Excited-state Raman spectroscopy with and without actinic excitation: S1 Raman spectra of trans-azobenzene A. L. Dobryakov, M. Quick, I. N. Ioffe,a A. A. Granovsky,b N. P. Ernsting,* and S. A. Kovalenko* Department of Chemistry, Humboldt-Universität zu Berlin, Brook-Taylor-Str. 2, D-12489 Berlin, Germany Supporting Information 1 A. THE ELECTRIC FIELD AND BASIC CALCULATION OF THE TRANSIENT RAMAN SPECTRUM Nonlinear spectroscopic signals can be calculated with the response function formalism developed by Mukamel et al.1,2 The basic concepts and key definitions from Ref. 3-9 are adapted for the present work. The femtosecond stimulated Raman signal is treated within the fifth-order perturbation formalism. An useful approximation is the assumption that the interaction with the actinic pump and the scattering events, induced by the Raman and probe pulses, are well separated in time with a time delay td. The actinic pump prepares the system with population in a specific excited state p(a ) . The Raman and probe pulses induce the optical changes in the third-order of the incoming electric fields. In a previous papers3-9 we developed a unified description of sequential and coherent contributions to optical transients in the third-order. The sequential contribution generates the background and is not considered here. We focus on the coherent contribution which arises from the simultaneous Raman and probe pulses, A(3) (2 ,0) , and generates the background-free Raman signal. The quantity of interest is the transient spectrum A ( 5) (2 , t d ) induced by the actinic pump and measured at delay td by the coinciding Raman and probe pulses as function of probe frequency 2 ; it can be written as A(5) (2 , t d ) 22 p(a , t d )A(3) (2 ,0) (A1) a A(3) (2 ,0) Im P(3) (2 ) / E 2 (2 ) (A2) Note that in the absence of actinic excitation p(a,td) corresponds to the timeindependent population in the ground state, and the ground state Raman signal is defined by Eq.(A2). The induced polarization P(3) (2 ) which is taken in the probe direction k 2 k1 k1 k 2 , and which causes the transient signal A(3) (2 ,0) , is captured though the nonlinear response R ( 3) ( t 3 , t 2 , t1 ) 1-2 and the Fourier transform ( FT(...) ) of the effective coherent field product E (3) ( t , t 3 , t 2 , t1 ) 4-9 0 0 0 P (3) (2 ) dt 3 dt 2 dt1R (3) ( t 3 , t 2 , t1 )FT E (3) ( t, t 3 , t 2 , t1 ) . E (3) ( t , t 3 , t 2 , t1 ) E1 ( t , t 3 , t 2 , t1 ) E 2 ( t , t 3 , t 2 , t1 ) E1(t, t 3 , t 2 , t1 ) E1(t t 3 )E2 (t t 3 t 2 )E1 (t t 3 t 2 t1) (A3) (A4) (A5) 2 E2 (t, t 3 , t 2 , t1 ) E1 (t t 3 )E1 (t t 3 t 2 )E2 (t t 3 t 2 t1 ) (A6) E1 (t ) and E 2 (t ) represent in Eqs.(A5-A6) the Raman/probe pulses, ~ E1, 2 ( t ) E1, 2 ( t ) exp( i1, 2 t ) (A7) ~ where 1, 2 and E1, 2 are the central frequency and temporal envelope of Raman/probe pulses, respectively. Exact forms for FTE (3) ( t , t 3 , t 2 , t1 ) with transform-limited and linearly chirped Gaussian envelopes are presented in Ref. 3-8 and the reader is referred to these papers for details. Here we present a useful form for the calculation of backgroundfree Raman signal with two-sided exponential decay pulse envelope9, i.e, ~ E1, 2 ( t ) exp 1, 2 t with pulse width 1, 2 . This form is preferred over a Gaussian, since it allows one to find a simple analytic expression. When the probe is a much shorter than Raman pulse, 1 2 , the result is obtained as FT E (3) ( t , t 3 , t 2 , t1 ) I1 ( t 3 , t 2 , t1 ) I 2 ( t 3 , t 2 , t1 ) (A8) I1 (t 3 , t 2 , t1 ) exp i2 t 3 i(2 1 i1 )t 2 i(1 i1 )t1 (A9) I2 (t 3 , t 2 , t1 ) exp i2 t 3 i(2 1 i1 )t 2 i(2 2i1 )t1 (A10) The calculation of P(3) (2 ) in Eq. (A3) involves a triple integration. To calculate the coherent contribution a reduced response function is used in the general form3-8 ~ t i ~ t i ~ t ). R (k3) (t 3 , t 2 , t1 ) iˆ k exp( i mn 3 kl 2 pq 1 (A11) ~ i . Two subscripts indicate the frequency with complex frequency ab ab ab difference, ab a b , and dephasing rate ab between states a and b . A pathway k is specified by subscripts mn , kl, pq and ̂k indicates the product of dipole matrix elements for transitions involved in the given pathway. Then the third-order polarization spectrum P (3) (2 ) is written as the sum over all possible pathways k : P(3) (2 ) k 0 0 0 ( 3) dt 3 dt 2 dt1R k (t 3 , t 2 , t1 ) I1 (t 3 , t 2 , t1 ) I2 (t 3 , t 2 , t1 ) (A12) After substitution of I1, 2 ( t 3 , t 2 , t1 ) and R (k3) (t 3 , t 2 , t1 ) into Eq. (A12), the integration is carried out analytically and the induced signal is expressed by auxiliary functions F1, 2 (mn , kl, pq) 3 A (3) 2 ,0 ˆ 1F1 (mn , kl, pq) ˆ 1F2 (mn , kl, pq) k F1, 2 mn , kl, pq Im fmn gkl h(pq1),( 2) (A13) (A14) ~ ), fmn 1 /(2 mn ~ i ) gkl i /(2 1 kl 1 (A15) ~ i ) , h(pq1) i /(1 pq 1 ~ 2i ) h(pq2) i /(2 pq 1 (A16) Taking the imaginary part in Eq. A14, the Raman signal in the 1 limit can be presented as F1 (mn , kl, pq) F2 (mn , kl, pq) a1x 2 b1x c1 (x mn )2 el2 (x )2 vib2 (pq1) 2 el2 a 2 x 2 b2 x c2 2 ( x mn ) 2 el2 ( x ) 2 vib ( x (pq2) )2 el2 (A17) (A18) a1 el , b1 el (mn (pq1) ) vib(pq1) , (A19) c1 el2vib el(mn (pq1) ) vibmn (pq1) (A20) a 2 2el vib , b2 el (mn 2 (pq2) ) vib (mn (pq2) ) , (A21) c2 el2vib el(mn (pq2) ) vibmn (pq2) (A22) where x 2 1 is the probe-Raman detuning, is vibrational frequency, and we used (pq1),( 2) 1 pq , mn 1 mn and el mn pq , vib kl . The overall transient signal is the sum of all pathways [k] where all vibrational manifolds in ground gv1, v2 ,... and excited states ev1, v2 ,... , f v1, v2 ,... are included. As regards the influence of environment, remember that this was already taken into account by the empirical population and pure dephasing times. The corresponding decay rates discussed so far are the result of fast perturbations by solvents. The remaining influence on the chromophore is considered here in the limit of an infinitely long bath correlation time, i.e. for a frozen solvent. This static inhomogeneous broadening may be incorporated1 by convolution the homogeneous response functions, Eq. (A13), with a static (Gaussian) distribution of transition frequencies. 4 B. CALCULATIONS OF RAMAN DIAGRAMS Here we present the rules to calculate the Raman diagrams presented in Fig. 2. The induced polarization P(3) (2 ) which causes the transient signal A (3) 2 ,0 , is the sum over possible vibronic pathways [k] (see Eq. A13). We focus on the Raman pathways which are presented in Fig. 2 as energy ladder diagrams. For simplicity consider response function R 3 (diagram 1 in Fig. 2) and R1 (diagram 3a in Fig. 2) in Fig. S1. The system is prepared in the S0 state labeled as 1. R3(t3,t2,t1) E2 E1 c c d c a c a b a a E2 E2 E1 h g12 f 32 3 g 1 E2 c c d c d b d a a a ( 2) h 31 g 34 f 31 (1) 13 2 R1(t3,t2,t1) 1 3 E1 E1 e 4 1 3a Fig S1. Double-side Feyman1 and ladder diagrams for femtosecond stimulated Raman scattering of a model system with three electronic states. The system is prepared in the S0 state labeled as 1. Double-sided Feynman diagrams are named according to Ref. 1,2,7, the ladder diagrams are labelled according to Fig.2. The subscripts (1) and (2) denote the interaction order (see Eqs. A5-A6). Dashed arrows represent bra-side and full arrows ketside interaction. The electronic states are dressed with modes g and e (1) The first interaction alters the “bra” q-index ( h13 , F1mn , kl, pq F1mn , kl,13 ), ( 2) or the “ket” p-index ( h 31 , F2 mn , kl, pq F2 mn , kl,31 ) for diagrams R 3 and R1 , respectively. We introduce the detuning of the Raman frequency from the electronic transition induced by this interaction (pq1) 1 pq , (pq2) 1 pq (B1) Analogously the next interaction changes index k or l in g kl , i.e. F1mn , kl, pq F1mn ,12,13 and F2 mn , kl, pq F2 mn ,34,31. The vibrational coherence 5 generated after these interactions is indicated by factors g12 and g 34 and corresponds to the complex frequency ~ i i kl kl kl vib (B2) The last interaction changes the m-index for R 3 and n-index for R1 , i.e., F1 mn , kl, pq F1 32,12,13 and F2 mn , kl, pq F2 31,34,31 . The corresponding electronic detuning from the Raman frequency is given as mn 1 mn (B3) Taking the imaginary part in Eq. A14, the Raman signal in the 1 limit can be presented as F1 (mn , kl, pq) F2 (mn , kl, pq) a1x 2 b1x c1 (B4) (x mn )2 el2 (x )2 vib2 (pq1) 2 el2 a 2 x 2 b2 x c2 2 ( x (pq2) ) 2 el2 ( x mn ) 2 el2 ( x ) 2 vib (B5) a1 el , a 2 2el vib (B6) b1 el (mn (pq1) ) vib(pq1) , b2 el (mn 2 (pq2) ) vib (mn (pq2) ) (B7) c1 el2vib el(mn (pq1) ) vibmn (pq1) , c2 el2vib el(mn 2pq ) vibmn (pq2) (B8) where x 2 1 is the probe-Raman detuning and el mn pq , vib kl . Then, by some rearrangements, the contributions from R3/R1 diagrams is captured through (1) A1 F1 32,12,13 Im f 32 g12 h13 A 0 ( g ) L(vib , g ) ( 2) A 3b F2 31,34,31 Im f 31 g 34 h 31 A 0 ( e ) L(vib , e ) (B9) (B10) Here we have introduced the normalization factor A0 1/ el / vib and the auxiliary functions can be evaluated as 2 vib L(vib , g ) 2 el 2 2 el 2 2 2 eg el ( x e ) vib eg el 2 2 2 (B11) 6 el vib 2 el 2 2 2 2 2 eg el ( x e ) vib eg el 2 L(vib , , e ) eg el 2 ( g ) ( e ) el 2 2 (B12) 2 (B13) 2 ( eg e ) 2 el el 2 2 2( eg e )(el vib ) el vib 2 (x e ) (B14) Here we introduce detuning of the Raman frequency from the electronic transition g e , i.e. eg 1 eg . Then, by some rearrangements, the contributions from R3 diagram is captured through vib A1 2 el 2 2 4A 0 el 1 ( g ) 2 vib 2 2 (B15) The contributions from diagrams 3a and 3b in Fig.2 together with the contributions from excited state e ( diagrams 2a and 2b, see Fig.2) are obtained in a similar manner ( eg e g / 2)( g ) el 2 A 3a A 3b 1 2 2 4A 0 el vib el eg 2 2 vib (B16) ( ) 2 2 e vib 2 2 2 A 2a A 2 b fe ( g ) el el vib 1 4A 0 el vib el 2 eg 2 el 2 fe 2 ( e ) 2 vib 2 (B17) Here we used the detuning of the Raman frequency from the electronic transition e f , i.e. fe 1 fe . Collecting all S0-diagrams in Fig.2 we obtain the S0-Raman (for simplicity we consider here that ge fe ) signal as vib A 2 el 2 2 4A 0 el ( g ) 2 vib 2 2 ( e g )( g ) 2 el 2 2 2 el vib el 2 2 vib ( ) 2 2 e vib (B18) 7 The contributions from diagrams 4-8 in Fig.2 may be obtained is the similar manner. C. DOUBLE-SIDED FEYNMAN DIAGRAMS AND DIAGRAMS, AND THE TRANSIENT RAMAN SIGNAL ENERGY LADDER We consider the electronic ground state g , the first excited state e , and a higher electronic state f . To treat vibrational activity we dress each electronic state with modes g , e and f . The (dimensionless) mode displacements between g and e are 2 . For simplicity, the same displacements are assumed between modes in e and f and transition dipole momets are eg fe 1 . The detuning of the Raman frequency is equal for g e and e f electronic transitions, i.e. eg fe . Dephasing times contain the electronic ( el 1/ 5 fs ) and vibrational ( vib 1 / 5 ps ) dephasing times. Simulations of transient Raman signal for the model system with three electronic level are shown in Figs.S2-S5. 8 R6(t3,t2,t1) R3(t3,t2,t1) E2 c E1 E2 c d c a c a E2 a E2 _ c b d b d a a a E2 E1 2a 1 -1000 -500 0 +500 +1000 -1.0 -1.5 c c d c d c E1 b d b d b a b d a a b a a a a a a E1 E2 E1 _ 3a 3b -1000 -500 0 +500 -1000 E1 E1 0.0 -1 RA2b E2 _ detuning, (cm ) 1.0 0.0 -0.5 R2 RA3a -1 detuning, (cm ) -1000 -500 0 +500 -1000 0.5 0 -2.0 c d -1 -1000 -500 0 +500 +1000 E2 c b 2b detuning, (cm ) RA2a -1 detuning, (cm ) A1 R2(t3,t2,t1) c + 0.0 -0.5 E2 b E1 + 1 differential absorbance A (a.u.) b b E1 E1 R1(t3,t2,t1) E 2 b b a R5(t3,t2,t1) -1.0 -1 detuning, (cm ) -0.5 -1000 -500 0 +500 +1000 -1.0 0.0 -2.5 -1120 -1100 -1080 -1 Stokes wavenumber (cm ) -920 -900 -880 -1 Stokes wavenumber (cm ) -920 -900 -880 -1 Stokes wavenumber (cm ) -920 -900 -880 -1 Stokes wavenumber (cm ) -920 -900 -880 -1 Stokes wavenumber (cm ) Fig. S2. Double-sided Feynman1 and energy ladder diagrams representing the main pathways for stimulated Raman scattering (starting in S0, without actinic excitation) of a model system with three electronic level. Double-side Feynman diagrams are named according to Ref. 1,2,7, the ladder diagrams are labelled according to Fig.2. 9 differential absorbance A (a.u.) 1 0 A1 -1 A2a+A2b A3a+A3b -2 -1120 detuning -1100 -920 -900 -880 -1 Stokes wavenumber (cm ) Fig. S3. Resonant femtosecond stimulated Raman signal A Ai (starting in S0, without actinic excitation) of a model system with three electronic level ( el 1/ 5 fs , vib 1 / 5 ps ) with vibrational mode g 1100 cm1 and e 900 cm 1 in the ground and excited electronic states, respectively. 10 R8(t3,t2,t1) R3(t3,t2,t1) R3(t3,t2,t1) R8(t3,t2,t1) R5(t3,t2,t1) R6(t3,t2,t1) E2 E2 d d a d a c a b a a E2 E1 c E1 E1 E2 E2 c d c a c E1 a b E2 a a c E1 d d a d d c a c a b a a a E2 E 2 E1 E1 c a b a a E2 E1 + _ 4 b b c b d b a b a a detuning, cm 1 6 7 0 detuning, cm detuning, cm A5 -1 -1000 -500 0 +500 +1000 -2 -900 -880 -1 Stokes wavenumber (cm ) -920 b E1 d a a a 8b -1 A6 -1 -1000 -500 0 +500 +1000 -2 2 detuning, cm 7 E2 1 -1000 -500 0 +500 +1000 8a -1000 -500 0 +500 +1000 1 -1 -1 -900 -880 -1 Stokes wavenumber (cm ) -920 -900 Stokes wavenumber [1/cm] -880 1 detuning, cm A8b -1 -1000 -500 0 +500 +1000 0 0 0 -920 d 8a detuning, cm 0 -1 b E1 + -1 -1000 -500 0 +500 +1000 b c _ 5 A4 b + 0 2 E2 E2 E1 + differential absorbance A (a.u.) E1 c -920 -900 -880 -1 Stokes wavenumber (cm ) -1120 -1100 -1080 -1120 -1 -1100 -1080 -1 Stokes wavenumber (cm ) Stokes wavenumber (cm ) Fig. S4. Double-sided Feynman1 and energy ladder diagrams representing the main pathways for stimulated Raman scattering (starting in S1, with actinic excitation) of a model system with three electronic level. Double-side Feyman diagrams are named according to Ref. 1,2,7, the ladder diagrams are labelled according to Fig.2. 11 differential absorbance A (a.u.) 4 2 0 A A8a+A8b -2 A5+A6 A4+A7 -4 -1120 -1100 -1080 detuning =0 -920 -900 -880 -1 Stokes wavenumber (cm ) Fig. S5. Resonant femtosecond stimulated Raman signal A Ai (starting in S1, with actinic excitation) of a model system with three electronic level ( el 1/ 5 fs , vib 1 / 5 ps ) with vibrational mode g 1100 cm1 and e 900 cm 1 in the ground and excited electronic states, respectively. 12 References 1 S. Mukamel, Principles of Nonlinear Optical Spectroscopy (Oxford University: New York, 1995). 2 Y.J. Yan, S. Mukamel, Phys. Rev. A 41, 6485 (1990); S. Mukamel, Annu. Rev. Phys. Chem. 41, 647 (1990); R.F. Loring, Y.J. Yan, S. Mukamel, J. Chem. Phys. 87, 5840 (1987); Y.J. Yan, L.E. Fread, S. Mukamel, J. Phys. Chem. 93, 8149 (1989). 3 S.A. Kovalenko, A.L. Dobryakov, J. Ruthmann, N.P. Ernsting, Phys. Rev. A 59, 2369 (1999). 4 A.L. Dobryakov, S.A. Kovalenko, N. P. Ernsting, J. Chem. Phys. 119, 988 (2003). 5 A.L. Dobryakov, S.A. Kovalenko, N.P. Ernsting, J. Chem. Phys. 123, 044502 (2005) 6 A.L. Dobryakov, N.P. Ernsting, W. Gawelda, C. Bressler, M. Chergui, in: O. Kühn, L. Wöste (Eds) Analysis and Control of Ultrafast Photoinduced Reactions, Springer Series in Chemical Physics, Vol. 87, Springer, Heidelberg, 2007, pp.689. 7 A.L. Dobryakov, J.L. Perez Lustres, S.A. Kovalenko, N. P. Ernsting, Chem. Phys. 347, 127 (2008). 8 A.L. Dobryakov, N. P. Ernsting, J. Chem. Phys. 129, 184504 (2008). 9 A. Weigel, A. Dobryakov, B. Klaumuenzer, M. Sajadi, P. Saalfrank, N.P. Ernsting, J. Phys.Chem. B 115, 3656 (2011). 13 FSR spectra of trans-stilbene in n-hexane differential absorbance A (mOD) 0 S0 measured calculated -1 0 -1 S1 measured calculated -2 200 400 600 800 1000 1200 1400 1600 -1 Stokes wavenumber (cm ) Fig. S6. FSR spectra of trans-stilbene in n-hexane compared to calculations. Note that the spectral pattern in S0 and S1 state are different. At low frequencies, Raman activity is stronger in S1 than in S0 because the molecule is less rigid in the excited state. 14 experimental and calculated Raman spectra 0.0 -0.2 differential absorbance (mOD) -0.4 x20 -0.6 S0 -0.8 measured calculated -1.0 -1.2 200 400 644 0.04 0.02 600 202 294 800 1000 1200 1400 1600 847 0.00 -0.02 190 305 881 -0.04 -0.06 without actinic exc. with actinic exc. 1526 calculated 1566 657 -0.08 -0.10 200 400 600 S1 800 1000 1200 1400 1600 -1 Stokes wavenumber (R )(cm ) Fig. S7. Enlarged copy of Fig. 5 shows that calculated Raman frequencies (green) are in reasonable agreement with experiment. (These details are difficult to see in Fig. 5 which is of one column width). 15 S0(14N) S1(14N) S0(15N) S1(15N) Raman shift (cm-1) Fig. S8. S0 and S1 spectra of trans-azobenzene in solution for two isotopomers 15 14 N and N from Ref. 23. Strong similarity between the S1 and S0 spectral is possibly due to imperfect subtraction of the S0 contributions. 16
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