behavior. In Figs. 6 and 7, an (w) is singular at two frequencies in the DZ, DZP, and aug—cc—pVDZ basis sets. In each basis set, these two frequencies correspond to the energies of transitions to the 112,]L and 212: states of H2. We also determined that 01er (w) is singular for singlet ‘1’ K states with Hut symmetry and that am, (w) is singular for singlet \I’ K states with Huy symmetry. Fig. 8 demonstrates this behavior for 01” (w) . According to Fig. 8, Ozmy (w) is singular at one frequency in the aug—cc-pVDZ basis set, and this frequency corresponds to the energy of a transition to the 111—In: state. Fig. 10 demonstrates this behavior for ayy (w) . According to Fig. 10, am, (w) is singular at one frequency in the aug-cc-pVDZ basis set, and this frequency corresponds to the energy of a transition to the 111-[uy state. The second major topic of this work is intermolecular interactions. We began our study of intermolecular interactions in Chap. 2, where we summarized the main results of several of the major theoretical approaches to intermolecular interactions. In Chap. 3, we reviewed known results for the second-order perturbation correction to the intermolecular interaction energy of two molecules A and B in the polarization approximation. This approximation is valid when the overlap between the electron distributions of the two molecules can be ignored. First, we showed that the second- order intermolecular interaction energy AEézAL is given by Eq. (158), where the first two terms in this equation give the induction energy due to the polarization of each molecule by the field of the permanent dipole of the other. Note that these results are valid within linear response and when we neglect effects caused by the non-uniformity of the field. Second, we used complex contour integration to prove Eq. (159), which is the Casimir-Polder formula with A = E39) — E83) and B = E)? — E62) from reference 106. Using Eq. (179), we showed that the denominator in the third 166 term of Eq. (158) is given by Eq. (159). At this point, we used the expressions for the frequency-dependent polarizabilities of A and B as given by Eqs. (186) and (187) to show that the third term in Eq. (158) is given by Eq. (188). Eq. (188) is the 2nd-order dispersion energy of interaction of A and B. In Chap. 4, we derive the third-order perturbation correction to the intermolecular . . 3 interaction energy AE( ) 0A8 of two molecules A and B in the polarization approxima- tion. In this derivation, we started with AEéiL as given by Eq. (190), with VAB and la/AB given by Eqs. (148) and (196), and with G given by Eqs. (144) - (147), respectively. We show that the third-order intermolecular interaction energy AEéiL is a sum of six terms which are given by Eqs. (214), (222), (230), (253), (271), and (289). Pg. (214), which is first-order in both ,1er and [130, describes higher-order induction effects. The permanent dipole on molecule A produces a field, and this field polarizes molecule B. This produces a reaction field at B that acts back on A. Specifically, the reaction field at B polarizes A, which then gives rise to a field acting on B and this alters the energy of the AB pair due to the permanent dipole of B. The energy of the AB pair is also affected by the higher-order induction effect produced by the same mechanism but with the roles of A and B interchanged. Eqs. (230) and (222), which are third-order in [M0 and third-order in 1130, respectively, describe hyperpolarization effects. The permanent dipole on molecule A produces a field that hyperpolarizes molecule B, and this effect causes an energy change in the AB pair that is given by Eq. (230). Similarly, the permanent dipole on molecule B produces a field that hyperpolarizes molecule A, and this effect causes an energy change in the AB pair that is given by Eq. (222). Eqs. (271) and (253), which are first-order in [4’40 and first-order in #80 , respectively, describe induction-dispersion effects. These effects result from the modification of the AB dispersion energy due to the static fields from the permanent dipoles of A and B. The static field from the perma- nent dipole of A, together with the field from the fluctuating dipole of A, polarizes B nonlinearly, changing its energy. In addition, the field from the permanent dipole of A 167 alters the correlations of the spontaneous charge-density fluctuations on B, and this affects the correlation energy (and similarly, with the roles of A and B interchanged). The induction, hyperpolarization, and induction-dispersion energies given by Eqs. (214), (230), (222), (271), and (253) agree with the results of earlier work. However, Eq. (289), which is zeroth-order in both “A0 and [430 and corresponds to the dispersion energy of the AB pair, is a new result. This is a pure dispersion effect, associated with correlations in the fluctuating charge densities of A and B beyond linear response. Molecule B is hyperpolarized by the fluctuating field from A; also, the fluctuating field from A alters the correlations of the charge-density fluctuations in B. Both mechanisms contribute to the third-order dispersion energy. In Chap. 5, we use our results for A1363; and A138; obtained in Chaps. 3 and 4, the definitions of Tag, HA0, [130,01’4 (2w ) and 05155:) )asgiven by Eqs. (149), (297), (186), and (187) to derive approximations to AEéi) and AE(3)B for specific geometries of A and B. Eq. (306) gives the second-order correction A1302)” to the energy of the AB complex when A and B are colinear, with each of their molecular axes oriented along the z-axis of the labOoratory frame shown in Fig. 12. This equation gives AEéiL in terms of #20 , ”£30 , 01:12, 05;, 01;: (w), 6!sz (w), and RAB . Using Eq. (306) and letting A and B be hydrogen fluoride (HF) molecules, we also derived an expression for the second-order correction to the energy of two colinear HF molecules with their molecular axes oriented along the Z-axis of the laboratory frame. This expression is given by Eqs. (307), (308), and (309), where the total second-order correction to the energy AEOIBF- HF of two HF molecules is the sum of these three 0 HF equations. These equations are given in terms of pH F , an , (1sz (2w), and RH F H F We simplified our expression for AE62) 0 HF_ HP by realizing that for this geometry, we can replace [1H F with pH F0’ in our equations for AE02) HF— HF . By assuming that the matrix elements in the equation for the static polarizability of HF are real and by using the Unsold approximation, we have derived an equation HF( which gives a w) in terms of the ionization potential E jHPF of HF, the static 168 HF 76 HF 76 (w) is polarizability a of HF, and frequency w. This expression for a given by Eq. (316). We also simplified AEOH)F— HF by using Eq. (316) in Eq. . . (2) (309), g1v1ng Eq. (318) for the AEOHF— HF (O, 0) component of AEOJR HF. We further simplified AEOH)—F HF (O, 0) by evaluating the integral over frequencies on in Eq. (318), giving Eq. (325) for AEotin HP (0, 0). Finally, using Eqs. (307) and (308) with 11"” 0) =n_ — 0. 7043 a u and am": 6.36 a. u., we obtained Eq. (310) for both AEOH)—F HF (2,0) and AEm (0, 2). 0HF- HF Also, using Eq. (325) with EIPF = 0.5896 a. u., aHF— — 6.36 a u., and 22 Griff: Gig/F = 5.22 a. u., we obtained Eq. (326). Multiplying Eq. (310) by two and adding the result to Eq. (326), we obtained Eq. (327) for AEOJfl HF . Since Eq. (327) is of the form 06(Hp_Hp)/(RHF_HF)6 . where 06(HF—HF) is a constant, then our results indicate that Cg( HF- H p) = —44.5 a. u. for two colinear HF molecules. We have also derived an expression for AEéiL when the internuclear axes of A and B are parallel to each other and to the :r-axis of the laboratory frame as shown in Fig. 13. In this geometry, the molecular and laboratory frames are not the same. Therefore, before obtaining a final expression for A1363; for this geometry, we rotated the nonzero components of the relevant properties of A and B for the parallel geometry shown in Fig. 13 from the molecular frame to the laboratory frame. We obtained the final expression for A5163; in this geometry by replacing the components in the AEéi; expression for the colinear arrangement of A and B shown in Fig. 12 (Eq. (306)) with the appropriate rotated components. The final expression for AEéiL for parallel A and B as shown in Fig. 13 is given by Eq. (330). We have used Eq. (330) with A = B =HF for AEéiL when A and B are arranged as shown in Fig. 13 to obtain an expression for the second-order correction AEéi; to the energy of interaction between two parallel HF molecules. This expres- sion is given by Eq. (331). We obtain this expression by letting A = B =HF in Eq. 169 (330). We simplified Eq. (331) using essentially the same procedure that we used to simplify Eqs. (307), (308), and (309) for A1363: of two colinear HF molecules (re- call that the sum of Eqs. (307), (308), and (309) gives the total 2nd-order correction (2) to the energy of interaction AE of two colinear HF molecules). After simpli- UHF—HF fying, we obtained Eq. (337) for AEéi)F_HF of two parallel HF molecules. Letting #5“? = 0.7043 a. u., QZF = erg/F = 5.22 a. u., and 0521: = 6.36 a. u. in Eq. (337), we obtained the final expression for AEéi; of two parallel HF molecules, which is given by Eq. (338). Eq. (338) is of the form C6(HF—HF)/(RHF—HF)6 , where 06(HF—HF) is aconstant. According to Eq. (338), 06(HF—HF) = —29.2 a. u. for two parallel HF molecules. We have also derived an expression for AEéi; when A and B are perpendicular to each other, as shown in Fig. 14. In this geometry, the laboratory and molecular frames are the same for A, but they are not the same for B. Therefore, before obtaining an expression for AEéi; for this particular geometry, we rotated the nonzero components of the relevant properties of molecule B from its molecular frame to the laboratory frame. After rotating these components, we obtained an expression for AEéiL in this geometry by replacing the components of molecule B in the colinear expression for AEéiL as given by Eqs. (292) - (293) with the appropriate rotated components. The expressions for the AEéi; (O, 2), AESjRB (2, 0), and AEéi; (0, 0) components of [3133333 for this geometry are given by Eqs. (342), (343), and (344). We have also derived an expression for the second-order correction to the energy of interaction AEm 0430 of three molecules A, B, and C. This energy is a sum of the second-order, two-body corrections AE(2) AESZ) and AEéZ: due to the OAB’ AC’ interactions between A and B, A and C, and B and C, and an irreducible three~body energy of second-order 13136322,. 2,2) ABC. We denote the sum of the second-order two—body corrections AEé Each second-order, two-body correction is a sum of three terms, two induction terms and a dispersion term. For example, as shown in Chap. 170 3, AEéiL is the sum of the induction terms AEéiL (0,2) and AESQA) 3(2’ 0),an the dispersion term AEOA)?2 (O, 0). Similarly, AEéi; is the sum of AESZL (0, 2), AEéi)‘, (2, 0) , and AEOA)C (0, 0), as shown by Eq. (347). Also, as shown by Eq. (348), AE(28)C is the sum of AEéf; (0,2), AE(2B)C (2,0), and AE0:)C (0, 0) .The full nonadditive, 2nd-order correction to the energy AEé2’3) (350). is given by Eq. ABC Eq. (351) contains all contributions to the total second-order correction to the energr of the interaction of molecules A, B, and C. Based on this equation, we have obtained an equation for the total second-order correction to the energy of interaction of three colinear hydrogen fluoride molecules. We call the three HF molecules that we 2nd use in this derivation HF 1, HF2, and HF3, and we call the corresponding -order a ' ' 2 correction to the energy of interaction of these three molecules AEéJFl [”2 HF - " 3 . The three molecules are arranged so that their internuclear axes lie along the z- axis of the laboratory frame, as shown in Fig. 15. We have denoted the distances between the centers of mass of HF 1 and H172, HF 1 and HF 3, and HF 2 and HF3 by RHFl—Hth R115- (H173 , and R3143- 111:3 , respectively. We obtain the desired expression for AEQ) by replacing A, B, and C in Eq. (351) with 01-1171- --—HF2 HF3 HF 1, HFg, and HF3, respectively. This expression for AEOHLF __sz —HF3 is given (2 ,3) ”Fl—HFz—HF3 in Eq. (352) is given by Eq. (350) with molecules A, B, and C replaced by HP 1, HF 2, and HF3. The second-order, two-body terms AEm AEOH F1 OHFI -HF2 ’ by Eq. (352). The irreducible three-body energy of interaction AEO -HF3’ and AEéfiFTHFs in Eq. (352) are given by Eq. (306) with A, B, and C replaced by HF 1, HF 2, and HF3, respectively. According to Eq. (327), the second-order correction to the energy of interaction of two colinear HF molecules is AE(2) OHF— HF‘ = --44.5 a.u./(R1151- HF)6. We simplify Eq. (352) for AE0H)F1_M,2_W,3 by realizing (2) (2) . . that AEOW,1 —HF2 , AEOHL, _3HF , and AEOHF2-HF3 are all g1ven by Eq. (327) With the appropriate substitutions of HF], HF2, or HF3 for HF. We also simplify Eq. 171 . (2,3) (352) by replacmg AEOHFl—HFz—HFa AE(2 3) which is given by Eq. (356). 0HF1—-HF2 -3HF’ in Eq. (352) with a geometry-specific form of We have also derived an expression for the 2nd-order correction to the energy of interaction AEOH)F1_ of HFl, HF2, and HF 3 when these three HF molecules —HF2— HF3 ara parallel to each other. The three molecules are arranged so that their internuclear axes are parallel the x-axis of the laboratory frame, as shown in Fig. 16. Although Eq. (352) in our derivation of AE3:)F1_ ”F2 —HF3 applies to three colinear molecules, it is general enough that we used it as our starting point for deriving AEOH F1” F2” F 3 for three parallel HF molecules. The irreducible three-body energy of interaction AE‘z') ”3 in Eq. (352) for three parallel HF molecules is also given by Eq. OHFI— --HF2 HF3 (350), with molecules A, B, and C replaced by HFI, HF2, and HF3. According to Eq. (338), the second-order correction to the energy of interaction of two parallel HF HF_ HF —- ——29.2 a.u./(RHF_HF)6 . We Simplify Eq). (352) for this geometry by realizing that AE(2) AEm and AE02) are OHF —2HF’ OHF -3aHF’ HFz- -HF3 molecules is AEé2) all given by Eq. (338) with the appropriate substitutions of HF], HF2, and HF3 for HP. We also simplify Eq. (352) by replacing AEéiib HF _HF in Eq. (352) with a . 2 ,3 geometry spec1fic form of Eq. AEéfl’FL HF2- -3HF , which 18 given by Eq. (361). Using the expression for AEOA; derived in Chap. 4, which is correct for any geometry of the AB complex, we have also derived an expression for AEéi; when A and B are colinear. This expression is given by Eq. (290) in Chap. 4, and again by Eq.) (362) in Chap. 5. Recall that Eq. (362) consists of six terms, which are (3) (3) (3) E(3) E053 (1,1), AEOAB (3,0), AEOAB(O,3), AEOAB (1, 0),A B,(0 1), and :EOA)B (O, 0). The equations for each of these six terms are listed in Eq. (363). We derive the overall expression for AE33)B when A and B are colinear by) deriving the expressions for AE$)B,(11), AEéi; (3,0), AEéiL (0,3), AEOiL (1,0), AEOA)B (0, 1), and AE0:)B (0, 0) separately, and then adding all of the resulting expressions together. Note that in this geometry, the internuclear axes of A and B are oriented along the z-axis of the laboratory frame, as shown in Fig. 12. 172 First, we show that EOAB )(1, 1) in this geometry is given by Eq. (367). GA B 022? C1227 RAB . Next, we show that AEé? 3(0’ 3) and AEGi); (3,0) (in this geometry) In this equation, AE(3)B,(1 1) is given in terms of 11,0 , ”£30 , and are given by Eqs. (370) and (373),A respectively. Eq. (370) is given in terms of [1:30, 182221 and RAB , and Eq. (373) is given in terms of 11:10, 52 , and RAB- Numerical values of an and fizzz are available for many molecules. Also, for this geometry, ”:10 = ”A0 and #280 = ,uBO, and numerical values of [LAO and HBO are also available for many molecules. We then show that AEOA)B (0, 1) is given by Eq. (375) which contains Tm, Tyy, Tu, [150, each diagonal component of the frequency-dependent polarizability 01A (w), and several components of ,BA (—zw; 2w, 0). We simplified Eq. (375) by replacing Tm, Tyy , and T22 with the appropriate expressions for these quantities given in terms of RAB , and by replacing 11,30 with ”BO. We also simplified Eq. (375) by letting HF: A in Eq. (317), and using these expressions for A A m: yy ities a? x(zw), 0:14,!(260), and 0124,0122) given by Eq. (317) (with HF: A) are given 14 .A 1131:, ayyia zzi a (w), a (w), and 0A z'(zw) in Eq. (375). The expressions for the polarizabil- in terms of the static polarizabilities a the ionization potential E 1 P of A, and the frequency w . The static polarizabilities and ionization potential are known for many molecules, so that it is easy to compute 03:42 (W), 03y (w), and A 2, (w) for these molecules. (1 To complete our simplification of Eq. (375), we needed to replace the various components of 3A (—zw; 2w, 0) with expressions that contain quantities whose numerical values are known. Using the expression for the frequency-dependent hy- perpolarizabilityfi [3170— -—;zw 2w ,0) given by Eq. (394), the Unsold approximation, and a few manipulations of Eq. (394), we showed that 22,7 (—zw; 2w, 0) is given by Eq. (399). We also used the expression for the static polarizability fig?” given by Eq. (376), the Unsold and closure approximations, and other manipulations to show 173 that the matrix elements in Eq. (399) for 3:37 (—zw; 2w, 0) are given by Eq. (393). We obtained our final expression for £7 (-—zw; 2w, 0), given by Eq. (400), by using Eq. (393) in Eq. (399), and by combining the denominators in Eq. (399). Eq. (400) depends on 18.2017: Efp, and w. Since these quantities are known for several molecules, one can easily compute fig?” (—zw; zw, 0) using Eq. (400). Equations for specific components of ,3607 (— w; w, 0) can be obtained by replacing 6, Oz, and ’y in Eq. (400) with the appr0priate Cartesian coordinates. At this point, we obtained a simplified expression for AEéi; (0, 1) by replacing fizm(-— 2w; zw ,,0) z@y(—w;zw,0), and £34,, (—zw;ua,0) in Eq. (375) with Eq. (400), with the appropriate substitutions for 5, Oz, and ’7 . This expression E(3) EOAB AE(3A) (0, 1) , given by Eq. (407), by evaluating the integrals in Eq. (402). We OAB for (0,1) is given by Eq. (402). We obtained the final expression for derived the final expression for AEéi; (1,0) by interchanging A and B in Eq. (407). We presented the final expression for AEéiL (1,0) in Eq. (408). The last step in deriving an expression for AEéi; for the interaction between A and B when they are colinear (with their internuclear axes oriented along the Z-axis of the laboratory frame) involved the simplification of the expression for AE03)B (0, 0) containedin Eq. (362). The form of AE(3)B (0, 0) inEq. (362) for AEéAL isgiven in Eq. (363). To begin our simplification, we showed that (1’4 is given by Eq. (413). Here, Eq. (413) gives bA 7016 (w; 210' — 2w, —zw') 706 (w; zw — 2w, —zw’) in terms of 3,405 , E3413 , and w . It is possible to give béficb (w; zw’ — w, —zw’) and the other frequency-dependent (353.1 terms contained in AEéi; (0, 0) in terms of 5,534, , EB; , and w . Since numerical values of static polarizabilities and ionization potentials are available for many 3molecules, it is possible to use our expression for AE(3) (0, 0) to compute AEéi) 3(0’0) at various RAB and w. 0A3 There are several possibilities for future work on the charge-density susceptibility x(r, l"; w) . Future applications of the charge-density susceptibility include calcu- lating X (r, I"; w) for several other centrosymmetric diatomic molecules such as N2, 174 02, Clo, and F 2, and also for noncentrosymmetric diatomic molecules such HF, HCl, and CO. We may also calculate X (r, r’; w) for small polyatomic atomic molecules such as H20, and 002. We may also calculate x(r, I"; w) for H2 in higher level basis sets and compare x(r, r’; (.0) obtained in different basis sets to determine the relative contributions of different orbital types to x(r, I"; w) of H2. We may also calculate x(r, r’; w) of other molecules mentioned above as a function of basis set. This would allow us to determine the relative contributions of different orbital types to x(r, I"; w) for these molecules. We plan to improve our results for x(r, r’; w) of H2 by calculating x(r, I"; w) of H2 at all of the same conditions as those used in this work, with the exception of the step sizes Ag and AZ between 3] and 2 data points (recall that we have x = 0 ). Specifically, we plan on calculating x(r, r’ ;w) of H2 with step sizes Ay and AZ that are smaller than the current step sizes. This will allow us to determine if X (r, r’; w) for H2 calculated with smaller step sizes has features that are unresolved in our results for X (r, r'; w) of H2. If we calculate x(r, r’; w) of other molecules, we can also calculate x(r, I"; w) of these molecules as a function of step size. From these calculations, we can determine if the shape of x(r, r’; w) for these molecules is independent of Ag and A2, or if we resolve more features of x(r, r’; w) as we decrease Ag and AZ. Other future work may involve modifying the current program for calculating x(r, r’; w) to improve its efficiency and speed. We could improve the efficiency and speed of our program by explicitly removing triplet states and singlet states with improper symmetries from the sum-over-states calculation of x(r, r’; w). Depending on the results of x(r, I"; w) calculations for different molecules, r values, r’ values, and to values, it may also be possible to develop programs to approximate X(r, 1"; w)- Another very important future project involves the development of algorithms and 175 would be to develop algorithms and write computer programs that use x(r, r’; w) to calculate other properties, including dipole and higher-order polarizabilities, induc— tion and dispersion energies for interacting molecules, infrared intensities, and nonlo- cal intramolecular dielectric functions. We have given an extensive list of molecular properties related to x(r, r’; w) in Chap. 1. Future work on intermolecular interactions will involve comparing the results of the calculations presented here with the corresponding results of similar calculations presented in the literature. For example, we plan to compare the values of C 6 obtained here for AE3:)F_HF of two colinear and of two parallel HF molecules with the corresponding values of Cs obtained by Meath and co—workers,289 and similarly for two perpendicular HF molecules. We also plan to compare C9 values for three HF molecules with the corresponding values of Meath et. al..289 176 Appendices 177 Appendix A. Fortran CISD Code for Calculating x(r, r’; w) and flag (w) 178 00000000000 0000000000000000000000000000000000000 Appendix A. Fortran CISD Code for Calculating x(r, r’; w) and (lag (w) PROGRAM CHICALC This program solves the configuration-interaction with singles and doubles (CISD) eigenvalue problem for the specified molecule and computes the charge-density susceptibility of that molecule at coordinates r = x, y, z, and r’ = x’, y’, z’. The program also computes the xx, yy, 22, and xy components of the polarizability of the molecule. Declare that all variables with names that begin with letters A-H or 0-2 will be double-precision numbers. IMPLICIT DOUBLE PRECISION (A-H, D-Z) Description of all variables and/or arrays used in the program: NRE = Integer array whose values correspond to the number of irreducible representations in the C1 (lst element) point group; the C2, CS, and CI point groups (2nd element); the C2V, C2H, and D2 (3rd element) point groups; and the D2H point group (4th element). MC = Integer array which contains the irreducible represen- tations of the C1, C2, C8, CI, C2V, C2H, D2 and D2H point groups. IG = Integer set to the number of irreducible representations in the point group. GRP = Point group of molecular system (character variable). GRPREP = One-dimensional character array (with at most eight elements) which is set to the list of (symbols for the) ir— reducible representations for the point group of the molecule. SYMMl = One-dimensional array of integers. The value of each element represents the symmetry of a spatial orbital in the molecular system. The symmetries are arranged according to the energies of their corresponding orbitals. SYMM2 = One-dimensional array of integers. The value of each element represents the symmetry of a spin orbital in the molecular system. The symmetries are arranged according to the energies of their corresponding orbitals. IRREP = Two-dimensional integer array which contains the ir- reducible representations of the symmetries of all spin orbitals in the molecule. 179 0000000000000000000000000000000000000000000000000000000 NOCC1 = Number of occupied spatial orbitals. NUNDCCI = Number of unoccupied spatial orbitals. NTDTl = Total number of spatial orbitals. NTDT2 = Total number of spin orbitals. NELEC = Number of electrons in the molecular system. SPIN2 = One-dimensional array of integers. The value of an element with an odd index is +1, and the value of an element with an even index is -1. The value of each element corres- ponds to the spin that an electron would have if it were to occupy that spin orbital (and if the value of the element were multiplied by 0.5). RSYM2 = Two-dimensional integer array which represents the symmetry of each occupied orbital in the reference deter- minant (each occupied orbital has between one and eight values associated with it, depending on the point group of the molecule. These associated values correspond to the irreducible representation of the orbital’s symmetry). RTOTSYM2 = One-dimensional integer array which represents the overall symmetry of the reference (the array is the irreducible representation which represents the overall symmetry of the reference determinant). C = Two-dimensional array of integers which is used to construct all possible (but not necessarily spin or symmetry allowed) determinants. The first index refers to the determinant number (to count and distinguish between determinants), and the second index refers to a spin orbital. The element corresponding to a par- ticular determinant and orbital will have a value of 1 or 0 if the orbital is occupied or unoccupied, res- pectively. NC = Integer variable which is used to keep track of the total number of determinants (not necessarily spin or symmetry allowed). CSPIN = One-dimensional array whose index corresponds to determinant number, and each of whose elements has a value which (when multiplied by 0.5) corresponds to the total spin of a specific determinant. C2 = Two-dimensional array of integers which is used to construct all possible spin-allowed determinants. The first index refers to the determinant number (to count and distinguish between determinants), and the second index refers to a spin orbital. The element corresponding to a particular determinant and orbital will have a value of 1 or 0 if the orbital is occupied or unoccupied, 180 0000000000000000000000000000000000000000000000000000000 respectively. NC2 = Integer variable which is used to keep track of the total number of spin-allowed determinants. CIRREP2 = Two-dimensional integer array which contains the irreducible representations for the overall symmetries of all possible spin-allowed determinants. C3 = Two-dimensional array of integers which is used to construct all possible spin- and symmetry-allowed determinants. NC3 = Integer variable which is used to keep track of the total number of spin- and symmetry-allowed determinants. H = CISD Hamiltonian matrix (consists of all possible mat- rix elements formed from the Hamiltonian operator and two determinants). TDTDIFF = Two-dimensional array of integers used to keep track of the total number of occupation differences bet- ween any two spin- and symmetry-allowed determinants. For example, if two electrons are in different orbitals in I and J, then TOTDIFF(I,J) will be set to two. E1SPAT = Array of one-electron integrals and indeces. This array is read from the "*.int.out" input file, which is generated by a GAMESS calculation. The integrals and indeces in this array are in terms of spatial orbitals. E2SPAT = Array of two-electron integrals and indeces. This array is read from the "*.int.out" input file, which is generated by a GAMESS calculation. The integrals and indeces in this array are in terms of spatial orbitals. VNN = Nuclear repulsion energy. Read from "*.int.out" input file. INPUT4 = Character variable (length 5) used when reading one- and two-electron integral information from the "*.int.out" input file. CJ = Two-dimensional array of coefficients which are produced when the CISD eigenvalue problem is solved. Each CISD wavefunction is a linear combination of deter- minants weighted by these coefficients. The first index in this array corresponds to the determinant number, and the second index corresponds to the state number. E = One-dimensional array of energy eigenvalues produced when the CISD eigenvalue problem is solved. The elements of the array are arranged in order of increasing energy. FFWDRK = One-dimensional array corresponding to the FWDRK 181 0000000000000000000000000000000000000000000000000000000 array in the rsm subroutine (see rsm subroutine for an explanation of the FWORK array). IIWORK = One-dimensional array corresponding to the IWORK array in the rsm subroutine (see rsm subroutine for an explanation of the IWDRK array). CJSUM = One-dimensional array. Each element contains the sum of the squares of all the CJ coefficients for a par- ticular state. NAO Total number of atomic orbitals. NMO Total number of molecular orbitals. OMEGA = Frequency variable, read from input file. This variable indicates what frequency should be used to cal- culate the charge-density susceptibility. DOEFF = Two-dimensional array of coefficients for con- verting atomic orbitals into molecular orbitals. Read from the "mod..." input file. CHI = Value of the charge-density susceptibility at the r = x, y, z and r’ = x’, y’, z’ coordinates (shifted by the nuclear coordintes) of interest. AAMU = Three-dimensional array of dipole-moment integ- rals. The first and second indeces in this array corres- pond to atomic orbital number, and the third index, which goes from 1 to 3, corresponds to x (1), y (2) or z (3). This array is read from the "fort.250" input file. POLXX = xx-component of the polarizability of the molecule of interest. POLYY = yy-component of the polarizability of the molecule of interest. POLZZ = zz-component of the polarizability of the molecule of interest. POLXY = xy-component of the polarizability of the AAO = One-dimensional array of atomic orbitals evaluated at r = x, y, z (shifted by the relevant nuclear coor- dinates). These values are provided by the ADROUT sub routine (the A0 array in the ADROUT subroutine is returned to the main program as AAO). ARPRIME = One-dimensional array of atomic orbitals evaluated at r’ = x’, y’, z’ (shifted by the relevant nuclear coordinates). These values are provided by the AORDUT subroutine (the A0 array evaluated at r’ = x’, y’, z’ (shifted by nuclear coordinates) in the AOROUT subroutine is returned to the main program as ARPRIME). AVEC = One-dimensional array used to facilitate reading 182 000000 of $VEC group from "mod..." GAMESS input file. STUFF, STUFF2 = Character variables 80 characters in length which are used to read lines from the "fort.250" input file. CHARACTER fileinp*80 INTEGER MC,NRE DIMENSION MC(8,8,4),NRE(4) CHARACTER GRP*3,GRPREP*3 DIMENSION GRPREP(8) INTEGER SYMM1,SYMM2 DIMENSION SYMM1(100),SYMM2(200) INTEGER IRREP DIMENSION IRREP(200,8) INTEGER SPIN2 DIMENSION SPIN2(200) INTEGER RSYM2,RTOTSYM2 DIMENSION RSYM2(200,8),RTOTSYM2(8) INTEGER C,C2,C3 DIMENSION C(10000,200),C2(10000,200) INTEGER CSPIN DIMENSION CSPIN(1000O) INTEGER CIRREP2 DIMENSION CIRREP2(10000,8) CHARACTER INPUT4*5,INPUT3*80 INTEGER TOTDIFF DIMENSION TOTDIFF(10000,1000O) COMMON /BLOCK1/ H(10000,10000) COMMON /BLOCK2/ EISPAT(100,100) COMMON /BLOCK3/ E2SPAT(100,100,100,100) COMMON /BLOCK4/ C3(10000,200) COMMON /BLOCK6/ NTOT2 COMMON /BLOCK12/ NC3 COMMON /BLOCK15/ NAO DIMENSION AAO(100),ARPRIME(100) DIMENSION E(10000) DIMENSION CJ(10000,10000) DIMENSION FFWORK(80000) DIMENSION IIWORK(1000O) DIMENSION CJSUM(1000O) DIMENSION ABIG1(50,50,50,50) DIMENSION ABIG2(50,50,50,50) DIMENSION AVECCS) DIMENSION DCOEFF(100,100) 183 0 2283 473 472 474 6009 6010 6008 6007 6006 6005 CHARACTER STUFF*80,STUFF2*80 DIMENSION AAMU(100,100,3) DIMENSION B(10000,50,50) DIMENSION BAOl(10000,50,50) DIMENSION BAO(10000,50,50) DIMENSION ILEFT(5000,5000) DIMENSION IRIGHT(5000,5000) DIMENSION ISIGNRHO(5000,5000) DIMENSION IOK1(5000) DIMENSION IOK2(5000) Set all of the elements in each array equal to zero. DO 472 II=1,100,1 DO 473 JJ=1,100,1 DCOEFF(II,JJ)=0.0d0 DO 2283 KK=1,3,1 AAMU(II,JJ,KK)=0.0d0 CONTINUE CONTINUE CONTINUE DO 474 IK=1,5,1 AVECCIK)=0.0d0 CONTINUE DO 6008 I=1,10000,1 CSPIN(I)=0 DO 6009 J=1,200,1 C(I.J)=O C2(I,J)=O CONTINUE DO 6010 J=1,8,1 CIRREP2(I,J)=0 CONTINUE CONTINUE DO 6007 I=1, RTOTSYM2( CONTINUE 8,1 I)=0 DO 6005 I=1,200,1 SPIN2(I)=0 SYMM2(I)=0 DO 6006 J=1,8,1 RSYM2(I,J)=0 IRREPCI,J)=0 CONTINUE CONTINUE DO 6020 II=1,100,1 DO 6002 J=1,100,1 EISPAT(II,J)=0.0D0 DO 6003 K=1,100,1 184 C 0 6004 6003 6002 6020 6063 6062 6061 6060 6136 6135 6130 224 223 222 6000 DO 6004 L=1,100,1 E2SPAT(II,J,K,L)=0.0D0 CONTINUE CONTINUE CONTINUE SYMM1(II)=0 AAOCII)=0.0D0 CONTINUE DO 6060 IP=1,50,1 DO 6061 IQ=1,50,1 DO 6062 IT=1,50,1 DO 6063 IU=1,50,1 ABIGI(IP,IQ,IT,IU)=0.0d0 ABIG2(IP,IQ,IT,IU)=0.0d0 CONTINUE CONTINUE CONTINUE CONTINUE DO 6130 I=1,10000,1 DO 6135 M=1,50,1 DO 6136 N=1,50,1 B(I,M,N)=0.0d0 CONTINUE CONTINUE CONTINUE DO 222 I=1,10000,1 E(I)=0.0DO CJSUMCI)=0.0D0 IIWORK(I)=0 DO 224 J=1,200,1 C3(I,J)=0 CONTINUE DO 223 J=1,10000,1 H(I,J)=0.0D0 TOTDIFF(I,J)=0 CJ(I,J)=0.0D0 CONTINUE CONTINUE DO 6000 I=1,80000,1 FFWORK(I)=0.0D0 CONTINUE Use data groups to set the values in the NRE and MC arrays. DATA NRE/1,2,4,8/ DATA MC/ 00 0 00000 0 00 9998 000 0000 0000 00000 ”RPEPWPRPK’RPK’ 0,0,0,0,0,0,0,0, 0 0 0,0,0 0 0 0 1,1,1,1,0,0,0,0, 1,1,-1,-L 0,0,0, 0, 1, 1, 1, L 0, 0, 0, 0, 1,-1,-1,1,0,0,0,0, 0,0,0,0,0,0,0,0, 0,0 ,0,0,0, 0 ,0,0, 0,0,0,0,0,0,0,0, 0,0,0,0,0,0,0,0, 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,-1,1,1,-1,-1,1, 1,-1,-1,1,-1,1,1,-1/ Open the input file containing the basic molecular information. call getenvC’INPUT’,fi1einp) open(unit=20,file=fileinp,status=’unknown’,form=’formatted’) Read the number of occupied orbitals, the number of unoccupied orbitals, and the total number of orbitals from the input file (all spatial orbitals). READ(20,*)NOC01,NUNOCC1,NTOT1 Set the total number of spin orbitals. NTOT2=NTOT1*2 Read the point group of the molecular system from the input file. FORMATCAB) READ(20,9998)GRP Read the symmetries of the spatial orbitals into the SYMM1 array. READ(20,*) (SYMM1(I), I=1,NTOT1) Compute the number of electrons and set the result to NELEC. NELEC=NOCCI*2 Read the frequency to be used for calculating the charge-density susceptibility into OMEGA. READ(20,*)OMEGA WRITE(6,*)’Frequency:’,OMEGA CALL FLUSHCG) Set the symmetries of the spin orbitals (using the symmetries of the spatial orbitals, which are contained in the SYMM1 array). DO 26 I=1,NTOT1,1 SYMM2((2*I)-1)=SYMM1(I) SYMM2(2*I)=SYMM1(I) 26 CONTINUE 186 0000000 0000 000000 00 000000 000000 28 30 34 33 32 Assign spin to each spin orbital in the system. (Note: The spins are assigned to orbitals rather than electrons to facilitate computation. Also, the spins are set to integers rather than +1/2 or -1/2 for the same reason). DO 28 I=1,NTOT1,1 SPIN2((2*I)-1)=1 SPIN2(2*I)=-1 CONTINUE Set the total number of all possible determinants (not necessarily spin and symmetry-allowed) to 1. NC=1 Construct the reference determinant. If a spin orbital is occupied in the reference determinant, the value of the corresponding element will be set to 1. If a spin orbital is not occupied, the value of the corresponding element will be set to zero. DO 30 I=1,NELEC,1 C(NC,I)=1 CONTINUE Increment the total number of determinants. NC=NC+1 Construct all possible (but not necessarily spin or sym- metry allowed) singly-excited determinants. Increment the total number of determinants each time a new determinant is produced. DO 32 I=1,NELEC,1 DO 33 J=(NELEC+1),NTOT2,1 C(NC,J)=1 DD 34 K=1,NELEC,1 IF (K.EQ.I) THEN ELSE C(NC,K)=1 ENDIF CONTINUE NC=NC+1 CONTINUE CONTINUE Construct all possible (but not necessarily spin or sym- metry allowed) doubly-excited determinants. Increment the total number of determinants each time a new determinant is produced. DO 55 I=1,(NELEC-1),1 DO 56 J=(I+1),NELEC,1 187 000000 0000 0000 0000000 59 58 57 56 55 68 67 74 73 DO 57 K=(NELEC+1),NTOT2,1 DO 58 L=(K+1),NTOT2,1 C(NC,K)=1 C(NC,L)=1 DO 59 M=1,NELEC,1 IF (M.EQ.I .OR. M.EQ.J) THEN ELSE C(NC,M)=1 ENDIF CONTINUE NC=NC+1 CONTINUE CONTINUE CONTINUE CONTINUE Decrease the total number of determinants by one to prevent improper counting of the total number of singly- and doubly-excited determinants (the previous loop overcounts the total number of determinants). NC=NC-1 Determine the total spin of each possible (but not necessarily spin- or symmetry-allowed) determinant. DO 67 I=1,NC,1 DO 68 J=1,NTOT2,1 IF (C(I,J).EQ.1) THEN CSPIN(I)=CSPIN(I)+SPIN2(J) ELSE ENDIF CONTINUE CONTINUE Set the total number of spin-allowed determinants to one. NC2=1 Determine which of the determinants in the C array are spin-allowed. Add the spin-allowed determinants to the C2 array. Increment the total number of spin-allowed determinants each time a determinant in the C array is added to the C2 array. DO 73 I=1,NC,1 IF (CSPIN(I).EQ.CSPIN(1)) THEN DO 74 J=1,NTOT2,1 C2(NC2,J)=C(I,J) CONTINUE NC2=NC2+1 ELSE ENDIF CONTINUE 188 000000 000000 Decrease the total number of spin-allowed determinants by one to prevent improper counting of these deter- minants (the previous loop overcounts the total number of spin-allowed determinants). NC2=NC2-1 According to the point group, set the irreducible rep- ‘resentations of the molecule. Point groups that can be handled by this program are: C1, C2, CS, CI, C2V, C2H, D2, and D2H. IF (GRP.EQ.’C1’) THEN IG=1 GRPREP(1)=’A’ ENDIF IF (GRP.EQ.’CZ’) THEN IG=2 GRPREP(1)=’A’ GRPREP(2)=’B’ ENDIF IF (GRP.EQ.’CS’) THEN IG=2 GRPREP(1)="A’" GRPREP(2)="A”" ENDIF IF (GRP.EQ.’CI’) THEN IG=2 GRPREP(1)=’Ag’ GRPREP(2)=’Au’ ENDIF IF (GRP.EQ.’C2V’) THEN IG=3 GRPREP(1)=’A1’ GRPREP(2)=’A2’ GRPREP(3)=’BI’ GRPREP(4)=’B2’ ENDIF IF (GRP.EQ.’D2’) THEN IG=3 GRPREP(1)=’A’ GRPREP(2)=’B1’ GRPREP(3)=’B2’ GRPREP(4)=’83’ ENDIF IF (GRP.EQ.’C2H’) THEN IG=3 GRPREP(1)=’Ag’ GRPREP(2)=’Au’ GRPREP(3)=’Bg’ GRPREP(4)=’Bu’ ENDIF IF (GRP.EQ.’D2H’) THEN IG=4 189 0000 GRPREP(1)=’Ag’ GRPREP(2)=’Au’ GRPREP(3)=’Blg’ GRPREP(4)=’Biu’ GRPREP(5)=’B2g’ GRPREP(6)=’B2u’ GRPREP(7)=’BBg’ GRPREP(8)=’BBu’ ENDIF Set the irreducible representation for the symmetry of each occupied and unoccupied spin orbital in the molecule. DO 108 I=1,NTOT2,1 IF (SYMM2(I).EQ.1) THEN DO 109 J=1,8,1 IRREP(I,J)=MC(1,J,IG) 109 CONTINUE ENDIF IF (SYMM2(I).EQ.2) THEN DO 110 J=1,8,1 IRREP(I,J)=MC(2,J,IG) 110 CONTINUE ENDIF IF (SYMM2(I).EQ.3) THEN DO 111 J=1,8,1 IRREP(I,J)=MC(3,J,IG) 111 CONTINUE ENDIF IF (SYMM2(I).EQ.4) THEN DO 112 J=1,8,1 IRREP(I,J)=MC(4,J,IG) 112 CONTINUE ENDIF IF (SYMM2(I).EQ.5) THEN DO 113 J=1,8,1 IRREP(I,J)=MC(5,J,IG) 113 CONTINUE ENDIF IF (SYMM2(I).EQ.6) THEN DO 114 J=1,8,1 IRREP(I,J)=MC(6,J,IG) 114 CONTINUE ENDIF IF (SYMM2(I).EQ.7) THEN DO 115 J=1,8,1 IRREP(I,J)=MC(7,J,IG) 115 CONTINUE ENDIF IF (SYMM2(I).EQ.8) THEN DO 116 J=1,8,1 IRREP(I,J)=MC(8,J,IG) 116 CONTINUE ENDIF 108 CONTINUE 190 0000 000000 00000 0000 0 0000 133 132 119 123 120 126 125 129 128 127 Set the irreducible representations of each occupied orbital in the reference determinant. DO 132 I=1,NELEC,1 DO 133 J=1,8,1 RSYM2(I,J)=IRREP(I,J) CONTINUE CONTINUE Set (initialize) each element in the RTOTSYM2 array (the array which will be set to the overall symmetry of the reference determinant) to one. DO 119 I=1,8,1 RTOTSYM2(I)=1 CONTINUE Determine the overall symmetry of the reference determinant by calculating the product of the irreducible representations (for the symmetries of the orbitals) of all occupied orbitals in the reference determinant. DO 120 I=1,NELEC,1 DO 123 J=1,8,1 RTOTSYM2(J)=RTOTSYM2(J)*RSYM2(I,J) CONTINUE CONTINUE Set (initialize) the value of each element in the CIRREP2 array to one. DO 125 I=1,10000,1 DO 126 J=1,8,1 CIRREP2(I,J)=1 CONTINUE CONTINUE Determine the overall symmetry of each spin-allowed determinant. DO 127 I=1,NC2,1 D0 128 J=1,NTOT2,1 IF (C2(I,J).EQ.1) THEN DO 129 K=1,8,1 CIRREP2(I,K)=CIRREP2(I,K)*IRREP(J,K) CONTINUE ELSE ENDIF CONTINUE CONTINUE Set the total number of spin- and symmetry-allowed determinants to one. NC3=1 191 00000 000000 00 0000 0000 139 140 138 137 621 620 Determine whether each spin-allowed determinant in the C2 array is also symmetry-allowed. If a determinants in the C2 array is symmetry-allowed, add it to the C3 array. DO 137 I=1,NC2,1 DO 138 J=1,8,1 IF (CIRREP2(I,J).EQ.RTOTSYM2(J)) THEN GO TO 139 ELSE GO TO 137 ENDIF IF (J.EQ.8) THEN DO 140 K=1,NTOT2,1 C3(NC3,K)=C2(I,K) CONTINUE NC3=NC3+1 ELSE ENDIF CONTINUE CONTINUE Decrease the total number of spin- and symmetry-allowed deter- minants by one to prevent improper counting of these deter- minants (the previous loop overcounts the total number of spin- and symmetry-allowed determinants). NCB=NC3-1 Write all spin and symmetry allowed determinants. WRITE(6,*)’Spin- and Symmetry-Allowed Determinantsz’ CALL FLUSH(6) DO 620 I=1,NC3,1 WRITE(6,*)’Determinant: ’,I CALL FLUSH(6) WRITE(6,*)’Occupied Orbitalsz’ CALL FLUSH(6) D0 621 J=1,NTOT2,1 IF (C3(I,J).EQ.1) THEN WRITE(6.*)J CALL FLUSH(6) ENDIF CONTINUE CONTINUE Close the input file containing the basic molecular information. CLOSE (20) Open the input file containing the one- and two-electron integrals. 192 00000 00 153 0000000 1507 0000 1509 0000000 0000000000 OPEN (UNIT=21 , &FILE=’h2cisd_MBS_C1.int.out’, &STATUS=’OLD’) Set the number of data-containing lines in the one- and two-electron integral file (represented by the variable NLINE) to zero. NLINE=0 Read the first five characters in the input file into INPUT4. FORMAT(A5) READ(21,153)INPUT4 If the first five characters of the input file are not blank spaces (meaning data is present), increment the number of of data-containing lines, and read the first five charac- ters in the next line. Continue to read and count lines until there are no more data-containing lines. IF (INPUT4.NE.’ ’) THEN NLINE=NLINE+1 READ(21,153)INPUT4 GO TO 1507 ENDIF Return to the beginning of the data-containing lines, backing up one line at a time. DO 1509 I=1,(NLINE+1),1 BACKSPACE(21) CONTINUE Read the first five characters of the current line (this is a check to make sure that we are at the beginning of the data -- if desired, print these characters to find out if we are indeed at the beginning of the data). Then return to the beginning of the current line. READ(21,153)INPUT4 BACKSPACE(21) Read the two- and one-electron integrals and indeces into the E2SPAT and EISPAT arrays, respectively. Also, read the nuclear repulsion energy into the variable VNN. Note: The input file’s list of integrals does not include all possible one- and two-electron integrals. Therefore, we will complete the list while reading the integrals from the input file. (The variable for the integral values is XXX, and the variable(s) for the integral indeces are IP,IQ,IR, and IS). DO 1510 I=1,NLINE,1 READ(21,*) XXX,IP,IQ,IR,IS IF (IR.NE.0) THEN 193 0000 0000000000000000 1510 149 E2SPAT(IP,IQ,IR,IS)=XXX E2SPAT(IQ,IP,IR,IS)=XXX E2SPAT(IP,IQ,IS,IR)=XXX E2SPAT(IQ,IP,IS,IR)=XXX E2SPAT(IR,IS,IP,IQ)=XXX E2SPAT(IS,IR,IP,IQ)=XXX E2SPAT(IR,IS,IQ,IP)=XXX E2SPAT(IS,IR,IQ,IP)=XXX ELSE IF (IP.NE.0 .AND. IQ.NE.0 .AND. IR.EQ.0 .AND. IS.EQ.0) THEN E1SPAT(IP,IQ)=XXX EISPAT(IQ,IP)=XXX ELSE IF (IP.EQ.0 .AND. IQ.EQ.0 .AND. IR.EQ.0 .AND. IS.EQ.0) THEN VNN=XXX ENDIF ENDIF ENDIF CONTINUE Close the input file containing the one- and two-electron integrals. CLOSE(21) For each pair of determinants (I,J) in which J is greater than or equal to I, subtract the occupation number in J from the occupation number in I for each spin orbital in the molecule, sum these differences, and set the result to TOTDIFF(I,J). Then, divide TOTDIFF(I,J) by two to determine the total number of spin-orbital occupation differences between the two determinants. If the two determinants differ by more than two occupancies, set H(I,J) to zero. If I and J differ by two occupancies, call subroutine (SLATER2) for forming two-electron integrals from two determinants that differ by two spin orbital occupancies. If I and J differ by one occupancy, call subroutine (SLATERi) for forming one- and two-electron integrals from two determinants that differ by one spin orbital occupancy. DO 9100 I=1,NC3,1 DO 9101 J=1,NC3,1 IF (J.GE.I) THEN DO 149 K=1,NTOT2,1 TOTDIFF(I,J)=TOTDIFF(I,J)+ & ABS(C3(I,K)-C3(J,K)) CONTINUE IF ((TOTDIFF(I,J)/2).GT.2) THEN H(I,J)=0.0D0 ELSE ENDIF IF ((TOTDIFF(I,J)/2).EQ.2) THEN 194 00000000000000000000 CALL SLATER2(I,J) ELSE ENDIF IF ((TOTDIFF(I,J)/2).EQ.1) THEN CALL SLATER1(I,J) ELSE ENDIF If I and J are the same, determine which spin orbitals are occupied in both I and J. Convert each spin orbital K (if occupied) in I and J to spatial orbital KS. Then, add the one-electron integral in which KS is occupied in both I and and J (E1SPAT(KS,KS)) to the Hamiltonian matrix element H(I,J). Also, for each pair of occupied spin orbitals L and M in I (and in J) in which M is greater than or equal to L, convert L and M to spatial orbitals LS and MS, calculate the spins of LS and MS, and set these spins to LSPIN and MSPIN. Then, if the spins LSPIN and MSPIN are the same, add the antisymmetrized two-electron integral for these orbitals to the Hamiltonian matrix element H(I,J). The antisymmetrized two-electron integral is E2SPAT(LS,LS,MS,MS) - E2SPAT(LS,MS,MS,LS). If spins LSPIN and MSPIN are different, add the two-electron integral EZSPAT(LS,LS,MS,MS) to H(I,J). Note: For an explanation of the calculations of matrix elements H(I,J), review the Slater rules for calculating one- and two-electron matrix elements of the Hamiltonian. IF ((TOTDIFF(I,J)/2).EQ.0) THEN DO 160 K=1,NTOT2,1 IF (C3(I,K).EQ.1) THEN IF (MOD(K,2).EQ.0) THEN KS=(K/2) ELSE ENDIF IF (MOD(K,2).EQ.1) THEN KS=((K+1)/2) ELSE ENDIF H(I,J)=H(I,J)+E1SPAT(KS,KS) ELSE ENDIF 160 CONTINUE ELSE ENDIF IF ((TOTDIFF(I,J)/2).EQ.O) THEN DO 161 L=1,NTOT2,1 DO 162 M=1,NTOT2,1 IF (M.GT.L) THEN IF (C3(I,L).EQ.1 .AND. & C3(I,M).EQ.1) THEN IF (MOD(L,2).EQ.0) THEN LS=(L/2) LSPIN=-1 ELSE ENDIF 195 000000 0000 IF (MOD(L,2).EQ.1) THEN LS=((L+1)/2) LSPIN=1 ELSE ENDIF IF (MOD(M,2).EQ.0) THEN MS=(M/2) MSPIN=-1 ELSE ENDIF IF (MOD(M,2).EQ.1) THEN MS=((M+1)/2) MSPIN=1 ELSE ENDIF IF (LSPIN.EQ.MSPIN) THEN H(I,J)=H(I,J)+ & E2SPAT(LS,LS,MS,MS)- & E2SPAT(LS,MS,MS,LS) ELSE ENDIF IF (LSPIN.NE.MSPIN) THEN H(I,J)=H(I,J)+ & E2SPAT(LS,LS,MS,MS) ELSE ENDIF ELSE ENDIF ELSE ENDIF 162 CONTINUE 161 CONTINUE ELSE ENDIF ELSE ENDIF 9101 CONTINUE 9100 CONTINUE For each pair of determinants (I,J) with J greater than I, set TOTDIFF(J,I) equal to TOTDIFF(I,J). TOTDIFF(I,J) was calculated in the previous loop. This can be done because the Hamiltonian matrix H(I,J) is Hermetian. DO 2025 I=1,NC3,1 DO 2026 J=1,NC3,1 IF (J.GE.I) THEN TOTDIFF(J,I)=TOTDIFF(I,J) ENDIF 2026 CONTINUE 2025 CONTINUE For each pair of determinants (I,J) with J greater than I, set H(J,I) equal to H(I,J). H(I,J) was calculated in the previous loop. This can be done because the Hamiltonian matrix H(I,J) 196 174 173 0000000000 2003 00000000 000000 00000 is Hermetian. DO 173 IL=1,NC3,1 DO 174 JL=1,NC3,1 IF (JL.GE.IL) THEN H(JL,IL)=H(IL,JL) ENDIF CONTINUE CONTINUE List the matrix elements of the Hamiltonian. WRITE(6,*)’CISD Hamiltonian matrix elements:’ CALL FLUSH(6) DO 2001 I=1,NC3,1 DO 2002 J=1,NC3,1 WRITE(6,*)I,J,H(I,J) CALL FLUSH(6) CONTINUE CONTINUE Set each diagonal matrix element within the set H(NC3+1,NC3+1) ...H(10000,10000) to 1000. This is done to facilitate the operation of the rsm subroutine. This enables the main program to provide rsm with a fixed-dimension Hamiltonian matrix H without preventing rsm from solving variably-sized CISD eigen- value problems. DO 2003 NH=NC3+1,10000,1 H(NH,NH)=1000.0D0 CONTINUE Set the error indicator IIERR (for the rsm subroutine) to 1,000 (This will ensure that if the value of IIERR is zero, then it is zero because rsm set it to zero and not by default). Note: IIERR in the main program corresponds to IERR in the rsm sub- routine. Also, if IIERR is zero, the rsm subroutine ran without generating any errors. IIERR=1000 Call the subroutine for solving the CISD eigenvalue problem. Note: To determine what each of the arguments in the rsm call statement corresponds to, see the comments for this program and the rsm subroutine. CALL rsm(10000,10000,H,E,NC3,CJ,FFWORK,IIWORK,IIERR) For each eigenvector, calculate the sum of the squares of the coefficients for that eigenvector. Print the sum of the squares of the coefficients, if desired. DO 2023 LK=1,NCB,1 DO 2024 LL=1,NC3,1 197 2024 c c & 2023 00000 8821 0000000000 CJSUM(LK)=CJSUM(LK)+(CJ(LL,LK)**2) CONTINUE WRITE(6,*)’Eigenvector:’,LK,’Sum of squares of coeffs.:’, CJSUM(LK) CONTINUE For each state I, calculate and write the difference between the energy of the Ith eigenvector and the 1st eigenvector (i.e., calculate the resonances). WRITE(6,*)’Resonances:’ CALL FLUSH(6) DO 8821 I=1,NC3,1 WRITE(6,*)(E(I)-E(1)) CALL FLUSH(6) CONTINUE Write the CI coefficients. WRITE(6,*)’Determinant ’, ’State ’,’CJ(Determinant, State)’ CALL FLUSH(6) DO 2382 I=1,NC3,1 DO 2383 J=1,NC3,1 WRITE(6,*)I,J,CJ(I,J) CALL FLUSH(6) CONTINUE CONTINUE Open the "mod..." input file, which is the input file for a GAMESS CISD energy calculation. OPEN (UN IT=23 , &FILE=’mod_h2cisd_MBS_C1.inp’, &STATUS=’OLD’, FORM=’FORMATTED’) 00000 6100 000000 6102 0000 Read the first line (actually, the first 80 characters of the line, which is essentially the whole line) of the input file into INPUTS. FORMAT(A80) READ(23,6100)INPUT3 If the first five characters of the first line in the input file are NOT " $VEC", then read the next line of the input file. Continue reading lines in the input file until the first five characters of the line ARE " $VEC". DO 6102 WHILE (INPUT3(1:5).NE.’ $VEC’) READ(23,6100)INPUT3 CONTINUE Set ICOUNT (an integer variable which will be used to keep track of the number of lines in the " $VEC" group) to zero. 198 ICOUNT=0 If the first five characters of the current line ARE " $VEC", read the next line in the input file and increment ICOUNT. Continue to read lines and increment ICOUNT until a line whose first five characters are " $END" is read. 000000 IF (INPUT3(1:5).EQ.’ $VEC’) THEN DO 4446 WHILE (INPUT3(1:5).NE.’ $END’) READ(23,6100)INPUT3 ICOUNT = ICOUNT + 1 4446 CONTINUE ENDIF : Set a new variable, JCOUNT, equal to ICOUNT plus one. c JCOUNT = ICOUNT + 1 2 Return (by rewinding line by line) to the line whose c first five characters are " $VEC". c DO 4447 IBACK = 1, JCOUNT BACKSPACE (23) 4447 CONTINUE Read the current line. It should be the " $VEC" line (you have to print the contents of the line to make sure). This is the beginning of the GAMESS " $VEC" group. The actual data begins on the next line. 000000 READ(23,6100)INPUT3 Read the contents of the " $VEC" group into the DCOEFF array. Note: The " $VEC" group always has a very specific format -- the first number in every line is an integer representing the molecular orbital number, the second number is an integer representing the current line number (each molecular orbital has a certain number of lines of coefficients in the " $VEC" group), and the last five numbers are coeffients for converting the atomic orbitals into molecule orbitals. The 4448 statement gives the format for reading these lines. 0000000000000 4448 FORMAT (I2, 1X, I2, 5E15.8) 0 DO 6103 IVROW=1,ICOUNT-1 READ (23,4448) IMO,LIN,(AVEC(JVCOL),JVCOL=1,5) DO 6104 IVCOL=1,5 IAO=(LIN-1)*5+IVCOL DCOEFF(IAO,IMO)=AVEC(IVCOL) 6104 CONTINUE 6103 CONTINUE c 199 Set the total number of molecular orbitals NMO equal to the number of the molecular orbital IMO whose coefficients were just read into DCOEFF. Set the total number of atomic orbitals IAO equal to the total number of molecular orbitals. 00000 NMO=IMO NAO=NMO Write (if desired) the coefficients for converting the atomic orbitals to molecular orbitals. WRITE(6,*)’Coefficients for converting a.o.s to m.o.s:’ CALL FLUSH(6) WRITE(6,*)’ao mo coeff’ CALL FLUSH(6) DO 8831 I=1,NAO,1 DO 8832 J=1,NAO,1 WRITE(6,*)I,J,DCOEFF(I,J) CALL FLUSH(6) C8832 CONTINUE C8831 CONTINUE 000000000000 c c Close the "mod..." input file. c CLOSE(23) c c Open the file containing the dipole moment integrals. c OPEN (UNIT=25, FILE=’fort.250’, &STATUS= ’ OLD ’ , FORM= ’ FORMATTED ’ ) c c Read the first line (actually, the first 80 characters c of the first line) into STUFF, and read the second line c (again, the first 80 characters of the second line) into c STUFF2. c 2277 FORMAT(A80) READ(25,2277)STUFF READ(25,2277)STUFF2 c c Calculate the total number of lines of data in the c file containing the dipole moment integrals and set c this number equal to LIM. This number is obtained c by multiplying the square of the number of atomic c orbitals (NAO‘2) by three. c LIM=(NAO*NAO*3) c c Read the dipole moment integrals into the AAMU array. c Also, write these integrals, if desired. c c WRITE(6,*)’IJ ’,’KJ ’,’LJ ’,’AAMU(IJ,KJ,LJ)’ c CALL FLUSH(6) DO 2276 NL=1,LIM,1 READ(25,*)IJ,KJ,LJ,XXX 200 C C 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2276 902 904 903 901 AAMU(IJ,KJ,LJ)=XXX WRITE(6,*)IJ,KJ,LJ,AAMU(IJ,KJ,LJ) CALL FLUSH(6) CONTINUE Close the "fort.250" input file. CLOSE(25) Set each matrix element in the ILEFT, IRIGHT, ISIGNRHO, B, BAOl and BAO arrays equal to zero. DO 901 IKH=1,NC3,1 DO 902 JKH=1,NC3,1 ILEFT(IKH,JKH)=0 IRIGHT(IKH,JKH)=0 ISIGNRHO(IKH,JKH)=0 CONTINUE DO 903 JKH=1,NTOT1,1 DO 904 KKH=1,NTOT1,1 B(IKH,JKH,KKH)=0.0d0 BA01(IKH,JKH,KKH)=0.0d0 BAO(IKH,JKH,KKH)=0.0d0 CONTINUE CONTINUE CONTINUE *************************************************** At this point, we will begin to calculate the matrix elements of the electronic charge-density operator involving determinants that differ by one spin orbital occupancy. *************************************************** For each pair of configurations (II, JJ), where JJ is less than II and II and JJ differ by only one spin orbital occupancy, determine the spin orbital which is occupied in II and vacant in JJ and set this orbital equal to ILEFTS. Then, convert spin orbital ILEFTS to a spatial orbital and set the result equal to ILEFT(II,JJ). Similarly, determine the spin orbital which is occupied in JJ and vacant in II and set this orbital equal to IRIGHTS. Then, convert spin orbital IRIGHTS to a spatial orbital and set the result equal to IRIGHT(II,JJ). DO 7001 II=2,NC3,1 DO 7002 JJ=1,(II-1),1 IF ((TOTDIFF(II,JJ)/2).EQ.1) THEN DO 410 KJ=1,NTOT2,1 IF ((C3(II,KJ)-C3(JJ,KJ)).EQ.1) THEN 201 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 410 448 449 7002 7001 ILEFT(II,JJ)=((KJ+1)/2) ILEFTS=KJ ENDIF IF ((C3(JJ,KJ)-C3(II,KJ)).EQ.1) THEN IRIGHT(II,JJ)=((KJ+1)/2) IRIGHTS=KJ ENDIF CONTINUE Set ISUMLEFT (a variable which will be used to determine the number of occupied spin orbitals in II that are before ILEFTS) and ISUMRIGHT (a variable which will be used to determine the number of occupied spin orbitals in JJ that are before IRIGHTS) equal to zero. ISUMLEFT=0 ISUMRIGHT=0 Count the number of occupied spin orbitals in II that occur before ILEFTS. For each of these occupied orbitals, increment ISUMLEFT. Then, count the number of occupied spin orbitals in JJ that occur before IRIGHTS. For each of these occupied orbitals, increment ISUMRIGHT. DO 448 ML=1,ILEFTS,1 IF (C3(II,ML).EQ.1) THEN ISUMLEFT=ISUMLEFT+1 ENDIF CONTINUE DO 449 MK=1,IRIGHTS,1 IF (C3(JJ,MK).EQ.1) THEN ISUMRIGHT=ISUMRIGHT+1 ENDIF CONTINUE Now, we will determine the sign of the matrix element of the electronic charge-density operator involving determinants II and JJ, and set the result equal to ISIGNRHO(II,JJ). The default value of ISIGNRHO is -1. If determinants II and JJ have the same number of occupied spin orbitals before ILEFTS and IRIGHTS (respectively), then set ISIGNRHO equal to 1. ISIGNRHO(II,JJ)=-1 IF (ISUMLEFT.EQ.ISUMRIGHT) THEN ISIGNRHO(II,JJ)=1 ENDIF ENDIF CONTINUE CONTINUE ********************************************************* 202 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 415 7003 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 At this point, we are almost done calculating the matrix elements of the electronic charge-density operator involving determinants that differ by one spin orbital occupancy. Before finishing this calculation, however, we will begin to calculate the matrix elements of the electronic charge- density operator involving identical determinants. ********************************************************* For each pair of identical determinants (II, II), set the IOK1(II) and IOK2(II) matrix elements equal to zero. Then, find the first occupied spin orbital in determinant II, convert this spin orbital to a spatial orbital, and set the result to IOK1(II). Then, find the second occupied spin orbital in determinant II, convert this spin orbital to a spatial orbital, and set the result to IOK2(II). DO 7003 II=1,NC3,1 IOK1(II)=0 IOK2(II)=0 DO 415 KJ=1,NTOT2,1 IF ((C3(II,KJ).EQ.1) .AND. (IOK1(II).NE.0)) THEN IOK2(II)=((KJ+1)/2) ENDIF IF ((C3(II,KJ).EQ.1) .AND. (IOK1(II).EQ.0)) THEN IOK1(II)=((KJ+1)/2) ENDIF CONTINUE CONTINUE ********************************************************* We are almost done calculating the matrix elements of the electronic charge-density operator involving identical determinants. Before finishing this calculation, however, we will finish calculating the matrix elements of the electronic charge-density operator involving determinants that differ by one spin orbital occupancy. We now have enough information to begin computing the CI coefficients’ contribution to the charge-density susceptibility. ********************************************************* For each determinant II, where II is determinant 2 or larger, set the CI coefficient for the II determinant and state 1 equal (CJ(II,1)) to CJIND. Then, for each pair of determinants (II,JJ), where JJ is less than II and where the two determinants differ by only one spin orbital occupancy, set ILEFT(II,JJ) (determined earlier -- ILEFT(II,JJ) is the spatial orbital corresponding to the spin orbital that is occupied in II but not in JJ) equal to LL1. Also, set IRIGHT(II,JJ) (determined 203 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 6997 7005 7004 CONTINUE 0 0 0 0 0 000000000 6998 7007 7006 earlier -- IRIGHT(II,JJ) is the spatial orbital corres- ponding to the spin orbital that is occupied in JJ but not in II) equal to MM1. At this point, we will assign the sign of the matrix element of the electronic charge- density operator involving determinants II and JJ (ISIGHRHO(II,JJ) to the CI coefficients’ contribution to the charge-density susceptibility for this matrix element by multiplying ISIGNRHO(II,JJ) by CJIND, setting the result equal to VAL, and multiplying VAL by CJ(JJ,K). Then, we complete the calculation of the CI coefficents’ contribution to the charge-density susceptibility for for these matrix elements by determining CJ(JJ,K)*VAL for each excited state K, and setting the result equal to B(K,LL1,MM1). DO 7004 II=2,NC3,1 CJIND=CJ(II,1) DO 7005 JJ=1,(II-1),1 IF ((TOTDIFF(II,JJ)/2).EQ.1) THEN LL1=ILEFT(II,JJ) MM1=IRIGHT(II,JJ) VAL=(ISIGNRHO(II,JJ)*CJIND) DO 6997 K=2,NC3,1 B(K,LLl,MM1)=B(K,LL1,MM1)+(CJ(JJ,K)*VAL) CONTINUE ENDIF CONTINUE Repeat the process described in the above paragraph for all pairs of determinants (II, JJ), where II and JJ differ by one spin orbital occupancy and where JJ is GREATER than II. DO 7006 II=1,(NC3-1),1 CJIND=CJ(II,1) DO 7007 JJ=(II+1),NC3,1 IF ((TOTDIFF(II,JJ)/2).EQ.1) THEN LL1=ILEFT(JJ,II) MM1=IRIGHT(JJ,II) VAL=(ISIGNRHO(JJ,II)*CJIND) DO 6998 K=2,NC3,1 B(K,LL1,MM1)=B(K,LL1,MM1)+(CJ(JJ,K)*VAL) CONTINUE ENDIF CONTINUE CONTINUE ******************************************************** We have finished calculating the CI coefficients’ contribution to the charge-density susceptibility for matrix elements of the electronic charge-density operator involving pairs of determinants (II, JJ) that differ by one spin orbital occupancy. 204 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 6999 7008 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Now, we will calculate the CI coefficients’ contribution to the charge-density susceptibility for matrix elements of the electronic charge-density operator involving pairs of identical determinants (II, II). ******************************************************** For each determinants II, set the spatial equivalent of the first occupied spin orbital in II (i.e., IOK1(II)) equal to LL1, and set the spatial equivalent of the second occupied spin orbital in II (i.e., IOK2(II)) equal to MM1. Then, set the CI coefficient for the II determinant and the ground state (i.e., CJ(II,1)) equal to CJIND. At this point, we will split the calculation of the CI coefficients’ contribution to the charge-density susceptibility for matrix elements of the electronic charge-density operator involving identical determinants (II, II) into two parts: We we calculate the contribution due to spatial orbitals LL1 and MM1 separately. Specifically, for each excited state K, we will calculate the CI coefficients’ contribution to the charge-density susceptibility due to orbital LL1 by multiplying the coefficient for determinant II and state K (i.e., CJ(II,K)) by CJIND, and setting this result equal to B(K,LL1,LL1). Similarly, we will calculate the same contribution for each K due to orbital MM1 by multiplying CJ(II,K) by CJIND and setting the result equal to B(K,MM1,MM1). DO 7008 II=1,NC3,1 LL1=IOK1(II) MM1=IOK2(II) CJIND=CJ(II,1) DO 6999 K=2,NC3,1 B(K,LL1,LL1)=B(K,LL1,LL1)+(CJ(II,K)*CJIND) B(K,MM1,MM1)=B(K,MM1,MM1)+(CJ(II,K)*CJIND) CONTINUE CONTINUE ******************************************************** We have finished calculating the CI coefficients’ contribution to the charge-density susceptibility. Next, calculate the expansion coefficients’ (i.e., the coefficients for converting atomic orbitals to molecular orbitals) contribution to the susceptibility, and combine this with the CI coefficients’ contribution to the charge-density susceptibility. ******************************************************** DO 7014 K=2,NC3,1 DO 7011 LKH=1,NTOT1,1 205 0 0 0 0 0 0 0 0 0 0 7013 7012 7011 & 7016 7015 7010 7014 6036 6035 6034 DO 7012 JKH=1,NTOT1,1 DO 7013 MKH=1,NTOT1,1 BAO1(K,LKH,JKH)=BAOI(K,LKH,JKH)+ (B(K,LKH,MKH)*DCOEFF(JKH,MKH)) CONTINUE CONTINUE CONTINUE DO 7010 IKH=1,NTOT1,1 DO 7015 JKH=1,NTOT1,1 DO 7016 LKH=1,NTOT1,1 BAO(K,IKH,JKH)=BAO(K,IKH,JKH)+ (BA01(K,LKH,JKH)*DCOEFF(IKH,LKH)) CONTINUE CONTINUE CONTINUE CONTINUE Write the contents of the BAO array, if desired. WRITE(6,*)’K,KK,LL,BAO(K,KK,LL)’ CALL FLUSH(6) DO 6034 K=2,NC3,1 DO 6035 KK=1,NAO,1 DO 6036 LL=1,NAO,1 WRITE(6,*)K,KK,LL,BAO(K,KK,LL) CALL FLUSH(6) CONTINUE CONTINUE CONTINUE *************************************************************** Complete the calculation of the contribution of all coefficients to the charge-density susceptibilty, and add the frequency dependence to the susceptibility. *************************************************************** DO 6040 NP=1,NAO,1 DO 6041 NQ=1,NAO,1 DO 6042 NT=1,NAO,1 DO 6043 NU=1,NAO,1 DO 6044 K=2,NC3,1 ABIG1(NP,NQ,NT,NU)=ABIGI(NP,NQ,NT,NU) & +((BAO(K,NP,NQ)*BAO(K,NT,NU))/(E(K)-E(1)-OMEGA)) ABIG2(NP,NQ,NT,NU)=ABIG2(NP,NQ,NT,NU) & +((BAO(K,NP,NQ)*BAO(K,NT,NU))/(E(K)-E(1)+OMEGA)) 6044 6043 6042 6041 6040 CONTINUE CONTINUE CONTINUE CONTINUE CONTINUE Write the ABIG arrays, if desired. 206 0 0 0 0 0 0 c c6048 c6047 c6046 & DO 6045 NP=1,NAO,1 DO 6046 NQ=1,NAO,1 DO 6047 NT=1,NAO,1 DO 6048 NU=1,NAO,1 WRITE(6,*)NP,NQ,NT,NU, ABIG1(NP,NQ,NT,NU) CALL FLUSH(6) CONTINUE CONTINUE CONTINUE C6045 CONTINUE C 0 0 0 0 0 0 c c6052 c6051 c6050 & DO 6049 NP=1,NAO,1 DO 6050 NU=1,NAO,1 DO 6051 NT=1,NAO,1 DO 6052 NU=1,NAO,1 WRITE(6,*)NP,NQ,NT,NU, ABIG2(NP,NQ,NT,NU) CALL FLUSH(6) CONTINUE CONTINUE CONTINUE C6049 CONTINUE 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 ***************************************************** Calculate the charge-density susceptibility at each specified x, y, z and x’, y’, 2’. For each x, y, z and x’, y’, z’, calculate the contribution of the atomic orbitals evaluated at these points to the susceptibility, and combine this result with the coefficients’ contribution to the susceptibility. Also, calculate the xx, yy, zz, and xy components of the polarizability. Unlike the susceptibility, however, the polarizability components will only be calculated once, since these quantities are calculated from integrals over all x, y, z. ***************************************************** Set the values of x’, y’ and z’ to XRP, YRP, and ZRP, respectively. XRP=0.0d0 YRP=0.0d0 ZRP=0.0d0 Call the subroutine (i. e., subroutine AOROUT) for evaluating the atomic orbitals at any x, y, z or x’, y’, 2’. Obtain the values of the atomic orbitals evaluated at x’, y’, and z’ from AOROUT. These values will be returned from AOROUT in the AAO array. 207 00 00000 6369 6871 000000000000000000000000000 CALL AOROUT(XRP,YRP,ZRP,AAO) Write x’, y’, and z’. WRITE(6,*)’r-prime:’,XRP,YRP,ZRP CALL FLUSH(6) Set each AAO(N) equal an ARPRIME(N) (essentially, create an array which is identical to AAO and name it ARPRIME). DO 6369 N=1,NAO,1 ARPRIME(N)=AAO(N) CONTINUE Write the ARPRIME array, if desired. DO 6871 J=1,NAO,1 WRITE(80,*)ARPRIME(J) CONTINUE Use the three nested do loops that immediately follow to choose the grid of x, y, 2 points at which to calculate the spatial dependent part of the susceptibility. Use the I, J, and K loops to set up the x, y, and z coordinates, respectively. Each x coordinate (XX) is selected by taking the value of I (where I essentially corresponds to the number of the x point), multiplying this by DELTAXX (which is the x increment), and adding this to XXO (the initial x). The y (YY) and z (22) coordinates are set up in the same way. When I, J, and K are all equal to one, set the variables used for calculating the xx, yy, zz, and xy components of the polarizability equal to zero. Note: POLXX1, POLXX2, POLYY1, POLYY2, POLZZl, POLZZ2, POLXY1, and POLXY2 are intermediate variables used in calculating the xx (POLXX), yy (POLYY), zz (POLZZ), and xy (POLXY) components of the polarizability. DO 6361 I=1,1 DO 6362 J=1,1 DO 6363 K=-1,1 IF (I.EQ.1 .AND. J.EQ.1 & .AND. K.EQ.1) THEN POLXX1=0.0d0 POLXX2=0.0d0 POLYY1=0.0d0 POLYY2=0.0d0 POLZZl=0.0d0 POLZZ2=0.0d0 POLXY1=0.0d0 208 000000 000000 POLXY2=0.0d0 POLXX=0.0d0 POLYY=0.0d0 POLZZ=0.0d0 POLXY=0.0d0 ENDIF XXO=0.0d0 YYO=0.0d0 ZZO=0.0d0 DELTAXX=0.0d0 DELTAYY=0.0d0 DELTAZZ=0.05d0 XX=(XXO+I*DELTAXX) YY=(YYO+J*DELTAYY) ZZ=(ZZO+K*DELTAZZ) Call the AOROUT subroutine for evaluating the atomic orbitals at x, y, z. The atomic orbitals will be evaluated at XX, YY, 22 and their values will be returned to the main program in the AAO array. CALL AOROUT(XX,YY,ZZ,AAO) Write the x (XX), y (yy), and z (22) coordinates, if desired. WRITE(6,*)XX,YY,ZZ CALL FLUSH(6) A1SUM4=0.0d0 A2SUM4=0.0d0 DO 5365 IM=1,NAO,1 A1$UM3=0.0d0 A2SUM3=0.0d0 DO 5366 JM=1,NAO,1 A1$UM2=0.0d0 A2SUM2=0.0d0 DO 5367 KM=1,NAO,1 A1SUM1=0.0d0 A2SUM1=0.0d0 DO 5368 LM=1,NAO,1 A1SUM1=A1SUM1+ (ABIGl(IM,JM,KM,LM)*ARPRIME(LM)) IF (I.EQ.1 .AND. J.EQ.1 .AND. & K.EQ.1) THEN POLXX1=POLXX1+ (ABIG1(IM,JM,KM,LM)*AAMU(IM,JM,1) *AAMU(KM,LM,1)) 209 0 0000 POLXX2=POLXX2+ & (ABIG2(IM,JM,KM,LM)*AAMU(IM,JM,1) & *AAMU(KM,LM,1)) POLYY1=POLYY1+ & (ABIGi(IM,JM,KM,LM)*AAMU(IM,JM,2) & *AAMU(KM,LM,2)) POLYY2=POLYY2+ & (ABIG2(IM,JM,KM,LM)*AAMU(IM,JM,2) & *AAMU(KM,LM,2)) POLZZl=POLZZI+ & (ABIGi(IM,JM,KM,LM)*AAMU(IM,JM,3) & *AAMU(KM,LM,3)) POLZZ2=POLZZ2+ & (ABIG2(IM,JM,KM,LM)*AAMU(IM,JM,3) & *AAMU(KM,LM,3)) POLXY1=POLXY1+ & (ABIGI(IM,JM,KM,LM)*AAMU(IM,JM,1) & *AAMU(KM,LM,2)) POLXY2=POLXY2+ & (ABIG2(IM,JM,KM,LM)*AAMU(IM,JM,1) & *AAMU(KM,LM,2)) ENDIF A2SUM1=A2SUM1+ & (ABIG2(IM,JM,KM,LM)*AAO(LM)) 5368 CONTINUE AISUM2=AISUM2 & +(AISUM1*ARPRIME(KM)) A2SUM2=A2SUM2 & +(A2SUM1*AAO(KM)) 5367 CONTINUE A1$UM3=A1SUM3+(A13UM2*AAO(JM)) A2SUM3=A2SUM3+(A2SUM2 & *ARPRIME(JM)) 5366 CONTINUE A1SUM4=A1$UM4+(A1SUM3*AAO(IM)) A2SUM4=A2SUM4+(A2SUM3*ARPRIME(IM)) 5365 CONTINUE CHI=A1SUM4+A2SUM4 Write the value of the charge-density susceptibility at x (XX), y (YY), z (22). WRITE(6,*)CHI CALL FLUSH(6) 210 Write the xx, yy, 22, and xy components of the polarizability. Note: These will only be written once; when I, J, and K equal one. 0000 IF (I.EQ.1 .AND. J.EQ.1 & .AND. K.EQ.1) THEN POLXX=POLXX1+POLXX2 WRITE(6,*)’POLXX:’,POLXX CALL FLUSH(6) POLYY=POLYY1+POLYY2 WRITE(6,*)’POLYY:’,POLYY CALL FLUSH(6) POLZZ=POLZZi+POLZZ2 WRITE(6,*)’POLZZ:’,POLZZ CALL FLUSH(6) POLXY=POLXY1+POLXY2 WRITE(6,*)’POLXY:’,POLXY CALL FLUSH(6) ENDIF C 6363 CONTINUE 6362 CONTINUE 6361 CONTINUE C END 0 SUBROUTINE SLATER1(II,JJ) This subroutine evaluates the matrix elements of pairs of determinants which differ in the location of one electron. 0000 IMPLICIT DOUBLE PRECISION (A-H,O-Z) 0 INTEGER C3 COMMON /BLOCK1/ H(10000,10000) COMMON /BLOCK2/ E1SPAT(100,100) COMMON /BLOCK3/ E2SPAT(100,100,100,100) COMMON /BLOCK4/ C3(10000,200) COMMON /BLOCK6/ NTOT2 COMMON /BLOCK12/ N03 COMMON /BLOCK15/ NAO 11A=0 I2A=0 Determine where (i.e., what spin orbitals) determinants II and JJ differ, and set these orbitals to 11A and 12A. 0000 DO 151 L=1,NTOT2,1 211 00000000000 00 000000 0 000 00000 IF ((C3(II,L)-C3(JJ,L)).EQ.1 & .AND. I1A.EQ.0) THEN IiA=L ENDIF IF (((C3(II,L)-C3(JJ,L)).EQ.(-1)) & .AND. I1A.NE.L .AND. I2A.EQ.0) THEN I2A=L ENDIF 151 CONTINUE Determine the sign of the Hamiltonian matrix element which is being formed from determinants II and JJ, where II and JJ differ in the occupation of one spin orbital. First, count the number of occupied orbitals in determinant II that are lower in energy than the first orbital with different occupancies in II and JJ, and set the total to (Before beginning, set SUMI1A to zero). SUMIlA=0.0D0 DO 448 ML=1,(IlA-1),1 IF (C3(II,ML).EQ.1) THEN SUMI1A=SUMI1A+1.0D0 ENDIF 448 CONTINUE Multiply SUMIlA by -1 and set the result to SIGNIiA. SIGNIIA=((-1.0D0)**SUMIIA) Count the number of occupied orbitals in determinant JJ that are lower in energy than the second orbital with different occupancies in II and JJ, and set the total to SUMI2A. (Before beginning, set SUMI2A to zero). SUMI2A=0.0D0 DO 449 MK=1,(I2A-1),1 IF (CB(JJ,MK).EQ.1) THEN SUMI2A=SUMI2A+1.0DO ENDIF 449 CONTINUE Multiply SUMI2A by -1 and set the result to SIGNI2A. SIGNI2A=((-1.0D0)**SUMI2A) Determine the overall sign of H(II,JJ) by multiplying SIGNIIA by SIGNI2A and setting the result equal to SIGNIA. SIGNIA=(SIGNI1A*SIGNI2A) 212 000000000 00000 0000 Convert the spin orbitals 11A, I2A to spatial orbitals I1AS and I2AS, respectively. Each unique pair of consecutively-numbered spin orbitals is assigned to the same spatial orbital. Also, set the spins of I1AS and I2AS. If the spin orbital is even, set the spin of IlAS or I2AS to -1, and if the spin orbital is odd, set the spin of IlAS or I2AS to +1. (IlASPIN=spin of IlAS, I2ASPIN=spin of I2AS) IF (MOD(I1A,2).EQ.0) THEN IlAS=(11A/2) I1ASPIN=-1 ELSE IF (MOD(IlA,2).EQ.1) THEN IIAS=((I1A+1)/2) IlASPIN=1 ENDIF ENDIF IF (MOD(I2A,2).EQ.0) THEN I2AS=(I2A/2) I2ASPIN=-1 ELSE IF (MOD(I2A,2).EQ.1) THEN I2AS=((I2A+1)/2) I2ASPIN=1 ENDIF ENDIF Determine if the one-electron integral contribution to the Hamiltonian matrix element H(II,JJ) is spin-conserved. If so, add this integral to H(II,JJ). IF (IlASPIN.EQ.I2ASPIN) THEN H(II,JJ)=H(II,JJ)+E1SPAT(IlAS,I2AS) ENDIF Convert the two-electron integral contribution(s) to H(II,JJ) to (an) integra1(s) over spatial orbitals. DO 2000 K=1,NTOT2,1 IF (K.NE.IlA .AND. K.NE.I2A .AND. C3(II,K).EQ.1) THEN IF (MOD(K,2).EQ.0) THEN KS=(K/2) KSPIN=-1 ELSE IF (MOD(K,2).EQ.1) THEN KS=((K+1)/2) KSPIN=1 ENDIF ENDIF IF (I1ASPIN.EQ.I2ASPIN .AND. & I2ASPIN.EQ.KSPIN) THEN H(II,JJ)=H(II,JJ)+ 213 & E2SPAT(KS,KS,11AS,I2AS)- & E2SPAT(KS,I2AS,I1AS,KS) ENDIF IF (IiASPIN.EQ.I2ASPIN .AND. I2ASPIN.NE.KSPIN) & THEN H(II,JJ)=H(II,JJ)+ & E2SPAT(KS,KS,I1AS,I2AS) ENDIF ENDIF 2000 CONTINUE C H(II,JJ)=(H(II,JJ)*SIGNIA) C END 0 SUBROUTINE SLATER2(III,JJJ) This subroutine formulates the two-electron integral for a pair of determinants which differ in the locations of two electrons. 0000 IMPLICIT DOUBLE PRECISION (A-H,O-Z) 0 COMMON /BLOCK1/ H(10000,10000) COMMON /BLOCK2/ E1SPAT(100,100) COMMON /BLOCK3/ E2SPAT(100,100,100,100) COMMON /BLOCK4/ C3(10000,200) COMMON /BLOCK6/ NTOT2 COMMON /BLOCK12/ NC3 COMMON /BLOCK15/ NAO 0 INTEGER C3 Set the spin orbitals (in ascending order) which differ in occupation number in determinants I and J to I1,I2,I3 and I4. (Before beginning, set I1,I2,I3 and I4 to zero). WRITE(6,*) ’slater 2 1st check’ CALL FLUSH(6) 000000000 Il=0 I2=0 I3=0 I4=0 DO 150 KK=1,NTOT2,1 IF ((C3(III,KK)-C3(JJJ,KK)).EQ.1) & THEN IF (I1.EQ.0) THEN Il=KK GO TO 150 ENDIF IF (11.NE.0 .AND. I2.EQ.0) THEN I2=KK ENDIF ENDIF 214 0000000000 000 00000000 000 0000 150 CONTINUE DO 170 KK=1,NTOT2,1 IF ((C3(III,KK)-C3(JJJ,KK)).EQ.(-1)) & THEN IF (I3.EQ.0) THEN 13=KK GO TO 170 ENDIF IF (I4.EQ.0) THEN I4=KK ENDIF ENDIF 170 CONTINUE Determine the sign of the matrix element H(III,JJJ). First, count the number of occupied orbitals in determinant III that are lower in energy than the ist orbital in III which has a different occupation number than in JJJ, and set the total to SUMI1. (Before beginning, set SUMI1 to zero). SUM11=0.0D0 DO 450 MM=1,(I1-1),1 IF (C3(III,MM).EQ.1) THEN SUMI1=SUMI1+1.0D0 ENDIF 450 CONTINUE Then, multiply SUMI1 by -1, and set the result to SIGNIl. SIGNIl=((-1.0DO)**SUM11) Count the number of occupied orbitals in determinant III that are lower in energy than the 2nd orbital in III which has a different occupation number than in JJJ, and set the total to SUMI2. (Before beginning, set SUMI2 to zero). SUMI2=0.0D0 DO 451 MN=1,(I2-1),1 IF (C3(III,MN).EQ.1) THEN SUMI2=SUMI2+1.0D0 ENDIF 451 CONTINUE Multiply SUMI2 by -1, and set the result to SIGNI2. SIGNI2=((-1.0D0)**SUMI2) Count the number of occupied orbitals in determinant JJJ that are lower in energy than the 1st orbital in JJJ which has a different occupation number 215 0000 000 0 00000000 00 00000 0000000000 452 453 than in III, and set the total to SUMIB. (Before beginning, set SUMI3 to zero). SUMI3=0.0D0 DO 452 MO=1,(I3-1),1 IF (C3(JJJ,MO).EQ.1) THEN SUMI3=SUMI3+1.0d0 ENDIF CONTINUE Multiply SUMIB by -1, and set the result to SIGNI3. SIGN13=((-1.0D0)**SUM13) Count the number of occupied orbitals in determinant JJJ that are lower in energy than the 2nd orbital in JJJ which has a different occupation number than in III, and set the total to SUMI4. (Before beginning, set SUMI4 to zero). SUMI4=0.0D0 DO 453 MP=1,(I4-1),1 IF (C3(JJJ,MP).EQ.1) THEN SUMI4=SUMI4+1.0d0 ENDIF CONTINUE Multiply SUMI4 by -1, and set the result to SIGNI4. SIGNI4=((-1.0D0)**SUMI4) Calculate the overall sign of the two-electron integral(s) by multiplying the four signs together and setting the result to SIGNI. SIGNI=(SIGNI1*SIGNI2*SIGNI3*SIGNI4) Convert the spin orbitals Il,I2,I3 and I4 to spatial orbitals ISI,IS2,ISB and 184, respectively. Each unique pair of consecutive spin orbitals is assigned to the same spatial orbital. Set the spins of ISl,IS2,IS3 and 184. If the spin orbital is odd-numbered, set the spin of the spatial orbital to -1, and if the spin orbital is even, set the spin of the spatial orbital to +1. The variables for the spins of I81, 182, ISB and IS4 are IISPIN, I2SPIN, IBSPIN, and I4SPIN. IF (MOD(Il,2).EQ.0) THEN IS1=(11/2) IISPIN=-1 ELSE IF (MOD(Il,2).EQ.1) THEN IS1=((11+1)/2) IlSPIN=1 216 0000000000000 ELSE ENDIF ENDIF IF (MOD(I2,2).EQ.0) THEN IS2=(I2/2) I2SPIN=-1 ELSE IF (MOD(I2,2).EQ.1) THEN IS2=((I2+1)/2) I2SPIN=1 ELSE ENDIF ENDIF IF (MOD(13,2).EQ.0) THEN IS3=(I3/2) ISSPIN=-1 ELSE IF (MOD(13,2).EQ.1) THEN ISB=((13+1)/2) IBSPIN=1 ELSE ENDIF ENDIF IF (MOD(I4,2).EQ.0) THEN IS4=(I4/2) I4SPIN=-1 ELSE IF (MOD(I4,2).EQ.1) THEN IS4=((I4+1)/2) I4SPIN=1 ELSE ENDIF ENDIF WRITE(6,*) ’slater2, ok here’ CALL FLUSH(6) Determine the two-electron integral contribution to H(III,JJJ). First, determine whether the two-electron integrals formed by applying the Slater rules to determinants III and JJJ are spin-allowed. Add each spin-allowed two-electron integral to H(III,JJJ). IF (I1SPIN.EQ.IBSPIN .AND. &I2SPIN.EQ.I4SPIN .AND. ISSPIN.NE.I2SPIN) THEN H(III,JJJ)=H(III,JJJ)+E2SPAT(IS1,ISB,IS2,IS4) ENDIF IF (I1SPIN.EQ.I4SPIN .AND. 217 00000000000000000000000000000000 &I2SPIN.EO.13SPIN .AND. IiSPIN.NE.IBSPIN) THEN H(III,JJJ)=H(III,JJJ)- & E2SPAT(ISi,IS4,IS2,IS3) ENDIF IF (I1SPIN.EQ.I3SPIN .AND. &I2SPIN.EQ.I4SPIN .AND. IlSPIN.EQ.I4SPIN) THEN H(III,JJJ)=H(III,JJJ)+ & E2SPAT(IS1,ISB,IS2,IS4)- & E2SPAT(ISl,IS4,IS2,ISS) ENDIF Calculate the sign of H(III,JJJ). H(III,JJJ)=(H(III,JJJ)*SIGNI) END subroutine rsm(nm,n,a,w,m,z,fwork,iwork,ierr) integer n,nm,m,iwork(n),ierr integer k1,k2,k3,k4,k5,k6,k7 double precision a(nm,n),w(n),z(nm,m),fwork(1) this subroutine calls the recommended sequence of subroutines from the eigensystem subroutine package (eispack) to find all of the eigenvalues and some of the eigenvectors of a real symmetric matrix. on input nm must be set to the row dimension of the two-dimensional array parameters as declared in the calling program dimension statement. n is the order of the matrix a. a contains the real symmetric matrix. m the eigenvectors corresponding to the first m eigenvalues are to be computed. if m = 0 then no eigenvectors are computed. if m = n then all of the eigenvectors are computed. on output w contains all n eigenvalues in ascending order. 2 contains the orthonormal eigenvectors associated with the first m eigenvalues. ierr is an integer output variable set equal to an error completion code described in the documentation for tqlrat, imtqlv and tinvit. the normal completion code is zero. 218 00000000000 000 o n n n n o o 0 0 0 n o n o 10 50 X X fwork is a temporary storage array of dimension 8*n. iwork is an integer temporary storage array of dimension n. questions and comments should be directed to burton s. garbow, mathematics and computer science div, argonne national laboratory this version dated august 1983. ierr = 10 * n if (n .gt. nm .or. m .gt. nm) go to 50 k1 = 1 k2 = k1 + n k3 = k2 + n k4 = k3 + n k5 = k4 + n k6 = k5 + n k7 = k6 + n k8 = k7 + n if (m .gt. 0) go to 10 .......... find eigenvalues only .......... call tred1(nm,n,a,w,fwork(k1),fwork(k2)) call tqlrat(n,w,fwork(k2),ierr) go to 50 .......... find all eigenvalues and m eigenvectors .......... call tred1(nm,n,a,fwork(k1),fwork(k2),fwork(k3)) call imtqlv(n,fwork(kl),fwork(k2),fwork(k3),w,iwork, ierr,fwork(k4)) call tinvit(nm,n,fwork(k1),fwork(k2),fwork(k3),m,w,iwork,z,ierr, fwork(k4),fwork(k5),fwork(k6),fwork(k7),fwork(k8)) call trbak1(nm,n,a,fwork(k2),m,z) return end double precision function epslon (x) double precision x estimate unit roundoff in quantities of size x. double precision a,b,c,eps this program should function properly on all systems satisfying the following two assumptions, 1. the base used in representing floating point numbers is not a power of three. 2. the quantity a in statement 10 is represented to the accuracy used in floating point variables that are stored in memory. the statement number 10 and the go to 10 are intended to force optimizing compilers to generate code satisfying assumption 2. under these assumptions, it should be true that, a is not exactly equal to four-thirds, b has a zero for its last bit or digit, 219 00000000 000000000000000000000000000000000 10 c is not exactly equal to one, eps measures the separation of 1.0 from the next larger floating point number. the developers of eispack would appreciate being informed about any systems where these assumptions do not hold. this version dated 4/6/83. a = 4.0d0/3.0d0 b = a - 1.0d0 c = b + b + b eps = dabs(c-1.0d0) if (eps .eq. 0.0d0) go to 10 epslon = eps*dabs(x) return end subroutine imtqlv(n,d,e,e2,w,ind,ierr,rv1) integer i,j,k,1,m,n,ii,mml,tag,ierr double precision d(n),e(n),e2(n),w(n),rv1(n) double precision b,c,f,g,p,r,s,tst1,tst2,pythag integer ind(n) this subroutine is a variant of imtqll which is a translation of algol procedure imtqll, num. math. 12, 377-383(1968) by martin and wilkinson, as modified in num. math. 15, 450(1970) by dubrulle. handbook for auto. comp., vol.ii-linear algebra, 241-248(1971). this subroutine finds the eigenvalues of a symmetric tridiagonal matrix by the implicit ql method and associates with them their corresponding submatrix indices. on input n is the order of the matrix. d contains the diagonal elements of the input matrix. e contains the subdiagonal elements of the input matrix in its last n-1 positions. e(1) is arbitrary. e2 contains the squares of the corresponding elements of e. e2(1) is arbitrary. on output d and e are unaltered. elements of e2, corresponding to elements of e regarded as negligible, have been replaced by zero causing the matrix to split into a direct sum of submatrices. e2(1) is also set to zero. w contains the eigenvalues in ascending order. if an error exit is made, the eigenvalues are correct and 220 000000000000000000000000 100 105 110 120 125 130 ordered for indices 1,2,...ierr-1, but may not be the smallest eigenvalues. ind contains the submatrix indices associated with the corresponding eigenvalues in w -- 1 for eigenvalues belonging to the first submatrix from the top, 2 for those belonging to the second submatrix, etc.. ierr is set to zero for normal return, j if the j-th eigenvalue has not been determined after 30 iterations. rv1 is a temporary storage array. calls pythag for dsqrt(a*a + b*b) questions and comments should be directed to burton s. garbow, mathematics and computer science div, argonne national laboratory this version dated august 1983. ierr = 0 k = 0 tag = 0 do 100 i = 1, n w(i) = d(i) if (i .ne. 1) rv1(i-1) = e(i) continue e2(1) = 0.0d0 rv1(n) = 0.0d0 do 290 l = 1, n i=0 .......... look for small sub-diagonal element .......... do 110 m = l, n if (m .eq. n) go to 120 tst1 = dabs(w(m)) + dabs(w(m+1)) tst2 = tst1 + dabs(rv1(m)) if (tst2 .eq. tstl) go to 120 .......... guard against underflowed element of e2 .......... if (e2(m+1) .eq. 0.0d0) go to 125 continue if (m .le. k) go to 130 if (m .ne. n) e2(m+1) = 0.0d0 k = m tag = tag + 1 p = w(l) if (m .eq. 1) go to 215 if (j .eq. 30) go to 1000 221 J'=J'+1 .......... form shift .......... g = (w(l+1) - p) / (2.0d0 * rv1(1)) r = pythag(g,1.0d0) g = w(m) - p + rv1(l) / (g + dsign(r,g)) s = .0d0 c = .OdO = .OdO mml m - 1 .......... for i=m-1 step -1 until 1 do -- .......... do 200 ii = 1, mml ll OHH 1 = m - ii f = s * rv1(i) b = c * rv1(i) r = pythag(f,g) rv1(i+1) = r if (r .eq. 0.0d0) go to 210 s f / r g / r w(i+1) - p (w(i) - g) * s + 2.0d0 * c * b s * r ”+1) = g + p — c * r - b 200 continue H II II II II II A c 8 r P w 8 w(l) = w(l) - p rv1(l) rv1(m) go to 105 .......... recover from underflow .......... 210 w(i+1) = w(i+1) - p rv1(m) = 0.0d0 go to 105 .......... order eigenvalues .......... 215 if (1 .eq. 1) go to 250 .......... for i=1 step -1 until 2 do -- .......... do 230 ii = 2, 1 i = l + 2 - ii if (p .ge. w(i-1)) go to 270 8 0.0d0 w(i) = w(i-l) ind(i) = ind(i-l) 230 continue 250 i = 1 270 w(i) = p ind(i) = tag 290 continue go to 1001 .......... set error -- no convergence to an eigenvalue after 30 iterations .......... 1000 ierr = l 1001 return end 222 000000000000000000000000000000000000000 100 subroutine tqlrat(n,d,e2,ierr) integer i,j,l,m,n,ii,11,mm1,ierr double precision d(n),e2(n) double precision b,c,f,g,h,p,r,s,t,epslon,pythag this subroutine is a translation of the algol procedure tqlrat, algorithm 464, comm. acm 16, 689(1973) by rein sch. this subroutine finds the eigenvalues of a symmetric tridiagonal matrix by the rational ql method. on input n is the order of the matrix. d contains the diagonal elements of the input matrix. e2 contains the squares of the subdiagonal input matrix in its last n-1 positions. on output elements of the e2(1) is arbitrary. d contains the eigenvalues in ascending order. if an error exit is made, the eigenvalues are c orrect and ordered for indices 1,2,...ierr-1, but may not be the smallest eigenvalues. e2 has been destroyed. ierr is set to zero for normal return, j if the j-th eigenvalue has not determined after 30 iterations calls pythag for dsqrt(a*a + b*b) been questions and comments should be directed to burton s. garbow, mathematics and computer science div, argonne this version dated august 1983. national laboratory ierr = 0 if (n .eq. 1) go to 1001 do 100 i = 2, n e2(i-1) = e2(i) f = 0.0d0 t = 0.0d0 e2(n) = 0.0d0 do 290 l = 1, n 223 i=0 h = dabs(d(l)) + dsqrt(e2(l)) if (t .gt. h) go to 105 t = h b = epslon(t) c = b * b .......... look for small squared sub-diagonal element .......... 105 do 110 m = 1, n if (e2(m) .1e. c) go to 120 .......... e2(n) is always zero, so there is no exit through the bottom of the loop .......... 110 continue 120 if (m .eq. 1) go to 210 130 if (j .eq. 30) go to 1000 J=j+1 .......... form shift . ...... . 11 = l + 1 s = dsqrt(e2(l)) g = d(l) p = (d(ll) - g) / (2.0d0 * s) r = pythag(p,1.0d0) d(l) = s / (p + dsign(r,p)) h g - d(l) do 140 i = 11, n 140 d(i) = d(i) - h f = f + h .......... rational ql transformation .......... g = d(m) if (g .eq. 0.0d0) g = b h = g s = 0.0d0 mml = m - 1 .......... for i=m-1 step -1 until 1 do -- .......... do 200 ii = 1, mml 1 = m - ii p=s*h r = p + e2(i) e2(i+1) = s * r s = e2(i) / r d(i+1) = h + s * (h + d(i)) g = d(i) - e2(i) / 3 if (g .eq. 0.0d0) g = b h=g*p/r 200 continue e2(1) = s * g d(l) = h .......... guard against underflow in convergence test .......... if (h .eq. 0.0d0) go to 210 if (dabs(e2(l)) .le. dabs(c/h)) go to 210 e2(1) = h * e2(1) if (e2(1) .ne. 0.0d0) go to 130 224 000000 210 230 250 270 290 1000 1001 10 20 p = d(l) + f .......... order eigenvalues .......... if (1 .eq. 1) go to 250 .......... for i=1 step -1 until 2 do -- .......... do 230 ii = 2, l i = l + 2 - ii if (p .ge. d(i-1)) go to 270 d(i) = d(i—1) continue i = 1 d(i) = p continue go to 1001 .......... set error -- no convergence to an eigenvalue after 30 iterations .......... ierr = 1 return end double precision function pythag(a,b) double precision a,b finds dsqrt(a**2+b**2) without overflow or destructive underflow double precision p,r,s,t,u p = dmax1(dabs(a),dabs(b)) if (p .eq. 0.0d0) go to 20 r = (dmin1(dabs(a),dabs(b))/p)**2 continue t = 4.0d0 + r if (t .eq. 4.0d0) go to 20 s = r/t u = 1.0d0 + 2.0d0*s P = u*P r = (s/u)**2 * r go to 10 pythag = 9 return end subroutine tinvit(nm,n,d,e,e2,m,w,ind,z, x ierr,rv1,rv2,rv3,rv4,rv6) integer i,j,m,n,p,q,r,s,ii,ip,jj,nm,its,tag,ierr,group double precision d(n),e(n),e2(n),w(m),z(nm,m), x rv1(n),rv2(n),rv3(n),rv4(n),rv6(n) double precision u,v,uk,xu,x0,x1,eps2,ep33,eps4,norm,order,epslon, x pythag integer ind(m) this subroutine is a translation of the inverse iteration tech- nique in the algol procedure tristurm by peters and wilkinson. handbook for auto. comp., vol.ii-linear algebra, 418-439(1971). this subroutine finds those eigenvectors of a tridiagonal 225 0000000000000000000000000000000000000000000000000000000 symmetric matrix corresponding to specified eigenvalues, using inverse iteration. on input on nm must be set to the row dimension of two-dimensional array parameters as declared in the calling program dimension statement. is the order of the matrix. contains the diagonal elements of the input matrix. contains the subdiagonal elements of the input matrix in its last n-1 positions. e(1) is arbitrary. e2 contains the squares of the corresponding elements of e, m V with zeros corresponding to negligible elements of e. e(i) is considered negligible if it is not larger than the product of the relative machine precision and the sum of the magnitudes of d(i) and d(i-1). e2(1) must contain 0.0d0 if the eigenvalues are in ascending order, or 2.0d0 if the eigenvalues are in descending order. if bisect, tridib, or imtqlv has been used to find the eigenvalues, their output e2 array is exactly what is expected here. is the number of specified eigenvalues. contains the m eigenvalues in ascending or descending order. ind contains in its first m positions the submatrix indices associated with the corresponding eigenvalues in w -- 1 for eigenvalues belonging to the first submatrix from the top, 2 for those belonging to the second submatrix, etc. output all input arrays are unaltered. 2 contains the associated set of orthonormal eigenvectors. any vector which fails to converge is set to zero. ierr is set to zero for normal return, -r if the eigenvector corresponding to the r-th eigenvalue fails to converge in 5 iterations. rv1, rv2, rv3, rv4, and rv6 are temporary storage arrays. calls pythag for dsqrt(a*a + b*b) questions and comments should be directed to burton s. garbow, mathematics and computer science div, argonne national laboratory this version dated august 1983. 226 0 0000 ierr = 0 if (m .eq. 0) go to 1001 Mg 0 order = 1.0d0 - e2(1) q=0 .......... establish and process next submatrix .......... 100 p = q + 1 do 120 q = p, n if (q .eq. n) go to 140 if (e2(q+1) .eq. 0.0d0) go to 140 120 continue .......... find vectors by inverse iteration .......... 140t 3g = tag + 1 = 0 do 920 r = 1, m if (ind(r) .ne. tag) go to 920 its = 1 x1 = w(r) if (s .ne. 0) go to 510 .......... check for isolated root .......... xu = 1.0d0 if (p .ne. q) go to 490 rv6(p) = 1.0d0 go to 870 490 norm = dabs(d(p)) i=p p+1 do 500 i = ip, q 500 norm = dmax1(norm, dabs(d(i))+dabs(e(i))) .......... eps2 is the criterion for grouping, eps3 replaces zero pivots and equal roots are modified by eps3, eps4 is taken very small to avoid overflow .......... eps2 = 1.0d-3 * norm epsB = epslon(norm) uk=q-p+1 eps4 = uk * epsS uk = eps4 / dsqrt(uk) s = p 505 group = 0 go to 520 .......... look for close or coincident roots .......... 510 if (dabs(xl-xO) .ge. eps2) go to 505 group = group + 1 if (order * (x1 - x0) .1e. 0.0d0) x1 = x0 + order * epsB .......... elimination with interchanges and initialization of vector .......... 520 = 0.0d0 do 580 i = p, q 227 rv6(i) = uk if (1 .eq. p) go to 560 if (dabs(e(i)) .lt. dabs(u)) go to 540 .......... warning -- a divide check may occur here if e2 array has not been specified correctly .......... xu = u / e(i) rv4(i) = xu rv1(i-1) = e(i) rv2(i-1) = d(i) - x1 rv3(i-1) = 0.0d0 if (i .ne. q) rv3(i-1) = e(i+1) u = v - xu * rv2(i-1) v = -xu * rv3(i-1) go to 580 540 xu = e(i) / u rv4(i) = xu rv1(i-1) u rv2(i-1) v rv3(i-1) 0.0d0 560 u = d(i) x1 - xu * v if (i .ne. q) v = e(i+1) 580 continue if (u .eq. 0.0d0) u = epsS rv1(q) = u rv2(q) = 0.0d0 rv3(q) = 0.0d0 .......... back substitution for i=q step -1 until p do -- .......... 600 do 620 ii = p, q i = p + q - ii rv6(i) = (rv6(i) - u * rv2(i) - v * rv3(i)) / rv1(i) v = u u = rv6(i) 620 continue .......... orthogonalize with respect to previous members of group .......... if (group .eq. 0) go to 700 J - r do 680 jj = 1, group 630 j = ' - 1 if (ind(j) .ne. tag) go to 630 xu = 0.0d0 do 640 i = p, q 640 xu = xu + rv6(i) * z(i,j) do 660 i = p, 660 rv6(i) = rv6(i) - xu * z(i,j) 680 continue 700 norm = 0.0d0 228 do 720 i = p, q 720 norm = norm + dabs(rv6(i)) if (norm .ge. 1.0d0) go to 840 .......... forward substitution .......... if (its .eq. 5) go to 830 if (norm .ne. 0.0d0) go to 740 rv6(s) = eps4 s = s + 1 if (s .gt. q) s = p go to 780 740 xu = eps4 / norm do 760 i = p, q 760 rv6(i) = rv6(i) * xu .......... elimination operations on next vector iterate .......... 780 do 820 i = ip, q u = rv6(i) .......... if rv1(i-1) .eq. e(i), a row interchange was performed earlier in the triangularization process .......... if (rv1(i-1) .ne. e(i)) go to 800 u = rv6(i-1) rv6(i-1) = rv6(i) 800 rv6(i) = u - rv4(i) * rv6(i-1) 820 continue its = its + 1 go to 600 .......... set error -- non~converged eigenvector .......... 830 ierr = -r xu = 0.0d0 go to 870 .......... normalize so that sum of squares is 1 and expand to full order .......... 840 u = 0.0d0 do 860 i = p, q 860 u = pythag(u,rv6(i)) xu = 1.0d0 / u 870 do 880 i = 1, n 880 z(i,r) = 0.0d0 do 900 i - p, 900 z(i,r) = rv6(i) * xu x0 = x1 920 continue if (q .lt. n) go to 100 1001 return end 229 00000000000000000000000000000000000000 110 subroutine trbak1(nm,n,a,e,m,z) integer i,j,k,l,m,n,nm double precision a(nm,n),e(n),z(nm,m) double precision 3 this subroutine is a translation of the algol procedure trbak1, num. math. 11, 181-195(1968) by martin, reinsch, and wilkinson. handbook for auto. comp., vol.ii-linear algebra, 212-226(1971). this subroutine forms the eigenvectors of a real symmetric matrix by back transforming those of the corresponding symmetric tridiagonal matrix determined by tredl. on input nm must be set to the row dimension of two-dimensional array parameters as declared in the calling program dimension statement. n is the order of the matrix. a contains information about the orthogonal trans- formations used in the reduction by tred1 in its strict lower triangle. e contains the subdiagonal elements of the tridiagonal matrix in its last n-1 positions. e(1) is arbitrary. m is the number of eigenvectors to be back transformed. 2 contains the eigenvectors to be back transformed in its first m columns. note that trbak1 preserves vector euclidean norms. questions and comments should be directed to burton s. garbow, mathematics and computer science div, argonne national laboratory this version dated august 1983. if (m .eq. 0) go to 200 if (n .eq. 1) go to 200 do 140 i = 2, n l = i - 1 if (e(i) .eq. 0.0d0) go to 140 do 130 j = 1, m s = 0.0d0 do 110 k = 1, l s = s + a(i,k) * z(k,j) 230 0000000000000000000000000000000000000 120 130 140 200 .......... divisor below is negative of h formed in tredl. double division avoids possible underflow .......... s = (s / a(i,1)) / e(i) do 120 k = 1, 1 z(k,j) = z(k,j) + s * a(i,k) continue continue return end subroutine tred1(nm,n,a,d,e,e2) integer i,j,k,l,n,ii,nm,jp1 double precision a(nm,n),d(n),e(n),e2(n) double precision f,g,h,scale this subroutine is a translation of the algol procedure tred1, num. math. 11, 181-195(1968) by martin, reinsch, and wilkinson. handbook for auto. comp., vol.ii-linear algebra, 212-226(1971). this subroutine reduces a real symmetric matrix to a symmetric tridiagonal matrix using orthogonal similarity transformations. on input nm must be set to the row dimension of two-dimensional array parameters as declared in the calling program dimension statement. n is the order of the matrix. a contains the real symmetric input matrix. only the lower triangle of the matrix need be supplied. on output a contains information about the orthogonal trans- formations used in the reduction in its strict lower triangle. the full upper triangle of a is unaltered. d contains the diagonal elements of the tridiagonal matrix. e contains the subdiagonal elements of the tridiagonal matrix in its last n-1 positions. e(1) is set to zero. e2 contains the squares of the corresponding elements of e. e2 may coincide with e if the squares are not needed. questions and comments should be directed to burton s. garbow, mathematics and computer science div, argonne national laboratory 231 0000 100 120 125 130 140 150 170 this version dated august 1983. do 100 i = 1, n d(i) = a(n,i) a(n,i) = a(i.i) continue .......... for i=n step -1 until 1 do -- do 300 ii = 1, n 1 = n + 1 - ii 1 = i - 1 h = 0.0d0 scale = 0.0d0 if (1 .lt. 1) go to 130 .......... scale row (algol tol then not needed) .......... do 120 k = 1, 1 scale = scale + dabs(d(k)) if (scale .ne. 0.0d0) go to 140 continue e(i) = 0.0d0 e2(i) = 0.0d0 go to 300 do 150 k = 1, 1 d(k) = d(k) / scale h = h + d(k) * d(k) continue e2(i) = scale * scale * h f = d(l) g = -dsign(dsqrt(h),f) e(i) = scale * g h = h - f * g d(l) = f - g if (1 .eq. 1) go to 285 .......... form a*u .......... (j) (j) + a(j,j) * f j 1 k = jpl, l g + a(k,j) * d(k) 232 0 0000000000000 200 220 240 245 250 260 280 285 290 300 e(k) = e(k) + a(k,j) * f continue e(j) = continue .......... form p .......... f = 0.0d0 do 245 j = 1, l e(j) = e(j) / h f = f + e(j) * d(j) continue = f / (h + h) .......... form q .......... do 250 j = 1, 1 e(j) = e(j) - h * d(j) .......... form reduced a .......... do 280 j = 1,1 f = d(j) g = e(j) do 260 k = J, l a(k,j) = a(k.j) - f * e(k) - g * d(k) continue do 290 j = 1, l ”d( ) d(j) = Ja(l,j) a(l, j) = a(i,j) a(i, j) = f * scale continue continue return end SUBROUTINE AOROUT(XELEC,YELEC,ZELEC,AO) This subroutine uses the input for a GAMESS CISD energy cal- culation to compute the values of all atomic orbitals for a particular atom. Specifically, each atomic orbital is computed at a set of x, y, 2 electronic coordinates shifted by the X, Y, and Z coordinates of the atomic nucleus on which the atomic orbital is centered. Also, each atomic orbital is constructed from a linear combination of primitive gaussians, as specified by the GAMESS input. Declare that all variables with names that begin with letters A-H or 0-2 will be double-precision numbers. IMPLICIT DOUBLE PRECISION (A-H, O-Z) 233 0000000000000000000000000000000000000000000000000000000 Description of all variables and/or arrays used in the sub- routine: XATOM = x-coordinate of nucleus of atom YATOM = y-coordinate of nucleus of atom ZATOM = z-coordinate of nucleus of atom XELEC = x electronic coordinate YELEC = y electronic coordinate ZELEC = 2 electronic coordinate XDIFF = difference between x electronic coord. and x-coord. of nucleus of atom YDIFF = difference between y electronic coord. and y-coord. of nucleus of atom ZDIFF = difference between 2 electronic coord. and z-coord. of nucleus of atom. XDSQRD = square of difference between x electronic coord. and x-coord. of nucleus of atom YDSQRD = square of difference between y electronic coord. and y-coord. of nucleus of atom ZDSQRD = square of difference between 2 electronic coord. and z-coord. of nucleus of atom R = Sum of XDSQRD,YDSQRD,ZDSQRD. SNUMPG, PNUMPG, DNUMPG = Integer variables set to the number of primitive gaussians in an S, P or D atomic orbital (respectively). SPGAUSS = 100 x 100 dimension array containing the exponents and coefficients for the primitive gaussians used in a S-type atomic orbital. PPGAUSS = 100 x 100 dimension array containing the exponents and coefficients for the primitive gaussians used in a P-type atomic orbital. DPGAUSS = 100 x 100 dimension array containing the exponents and coefficients for the primitive gaussians used in a D-type atomic orbital. SCHIMU = numerical value of a S-type atomic orbital computed at x-Z, y-Y, z-Z PXCHIMU, PYCHIMU, PZCHIMU = numerical values of Px-type, Py-type, and Pz-type atomic orbitals computed the x-Z, y-Y, z-Z DXY, DXZ, DYZ, DXSQRD, DYSQRD, DZSQRD = numerical values of ny-type, sz-type, Dyz-type, stquared-type, Dysquared-type and Dzsquared-type atomic orbitals computed at the x-X,y-Y,z-Z PI = double-precision numerical constant for pi INPUT1 = Character variables used to read the lines in the GAMESS input file. 234 0000000000000000000000000000000000000000 SORBTOT, PORBTOT, DORBTOT = Total number of S, P and D basis functions (3 x PORBTOT = total number of P orbitals, 6 x DORBTOT = total number of D orbitals). PXORBTOT, PYORBTOT, PZORBTOT, DXYTOT, DXZTOT, DYZTOT, DX2TOT, DY2TOT, DZ2TOT = variables representing the total number of Px, Py, Pz, ny, sz, Dyz, stquared, Dysquared, Dzsquared orbitals, respectively. ATOM = character variable used to read the name of the atom on which the molecular orbital is centered. NUMELEC = Integer variable used to read the number of electrons in the atom on which the molecular orbital is centered. AORBTOT = Integer variable representing the total number of atomic orbitals for an atom. A0 = One-dimensional array which holds the values of all atomic orbitals at x-X, y-Y, z-Z. ATOMTOT = The total number of atoms in the molecule of interest. SORB = Two-letter character variable used to read the letter S denoting a S-type basis function from the GAMESS input file. PORB = Two-letter character variable used to read the letter P denoting a P-type basis function from the GAMESS input file. DORB = Two-letter character variable used to read the letter D denoting a D-type basis function from the GAMESS input file. NUMATOM = One-dimensional array used to keep track of the number of atomic orbitals for each atom. For example the element corresponding to NUMATOM(1) is the number of atomic orbitals for the first atom (as listed in the GAMESS input file) in the molecule of interest. NCOUNT = Integer variable used to keep track of the total number of atomic orbitals for each atom. DIMENSION SPGAUSS(100, 100), PPGAUSS(100, 100), DPGAUSS(100,100) INTEGER SORBTOT, PORBTOT, DORBTOT, PXORBTOT, PYORBTOT, PZORBTOT INTEGER DXYTOT, DX2TOT, DY2TOT, DX2TOT, DY2TOT, DZ2TOT, AORBTOT CHARACTER INPUT*80, INPUT1*80, ATOM*15 REAL NUMELEC INTEGER SNUMPG, PNUMPG, DNUMPG, ATOMTOT CHARACTER SORB*2, PORB*2, DORB*2 DIMENSION NUMATOM(100) DIMENSION AO(100) COMMON /BLOCK15/ NAO Set the value of the constant pi (PI). PI = DACOS(-1.D0) 235 00 0000 00 100 2222 00000000000 0000 00000 0000 0 Set the total number of atoms equal to zero. ATOMTOT = 0 Set the total number of atomic orbitals for this atom equal to zero. AORBTOT = 0 Open the input file for a GAMESS CISD energy calculation. OPEN (UNIT=24, &FILE=’mod_h2cisd_MBS_C1.inp’, &STATUS= ’ OLD ’ , FORM= ’ FORMATTED ’ ) FORMAT (A80) Go back two lines in the input file. BACKSPACE(24) BACKSPACE(24) Read the current line in the input file into INPUT (actually, the first 80 characters of this line). READ(24,100)INPUT If the first five characters in the current line are not " $con", then go to line 2222 in the program. Note: " $con" belongs to the " $control" line in the input file. Since " $control" is always the first group in GAMESS input files, reading " $con" indicates that we are at the beginning of the file. Returning to line 2222 will allow us to keep reading until we reach the beginning of the input file. IF (INPUT(1:5).NE.’ $Con’) THEN GO TO 2222 ENDIF If we have read " $con", then go back one line in the file (then, once again, we are at the beginning of the file). BACKSPACE(24) Read the next two lines in the input file, one by one, into INPUT. READ(24,100)INPUT READ(24,100)INPUT If the first five characters of the current line are not equal to " $dat" or " $DAT" (indicating 236 that we have reached the " $data"/" $DATA" group in the GAMESS input file), the read the next line in the input file into INPUT. Keep reading until the first five characters ARE " $data" or " $DATA". 00000 101 IF (INPUT(1:5).NE.’ $dat’ .AND. &INPUT(1:5).NE.’ $DAT’) THEN READ(24,100)INPUT GO TO 101 ELSE ENDIF Once we read the " $data"/" $DATA" group, read the next three lines, one after another, into INPUT. 0000 102 FORMAT (A80) IF (INPUT(1:5).EQ.’ $dat’ .OR. INPUT(1:5).EQ.’ $DAT’) &THEN READ(24,102)INPUT READ(24,102)INPUT READ(24,102)INPUT ELSE END IF c Set NCOUNT equal to zero. NCOUNT=0 c Read the next line in the input file into INPUT. 777 READ(24,102)INPUT If the first five characters in the current line are blank spaces, then read the next line into INPUT. Continue reading until a line is read which DOES NOT have blank spaces for its first five characters. 000000 DO 1999 WHILE (INPUT(1:5).EQ.’ ’) READ(24,102)INPUT 1999 CONTINUE c c If the current line’s first five characters are c " Send", indicating that we have reached the end of c the data group in the GAMESS input file, then go to c line 5000. c IF (INPUT(1:5).EQ.’ $end’) THEN GO TO 5000 ELSE END IF 0 Go back to the previous line. BACKSPACE(24) 237 0 00 0000 00000 00000 00000 0000 0 103 Read the name of the atom, the number of electrons in the atom, and the x, y, and z coordinates of the atom’s nucleus. FORMAT (A15, F2.0, D20.10, D20.10, D20.10) READ(24,103)ATOM, NUMELEC, XATOM, YATOM, ZATOM Increment the total number of atoms. ATOMTOT=ATOMTOT+1 Set the total number of s, p, d, px, py, pz, dxy, dxz, dyz, dx2, dy2 and dz2 atomic orbitals equal to zero. 0 0 0 SORBTOT PORBTOT DORBTOT PXORBTOT PYORBTOT 0 0 0 U N M H O F] II II II II II II OOOOOOII II II DZ2TOT Calculate the difference between the x, y, and 2 electronic coordinates and the x, y, and z coordinates of the atom’s nucleus. XDIFF = XELEC - XATOM YDIFF = YELEC - YATOM ZDIFF = ZELEC - ZATOM Square the differences between the x, y, and 2 electronic coordinates and the x, y, and z coordinates of the atom’s nucleus. XDSQRD = XDIFF**2 YDSQRD = YDIFF**2 ZDSQRD = ZDIFF**2 Add the squares of the differences between the x, y, and 2 electronic coordinates and the x, y, and z coordinates of the atom’s nucleus. R = XDSQRD + YDSQRD + ZDSQRD Set the INPUT1 character variable equal to the INPUT variable. INPUT1 = INPUT 9988 FORMAT (A5) 104 FORMAT (A80) 238 0000000000000 0000000 000000 000000 00000 200 201 105 If the first five Characters of INPUT1 are NOT all blanks, read the next line in the input file into INPUT1. If the first five characters of INPUT1 are " S ", then go to line 201. If the first five characters of INPUT1 are " P ", then go to line 202. If the first five Characters of INPUT1 are " D ", then go to line 203. Note: " S " indicates that we are about to read data for an s-type orbital, " P " indicates that we are about to read data for a p-type atomic orbital, and " D " indicates that we are about to read the data for a d-type atomic orbital. DO 200 WHILE (INPUT1(1:5).NE.’ ’) READ(24,104)INPUT1 IF (INPUT1(1:5).EQ.’ S ’) THEN GO TO 201 ELSE IF (INPUT1(1:5).EQ.’ P ’) THEN GO TO 202 ELSE IF (INPUT1(1:5).EQ.’ D ’) THEN GO TO 203 ELSE ENDIF CONTINUE If the first five characters of INPUT1 are blanks, then go to line 4999. Note: If the first five Characters of INPUT1 are blanks, this indicates that we have reached the end of the "$data" group in the GAMESS input file. IF (INPUT1(1:5).EQ.’ ’) THEN GO TO 4999 ELSE END IF This is line 201, which is the line to go to if a " S " was read into INPUT in the 200 DO loop. Go back to the previous line. BACKSPACE(24) Read the "S" indicating data for an s-type orbital and the number following the S (which is the number of primitive gaussians in the s-type orbital) into the SORB character variable and the SNUMPG integer variable, respectively. FORMAT (A2, I4) READ(24,105)SORB, SNUMPG Read the number of the primitive gaussian, the exponent for the gaussian, and the coefficient for the gaussian into the SPGAUSS array. Do this for all primitive gaussians in the s-type atomic 239 00 00 00000 0000 0 000 000000 0000000 106 300 202 & orbital. READ(24,*) ((SPGAUSS(ISROW,ISCOL), ISCOL=1,3), ISROW=1,SNUMPG) Use the primitive gaussians to calculate the value of the s-type atomic orbital at R, and read the value of the atomic orbital into SCHIMU. DO 106 I = 1, SNUMPG, 1 SCHIMU = SCHIMU + DEXP(-1.0D0*((SPGAUSS(I,2))*R))* (((2.0DO*(SPGAUSS(I,2)))/PI)**0.75D0)*(SPGAUSS(I,3)) CONTINUE Increment the total number of atomic orbitals. NCOUNT=NCOUNT+1 Read the value of the s-type atomic orbital into the AO array. AO(NCOUNT)=SCHIMU Increment the total number of s-type orbitals. SORBTOT = SORBTOT + 1 Clear the SCHIMU variable. SCHIMU=0 Clear the SPGAUSS array. DO 300 ISROW = 1, SNUMPG, 1 SPGAUSS(ISROW,1) = 0 SPGAUSS(ISROW,2) = 0 SPGAUSS(ISROW,3) = 0 CONTINUE Go back to line 200. GO TO 200 This is line 202, which is the line to go to if a " P " was read into INPUT in the 200 D0 loop. Go back to the previous line. BACKSPACE(24) Read the "P" indicating data for an p-type orbital and the number following the P (which is the number of primitive gaussians in the p-type orbital) into the PORB character variable and the PNUMPG integer variable, respectively. 240 0000000 000000 000 0000 000 0000 00 107 & fifi’fi’ WWW & & & 108 FORMAT (A2, I4) READ(24,107)PORB, PNUMPG Read the number of the primitive gaussian, the exponent for the gaussian, and the coefficient for the gaussian into the PPGAUSS array. Do this for all primitive gaussians in the p-type atomic orbital. READ(24,*) ((PPGAUSS(IPROW,IPCOL),IPCOL=1,3), IPROW=1,PNUMPG) Use the primitive gaussians to calculate the value of the px-type, py-type, and pz-type atomic orbitals at R, and read the values of these atomic orbitals into PXCHIMU, PYCHIMU, and PZCHIMU. DO 108 J = 1, PNUMPG, 1 PXCHIMU = PXCHIMU + DEXP(-1.0D0*((PPGAUSS(J,2))* R))*XDIFF*(PPGAUSS(J,3))* (((2.0D0**1.75D0)* ((PPGAUSS(J,2))**1.25D0))/(PI**.75D0)) PYCHIMU = PYCHIMU + DEXP(-1.0D0*((PPGAUSS(J,2))* R))*YDIFF*(PPGAUSS(J,3))* (((2.0D0**1.75D0)* ((PPGAUSS(J,2))**1.25D0))/(PI**.75D0)) PZCHIMU = PZCHIMU + DEXP(-1.0D0*((PPGAUSS(J,2))* R))*ZDIFF*(PPGAUSS(J,3))* (((2.0D0**1.75D0)* ((PPGAUSS(J,2))**1.25D0))/(PI**.75D0)) CONTINUE Increment the total number of atomic orbitals. NCOUNT=NCOUNT+1 Read the value of the px-type atomic orbital into the AO array. AO(NCOUNT)=PXCHIMU Increment the total number of atomic orbitals. NCOUNT=NCOUNT+1 Read the value of the py-type atomic orbital into the AO array. AO(NCOUNT)=PYCHIMU Increment the total number of atomic orbitals. NCOUNT=NCOUNT+1 241 0000 000 0 0000 0 000000 000 0000000 00000 325 203 109 Read the value of the pz-type atomic orbital into the AO array. AO(NCOUNT)=PZCHIMU Increment the total number of p-type atomic orbitals. PORBTOT = PORBTOT + 1 Increment the total number of px-type, py-type, and pz-type atomic orbitals. PXORBTOT = PXORBTOT + 1 PYORBTOT = PYORBTOT + 1 PZORBTOT = PZORBTOT + 1 Clear the PXCHIMU, PYCHIMU, and PZCHIMU variables. PXCHIMU = 0 PYCHIMU = 0 PZCHIMU = 0 Clear the PPGAUSS array. DO 325 IPROW = 1, PNUMPG, 1 PPGAUSS(IPROW,1) = 0 PPGAUSS(IPROW,2) = 0 PPGAUSS(IPROW,3) = 0 CONTINUE Return to the 200 D0 loop. GO TO 200 This is line 203, which is the line to go to if a " D " was read into INPUT in the 200 DO loop. Go back to the previous line. BACKSPACE(24) Read the "D" indicating data for an d-type orbital and the number following the D (which is the number of primitive gaussians in the d-type orbital) into the DORB character variable and the DNUMPG integer variable, respectively. FORMAT (A2, I4) READ(24,109)DORB, DNUMPG Read the number of the primitive gaussian, the exponent for the gaussian, and the coefficient for the gaussian into the DPGAUSS array. Do this for all primitive gaussians in the d-type atomic 242 00 0000000 orbital . READ(24,*)((DPGAUSS(IDROW,IDCOL), &IDCOL=1,3), IDROW=1,DNUMPG) RPfi'fi’ RPWRP ”w” ”a“? P”? & & & Use the primitive gaussians to calculate the value of the dxy-type, dxz-type, dy2-type, dx2, dy2, and dz2 atomic orbitals at R, and read the values of these atomic orbitals into PXCHIMU, PYCHIMU, and PZCHIMU. DO 110 K = 1, DNUMPG, 1 DXY = DXY + DEXP(-1.0D0*((DPGAUSS(K,2))*R))* XDIFF*YDIFF*(DPGAUSS(K,3))* (((2.0D0**2.75D0)* ((DPGAUSS(K,2))**1.75D0))/(PI**.75D0)) DXZ = DXZ + DEXP(-1.0D0*((DPGAUSS(K,2))*R))* XDIFF*ZDIFF*(DPGAUSS(K,3))* (((2.0DO**2.75D0)* ((DPGAUSS(K,2))**1.75D0))/(PI**.75D0)) DYZ = DYZ + DEXP(-1.0D0*((DPGAUSS(K,2))*R))* YDIFF*ZDIFF*(DPGAUSS(K,3))* (((2.0D0**2.75DO)* ((DPGAUSS(K,2))**1.75DO))/(PI**.75D0)) DXSQRD = DXSQRD + DEXP(-1.0D0*((DPGAUSS(K,2)) *R))*XDIFF*XDIFF*(DPGAUSS(K,3))* (((2.0D0**2.75D0)* ((DPGAUSS(K,2))**1.75D0))/((3.0D0**0.5D0)*(PI**.75D0))) DYSQRD = DYSQRD + DEXP(-1.0D0*((DPGAUSS(K,2)) *R))*YDIFF*YDIFF*(DPGAUSS(K,3))* (((2.0DO**2.75D0)* ((DPGAUSS(K,2))**1.75D0))/((3.0D0**0.5D0)*(PI**.75DO))) DZSQRD = DZSQRD + DEXP(-1.0D0*((DPGAUSS(K,2)) *R))*ZDIFF*ZDIFF*(DPGAUSS(K,3))* (((2.0D0**2.75D0)* ((DPGAUSS(K,2))**1.75D0))/((3.0D0**0.5D0)*(PI**.75D0))) 110 CONTINUE Increment the total number of atomic orbitals. NCOUNT=NCOUNT+1 Read the value of the dx2-atomic orbital into the AO array. AO(NCOUNT)=DXSQRD Increment the total number of atomic orbitals. NCOUNT=NCOUNT+1 243 Read the value of the dy2-atomic orbital into the AO array. AO(NCOUNT)=DYSQRD Increment the total number of atomic orbitals. NCOUNT=NCOUNT+1 Read the value of the dz2-atomic orbital into the AO array. AO(NCOUNT)=DZSQRD Increment the total number of atomic orbitals. NCOUNT=NCOUNT+1 Read the value of the dxy-atomic orbital into the AO array. AO(NCOUNT)=DXY Increment the total number of atomic orbitals. NCOUNT=NCOUNT+1 Read the value of the dxz-atomic orbital into the AO array. AO(NCOUNT)=DXZ Increment the total number of d-type atomic orbitals. DORBTOT = DORBTOT + 1 Increment the total number of dxy-type atomic orbitals. DXYTOT = DXYTOT + 1 Increment the total number of dxz—type atomic orbitals. DX2TOT = DXZTOT + 1 Increment the total number of dy2-type atomic orbitals. DYZTOT = DYZTOT + 1 Increment the total number of dx2-type atomic orbitals. DX2TOT = DX2TOT + 1 Increment the total number of dy2-type atomic orbitals. DY2TOT = DY2TOT + 1 Increment the total number of dz2-type atomic orbitals. DZ2TOT = DZ2TOT + 1 244 0000 375 00000000 00000 4999 0000 00 00 5000 0000 0 Clear the dxy-type, dxz-type, dy2-type, dx2-type, dy2-type and dz2-type atomic orbitals. DXY 0 DXZ DYZ DXSQRD DYSQRD DZSQRD 0 0 0 O 0 Clear the DPGAUSS array. DO 375 IDROW = 1, DNUMPG, 1 DPGAUSS(IDROW,1) = 0 DPGAUSS(IDROW,2) = 0 DPGAUSS(IDROW,3) = 0 CONTINUE At this point, we have finished reading the information for the d-type atomic orbitals and evaluating these orbitals at R. We are ready to read the information for the next atomic orbital, or (if all of the orbital information has already been read) return the evaluated atomic orbitals to the main program. Return to line 200, where we will decide what to do next. GO TO 200 We are done reading the information for all atomic orbitals of the atom and evaluating these orbitals at R. Now, we compute the total number of atomic orbitals for the atom. AORBTOT = SORBTOT + PXORBTOT + PYORBTOT + PZORBTOT + DXYTOT + DX2TOT + DYZTOT + DX2TOT + DY2TOT + DZ2TOT Read the total number of atomic orbitals for the current atom into NUMATOM(ATOMTOT). NUMATOM(ATOMTOT)=AORBTOT Return to line 777. GO TO 777 Close the GAMESS CISD input file. CLOSE(20) Return the values of the atomic orbitals (evaluated at R) to the main program, and return to the main program. RETURN END 245 Appendix B. Tables 246 Appendix B. Tables Table 1. Non-zero terms in the third-order interaction energy of molecules A and B, 0Classified by order m) the permanent dipoles of A and B. Note that we have let =|0A) and 111313—403). Term ,1“ order 1130 Name —(0,,03|VABGAH%T 0,3,1, BGBVABIOAOB) 1 1 1 — (1,1) —(OAOB|VABGAfi:‘ TWO), GAQ’BVABlOAOB) 0 1 2 — (0,1) ‘(0AOBIVABGAMQ TaaflfaoGAVABIOAOB) 0 3 3 - (013) -,1O(OAOB|VABGA :OT 3,18 BGAG’BVABIOAOB) 1 1 4— (1,1) —(0,10,)VA’-"G’3fif,1 T0111, BGAVABIOAOB) 1 1 5 — (1,1) —(oAOB|VABGBfif T11, BGAABVABmAOB) 1 0 6—(1,0) —(0A03|VABGBfiaTawgoaAABVAB|0103) 1 1 7 — (1,1) —<0101IVABGB112°T.1F§ CAI/“10103) 3 0 8 — (3, 0) —(0 ,0,;|VAA‘GAéABfifi‘Tafifi;g GAVAB|0 103) 0 1 (0, 1) —(01%|VABGAABEZTGBEEGBVAB|0103) 1 0 10 — (1, 0) —(OAOB|VABGA@Bfi:T gfigGA®BVABIOAOB) 0 0 11 — (0,0) —(0,,()B|VABGAAAAHZl T ,HgOGBVABonB) 1 1 12 — (1,1) —(0,10,,IVA’E’GAAAB,1;l T ngOGAABVABonB) 0 1 -— (0,1) (010,”VABGAAB,1A°T,,,,1,§3 GAVABloAOB) 1 1 14 — (1,1) —(010,4VABGAABHgOTOBASG/AABVAB[0,03) 1 0 15 — (1,0) 247 Table 2. Comparison of an (w) , 01% (w) , and an (w) values calculated by in- tegrating x(r, r’; w) using the algorithm described here and by finite-field calculations performed with the MOLPRO17 quantum chemistry software package. Polarizabili- ties were calculated in the DZ, DZP, and aug—cc—pVDZ basis sets, and polarizabilities are given in a.u. Basis Set q,t,,(w) ayy(w) ozzz (w) DZ“ 0.00031451 0.00031451 5.74696714 DZ” 0 0 5.74696958 DZP“ 0.6753247 3 0.67532473 5.87133714 DZP” 0.67532474 0.67532474 5.87133956 aug-cc-pVDZ“ 4.35229766 4.35229763 6.54719224 aug-cc—pVDZb 4.35229593 4.35229593 6.54717965 a MOLPROl7 results. b These results were obtained by integrating over x(r, r’;w) using the algorithm de- scribed in this work. 248 Appendix C. Figures 249 Appendix C. Figures 0.1 —2 O 2 y (bohr) 0.15) 0| —2 0 2 Fig. 1. The charge-density susceptibility of the H2 molecule at the CISD level with a) = 0 a.u., r' = 0,0,0, x = 0, -3.25 s y s 3.25 a.u., -3.25 s z s 3.25 a.u., and Ay = A2 = 0.05 a.u. in the aug-cc-pVDZ basis set. For this calculation, the internuclear axis of H2 was oriented along the z-axis of the laboratory frame. 250 0.05 C ,- _0 05 1 4 L A 1 I I I I g; 0 Fig. 2. The charge-density susceptibility of the H2 molecule at the CISD level with to = 0.3858668352248763 a.u., r' = 0,0,0, x = 0, -3.25 s y s 3.25 a.u., -3.25 s z s 3.25 a.u., and Ay = A2 = 0.05 a.u. in the aug-cc-pVDZ basis set. For this calculation, the internuclear axis of H2 was oriented along the z-axis of the laboratory frame. 251 13 , 4X10 _2 > 0 2x103» 2 ~“/ : y mer) ‘ O i ' ‘ \._.. L —2x 1013 L l —4x1013 , Fig. 3. The charge-density susceptibility of the H2 molecule at the CISD level with a) = 0. 4812104263202694 a.u., r' = 0,0,0, x = 0, -3.25 s y s 3.25 a.u., -3.25 s z s 3.25 a.u., and Ay = A2 = 0.05 a.u. in the aug-cc-pVDZ basis set. For this calculation, the internuclear axis of H2 was oriented along the z-axis of the laboratory frame. 252 l 0.6’ —2 i o 2! 0.2 ; 0; -0.2: 1 g A g —2 o 2 z (bohr) Fig. 4. The charge-density susceptibility of the H2 molecule at the CISD level with a) = 0.3858668352248763 a.u., r' = 0,0,0.7, x = O, -3.25 s y s 3.25 a.u., -3.25 s z s 3.25 a.u., and Ay = A2 = 0.05 a.u. in the aug-cc-pVDZ basis set. For this calculation, the internuclear axis of H2 was oriented along the z-axis of the laboratory frame. 253 2x1013[ ‘2 0 2 .. \ y (bohr) l -2 l A A ‘ ' "f_“_“T"'_ 0 —2 x 1013 A—A 0 2 z (bohr) Fig. 5. The charge-density susceptibility of the H2 molecule at the CISD level with co = 0.4648380650856789 a.u., r' = 0,0,0.7, x = 0, -3.25 s y s 3.25 a.u., -3.25 s z s 3.25 a.u., and Ay = A2 = 0.05 a.u. in the aug-cc-pVDZ basis set. For this calculation, the internuclear axis of H2 was oriented along the z-axis of the laboratory frame. 254 AAAAAALQL 0111(0))(au) O 1 I“ y. ‘0 i 1 g: I) b - 1 ~5x1015 E u 7 . DZ 1 41:10“ A 3 i . DZP 1 l -1 5x10“ ~ 0 aug-cc-pVDZ , o 25 o s o 75 1 1 25 1 5 1 15 Fig. 6. The 22 component of the frequency-dependent polarizability (13(0)) of H2 as a function of frequency a) at the CISD level in the DZ, DZP, and aug-cc-pVDZ basis sets. 255 200 A L41 A 150 E . j . ' i . , 0 0 1 100 +5 .. . j A i '. . I ,7 50 _T c . . j :1 1 ~ 3 i o o o o o I . .‘j/ 4 ‘ l A o r ‘..0000....‘ .— 0 ’ ‘ é ) .8‘ : it! o. o . , 5 "5° ) 3 1 : ° . 100 i : . . DZ 2 i ' . DZP i o 1 -150 - . aug-cc-pVDZ , , . 1 . . 0.25 0.5 0.75 1 1 25 1 5 Fig. 7. The 22 component of the frequency-dependent polarizability 01,2 (0)) of H2 at the CISD level as a function of a) in the DZ, DZP, and aug-cc-pVDZ basis sets. Here, we show the data included in -2005 0122 (0)) £200 a.u. in Fig. 6. 256 .75 1x10 ...fiffifi.y,.fififi....fjfi ..r.+j,,..rf t . 1 : 1 7.5x1015 : 1 * 1 5x10” 3 3 2.5x1015 i A. : =1 5 A a o $ : : c : c : : —‘-— :x:::::: a :::--:-_:::::: I: : 7 8 : - ‘5 -2.5x1015; : e i ‘ -5x1015 E . DZP 1 4.5.1111: E ' 111211-me A i . 1 L x 1 1L 4 4 LL 4 kg 4 1 A L 1 #1_1 L + A 1 g1 0.25 0.5 0.75 1 1.25 1.5 1.75 Fig. 8. The xx component of the frequency-dependent polarizability (13(0)) of H2 at the CISD level as a function of a) in the DZP and aug-cc-pVDZ basis sets. 257 an ((0) (a.u.) r—r—v—w—r-j ‘T—H—V y—r-v—V-Or-j-w—v—r v—T—v—r v—T—r-r—v' w—v—r-T—r-r—r-T —1- y—‘v—v— r . 4 O 0 O O O O Fig. 9. The xx component of the frequency-dependent polarizability 012,,(01) of H2 at the CISD level as a function of (0 in the DZP basis set. 258 1111015 7.5111015 5111015 2.5111015 0 0 1 on N U11) TV—V—r—T—‘H 'T' "I—V—rfl W'T—P‘Y—T—‘Tfifi—Y“. (1..., ((1)) (a.u.) -2.5><1015 y —5><1015 4.5111015 ffi—Y—V—T—T‘Tfi—Tfiffifi—T —1 x 1016 00 (a.u.) Fig. 10. The yy component of the frequency-dependent polarizability (1),),(01) of H2 at the CISDlevel as a fimction of 00 in the aug-cc-pVDZ basis set. 259 V Fig. 1 1. The semi-circular contour C of radius R, in the upper complex half plane. In this figure, 1m and Re denote the imaginary and real axes, respectively. Also, 0 is the angle between the real axis and R1, and S is the portion of C off the real axis. 260 RAB }...............q...-1,13........1 /\ Fig. 12. Colinear arrangement of molecules A and B. In this figure, x, y, and 2 denote the axes of the laboratory flame, and x', y', and 2' denote the axes of the molecular flames of A and B. Also, A, and A2 are the nuclei of molecule A, B, and B2 are the nuclei of molecule B, COM, and COMB are the centers of mass of molecules A and B, and Rug is the distance between the center of mass of A and the center of mass of B. 261 A2 ’1’, 32 l”’ Z \ COM, COM, ' A1 31 Fig. 13. Parallel arrangement of molecules A and B. In this figure, x, y, and 2 denote the axes of the laboratory flame, and x', y', and 2' denote the axes of the molecular flames of A and B. Also, A, and A2 are the nuclei of molecule A, B, and B2 are the nuclei of molecule B, COMA and COMB are the centers of mass of molecules A and B, and R4,, is the distance between the center of mass of A and the center of mass of B. 262 A RAB Fig. 14. Perpendicular arrangement of molecules A and B. In this figure, x, y, and z denote the axes of the laboratory flame, x’, y', and 2' denote the axes of the molecular flame of A, and x", y", and 2" denote the axes of the molecular flame of B. Also, A, and A2 are the nuclei of molecule A, B, and B2 are the nuclei of molecule B, COM, and COMB are the centers of mass of molecules A and B, and RAB is the distance between the center of mass of A and the center of mass of B. 263 RHFI- HF3 I.........................u F2 H1 COMHFI RHFI- HF2 COMHF2 RHFZ- HF3 COMHF3 Fig. 15. Colinear arrangement of three HF molecules. In this figure, we have labeled the three HF molecules HF,, HF 2, and HF 3 in order to distinguish between them. Also, x, y, and 2 denote the axes of the laboratory flame, x', y', and 2' denote the axes of the molecular flames of each HF molecule, H,, H2, and H3 are the hydrogen nuclei in HF,, HF2, and HF3, F,, F2 and F3 are the fluorine nuclei in HF,, HF2 and HF3, and COMHH, COMHn, and COMHpg are the centers of mass of HF,, HF2, and HF3. Finally, RHF,-,,,:2, Rama”, and Run-HF3 are the distances between the centers of mass of HF, and HP 2, HF, and HF3, and HF2 and HF3, respectively. 264 H1 H2 1 " z COMHFI COMHFZ I F1 F2 *I...-.... ...-......-*..-.......‘..........'.| RHFl- HF2 RHFz- HF3 . ...-........I..III.-I......-'...............I RHFl-HF3 v Fig. 16. Parallel arrangement of three HF molecules. In this figure, we have labeled the three HF molecules HF,, HF2, and HF 3 in order to distinguish between them. Also, x, y, and z denote the axes of the laboratory flame, x', y', and 2' denote the axes of the molecular flames of each HF molecule, H,, H2, and H3 are the hydrogen nuclei in HF,, HF2, and HF3, F,, F2 and F3 are the fluorine nuclei in HF ,, HF2 and HF3, and COMHH, COMHn, and COMHB are the centers of mass of HF ,, HP 2, and HF3. 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