Tomasz Błachowicz, "Numerical calculations of rotational contributions to the scattering coefficient in a piezoelectric LiTaO3 crystal," J. Opt. Soc. Am. B 15, 2599-2606 (1998)
A systematic theoretical analysis is presented of rotational contributions to light scattering in a piezoelectric crystal with small birefringence. The influence of rotational contributions on the intensity of nonelastically scattered light in a crystal—a trigonal system with symmetry—is described. Rotation affects the optical signals that result from two quasi-transverse waves. Experimental confirmation of such rotational contributions employed a formalism based on looking for eigenvectors and eigenvalues of a so-called characteristic matrix, which is a function of the direction of acoustic-wave propagation and the elastic constants of the medium, in this case modified by the piezoelectric effect. All calculations were performed (for both the hypersonic and the ultrasonic acoustic ranges) for 514.5-nm light. Velocities of acoustic waves in the hypersonic region were calculated under elastic constants taken from 20.9 to 38.5 GHz. Hypersonic data appear more relevant for investigating the effect that consists in measuring the changes of photon frequency scattered on acoustical phonons lying at the beginning of the first Brillouin zone.
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Numerical Results for the A Configuration Based on Hypersonic Dataa
Angle (deg)
Eigenvalues of Characteristic Matrix for Quasi-Transverse Waves
Polarization Vector of First Quasi-Transverse Wave
Polarization Vector of Second Quasi-Transverse Wave
118
9.33
8.79
0.87198
0.43831
-0.21800
0.42652
-0.89880
-0.10110
119
9.29
8.78
0.86863
0.45204
-0.20290
0.44131
-0.89200
-0.09800
126
9.06
8.77
0.82280
0.55880
-0.10355
0.55466
-0.82930
-0.06800
127
9.03
8.77
0.81300
0.57520
-0.09052
0.57185
-0.81800
-0.06220
128
9.00
8.78
0.80232
0.59180
-0.07780
0.58914
-0.80610
-0.05600
129
8.97
8.78
0.79087
0.60847
-0.06550
0.60647
-0.79360
-0.04940
130
8.95
8.79
0.77863
0.62519
-0.05360
0.62376
-0.78050
-0.04230
139
8.93
8.80
0.76560
0.64193
-0.04200
0.64100
-0.76680
-0.03470
140
8.95
8.79
0.77859
0.62530
-0.05351
0.62380
-0.78040
-0.04230
141
8.97
8.78
0.79081
0.60860
-0.06545
0.60660
-0.79350
-0.04930
142
9.00
8.78
0.80220
0.59191
-0.07770
0.58930
-0.80600
-0.05590
143
9.03
8.77
0.81288
0.57540
-0.09041
0.57200
-0.81790
-0.06210
144
9.06
8.77
0.82270
0.55900
-0.10340
0.55480
-0.82920
-0.06790
Eigenvalues and states of polarization for the first and the second quasi-transverse waves. Quotients of the scattering coefficients belong to the (0.1 ; 10) range; the difference of the quotients calculated with and without rotational contributions is more than 0.01 (cf. Table 2).
Table 2
Numerical Results for the A Configuration Based on Hypersonic Dataa
Angle (deg)
Frequencies of Quasi- Transverse Waves
Scattering Coefficient for First Quasi-Transverse Wave,
(1/m)
Scattering Coefficient for Second Quasi-Transverse Wave,
(1/m)
Quotient of Scattering Coefficient without Rotational Contributions,
Quotient of Scattering Coefficient with Rotational Contributions,
Difference between Quotients,
(GHz)
(GHz)
118
21.50
20.87
0.24
0.23
0.01
119
21.46
20.87
0.19
0.18
0.01
126
21.20
20.86
0.23
0.27
0.04
127
21.16
20.86
0.61
0.68
0.07
128
21.13
20.87
1.40
1.53
0.13
129
21.10
20.88
2.98
3.22
0.24
130
21.07
20.89
6.31
6.77
0.46
139
21.05
20.90
5.81
6.09
0.28
140
21.08
20.89
2.77
2.92
0.15
141
21.11
20.88
1.36
1.45
0.09
142
21.14
20.88
0.66
0.71
0.05
143
21.17
20.87
0.30
0.33
0.03
144
21.21
20.87
0.12
0.14
0.02
Quotients of scattering coefficients belong to the (0.1 ; 10) range; the difference of the quotients calculated with and without rotational contributions is more than 0.01.
Table 3
Numerical Results for the B Configuration Based on Hypersonic Dataa
Angle (deg)
Frequencies of Quasi-Transverse waves
Scattering Coefficient for First Quasi-Transverse Wave,
(1/m)
Scattering Coefficient for Second Quasi-Transverse Wave,
(1/m)
Quotient of Scattering Coefficient without Rotational Contributions,
Quotient of Scattering Coefficient with Rotational Contributions,
Difference between Quotients,
(GHz)
(GHz)
9
22.14
21.71
9.18
9.14
0.04
10
22.18
21.69
7.18
7.15
0.03
11
22.21
21.67
5.90
5.87
0.03
12
22.25
21.66
5.00
4.97
0.03
13
22.30
21.64
4.33
4.30
0.03
14
22.34
21.63
3.81
3.78
0.03
15
22.38
21.62
3.38
3.35
0.03
16
22.43
21.61
3.02
2.99
0.03
17
22.48
21.61
2.72
2.69
0.03
73
22.48
21.61
2.72
2.69
0.03
74
22.43
21.61
3.02
2.99
0.03
75
22.38
21.62
3.38
3.35
0.03
76
22.34
21.63
3.81
3.78
0.03
77
22.30
21.64
4.33
4.30
0.03
78
22.25
21.66
5.00
4.97
0.03
79
22.21
21.67
5.90
5.87
0.03
80
22.18
21.69
7.18
7.15
0.03
81
22.14
21.71
9.18
9.14
0.04
110
22.56
21.75
6.35
6.39
0.04
111
22.59
21.74
7.46
7.51
0.05
112
22.61
21.73
8.82
8.88
0.06
158
22.61
21.73
8.82
8.88
0.06
159
22.59
21.74
7.46
7.51
0.05
160
22.56
21.75
6.35
6.39
0.04
Quotients of the scattering coefficients belong to the (0.1 ; 10) range; the difference of the quotients calculated with and without rotational contributions is more than 0.03.
Table 4
Numerical Results for the D Configuration Based on Hypersonic Dataa
Angle (deg)
Frequencies of Quasi-Transverse Waves
Scattering Coefficient for First Quasi-Transverse Wave,
(1/m)
Scattering Coefficient for Second Quasi-Transverse Wave,
(1/m)
Quotient of Scattering Coefficient without Rotational Contributions,
Quotient of Scattering Coefficient with Rotational Contributions,
Difference between Quotients,
(GHz)
(GHz)
0
22.06
21.80
0.59
0.58
0.01
90
22.06
21.80
0.59
0.58
0.01
91
22.08
21.79
0.76
0.74
0.01
92
22.10
21.79
0.90
0.88
0.02
93
22.13
21.78
1.01
0.99
0.02
94
22.15
21.78
1.09
1.07
0.02
95
22.18
21.77
1.13
1.11
0.02
96
22.21
21.77
1.15
1.13
0.02
97
22.23
21.77
1.14
1.12
0.02
98
22.26
21.76
1.11
1.10
0.02
99
22.29
21.76
1.07
1.05
0.02
100
22.32
21.76
1.01
1.00
0.01
101
22.34
21.76
0.95
0.93
0.01
102
22.37
21.76
0.88
0.86
0.01
103
22.39
21.76
0.80
0.79
0.01
167
22.39
21.76
0.80
0.79
0.01
168
22.37
21.76
0.88
0.86
0.01
169
22.34
21.76
0.95
0.93
0.01
170
22.32
21.76
1.01
1.00
0.01
171
22.29
21.76
1.07
1.05
0.02
172
22.26
21.76
1.11
1.10
0.02
173
22.23
21.77
1.14
1.12
0.02
174
22.21
21.77
1.15
1.13
0.02
175
22.18
21.77
1.13
1.11
0.02
176
22.15
21.78
1.09
1.07
0.02
177
22.13
21.78
1.01
0.99
0.02
178
22.10
21.79
0.90
0.88
0.02
179
22.08
21.79
0.76
0.74
0.01
180
22.06
21.80
0.59
0.58
0.01
Quotients of the scattering coefficients belong to the (0.1 ; 10) range; the difference of the quotients calculated with and without rotational contributions is more than 0.01.
Table 5
Comparison of Hypersonica and Ultrasonicb Values of the Elastic Constants for the crystal
Constant
Experimental Frequency of Acoustic Wave or Range of Frequencies (GHz)
Numerical Results for the A Configuration Based on Hypersonic Dataa
Angle (deg)
Eigenvalues of Characteristic Matrix for Quasi-Transverse Waves
Polarization Vector of First Quasi-Transverse Wave
Polarization Vector of Second Quasi-Transverse Wave
118
9.33
8.79
0.87198
0.43831
-0.21800
0.42652
-0.89880
-0.10110
119
9.29
8.78
0.86863
0.45204
-0.20290
0.44131
-0.89200
-0.09800
126
9.06
8.77
0.82280
0.55880
-0.10355
0.55466
-0.82930
-0.06800
127
9.03
8.77
0.81300
0.57520
-0.09052
0.57185
-0.81800
-0.06220
128
9.00
8.78
0.80232
0.59180
-0.07780
0.58914
-0.80610
-0.05600
129
8.97
8.78
0.79087
0.60847
-0.06550
0.60647
-0.79360
-0.04940
130
8.95
8.79
0.77863
0.62519
-0.05360
0.62376
-0.78050
-0.04230
139
8.93
8.80
0.76560
0.64193
-0.04200
0.64100
-0.76680
-0.03470
140
8.95
8.79
0.77859
0.62530
-0.05351
0.62380
-0.78040
-0.04230
141
8.97
8.78
0.79081
0.60860
-0.06545
0.60660
-0.79350
-0.04930
142
9.00
8.78
0.80220
0.59191
-0.07770
0.58930
-0.80600
-0.05590
143
9.03
8.77
0.81288
0.57540
-0.09041
0.57200
-0.81790
-0.06210
144
9.06
8.77
0.82270
0.55900
-0.10340
0.55480
-0.82920
-0.06790
Eigenvalues and states of polarization for the first and the second quasi-transverse waves. Quotients of the scattering coefficients belong to the (0.1 ; 10) range; the difference of the quotients calculated with and without rotational contributions is more than 0.01 (cf. Table 2).
Table 2
Numerical Results for the A Configuration Based on Hypersonic Dataa
Angle (deg)
Frequencies of Quasi- Transverse Waves
Scattering Coefficient for First Quasi-Transverse Wave,
(1/m)
Scattering Coefficient for Second Quasi-Transverse Wave,
(1/m)
Quotient of Scattering Coefficient without Rotational Contributions,
Quotient of Scattering Coefficient with Rotational Contributions,
Difference between Quotients,
(GHz)
(GHz)
118
21.50
20.87
0.24
0.23
0.01
119
21.46
20.87
0.19
0.18
0.01
126
21.20
20.86
0.23
0.27
0.04
127
21.16
20.86
0.61
0.68
0.07
128
21.13
20.87
1.40
1.53
0.13
129
21.10
20.88
2.98
3.22
0.24
130
21.07
20.89
6.31
6.77
0.46
139
21.05
20.90
5.81
6.09
0.28
140
21.08
20.89
2.77
2.92
0.15
141
21.11
20.88
1.36
1.45
0.09
142
21.14
20.88
0.66
0.71
0.05
143
21.17
20.87
0.30
0.33
0.03
144
21.21
20.87
0.12
0.14
0.02
Quotients of scattering coefficients belong to the (0.1 ; 10) range; the difference of the quotients calculated with and without rotational contributions is more than 0.01.
Table 3
Numerical Results for the B Configuration Based on Hypersonic Dataa
Angle (deg)
Frequencies of Quasi-Transverse waves
Scattering Coefficient for First Quasi-Transverse Wave,
(1/m)
Scattering Coefficient for Second Quasi-Transverse Wave,
(1/m)
Quotient of Scattering Coefficient without Rotational Contributions,
Quotient of Scattering Coefficient with Rotational Contributions,
Difference between Quotients,
(GHz)
(GHz)
9
22.14
21.71
9.18
9.14
0.04
10
22.18
21.69
7.18
7.15
0.03
11
22.21
21.67
5.90
5.87
0.03
12
22.25
21.66
5.00
4.97
0.03
13
22.30
21.64
4.33
4.30
0.03
14
22.34
21.63
3.81
3.78
0.03
15
22.38
21.62
3.38
3.35
0.03
16
22.43
21.61
3.02
2.99
0.03
17
22.48
21.61
2.72
2.69
0.03
73
22.48
21.61
2.72
2.69
0.03
74
22.43
21.61
3.02
2.99
0.03
75
22.38
21.62
3.38
3.35
0.03
76
22.34
21.63
3.81
3.78
0.03
77
22.30
21.64
4.33
4.30
0.03
78
22.25
21.66
5.00
4.97
0.03
79
22.21
21.67
5.90
5.87
0.03
80
22.18
21.69
7.18
7.15
0.03
81
22.14
21.71
9.18
9.14
0.04
110
22.56
21.75
6.35
6.39
0.04
111
22.59
21.74
7.46
7.51
0.05
112
22.61
21.73
8.82
8.88
0.06
158
22.61
21.73
8.82
8.88
0.06
159
22.59
21.74
7.46
7.51
0.05
160
22.56
21.75
6.35
6.39
0.04
Quotients of the scattering coefficients belong to the (0.1 ; 10) range; the difference of the quotients calculated with and without rotational contributions is more than 0.03.
Table 4
Numerical Results for the D Configuration Based on Hypersonic Dataa
Angle (deg)
Frequencies of Quasi-Transverse Waves
Scattering Coefficient for First Quasi-Transverse Wave,
(1/m)
Scattering Coefficient for Second Quasi-Transverse Wave,
(1/m)
Quotient of Scattering Coefficient without Rotational Contributions,
Quotient of Scattering Coefficient with Rotational Contributions,
Difference between Quotients,
(GHz)
(GHz)
0
22.06
21.80
0.59
0.58
0.01
90
22.06
21.80
0.59
0.58
0.01
91
22.08
21.79
0.76
0.74
0.01
92
22.10
21.79
0.90
0.88
0.02
93
22.13
21.78
1.01
0.99
0.02
94
22.15
21.78
1.09
1.07
0.02
95
22.18
21.77
1.13
1.11
0.02
96
22.21
21.77
1.15
1.13
0.02
97
22.23
21.77
1.14
1.12
0.02
98
22.26
21.76
1.11
1.10
0.02
99
22.29
21.76
1.07
1.05
0.02
100
22.32
21.76
1.01
1.00
0.01
101
22.34
21.76
0.95
0.93
0.01
102
22.37
21.76
0.88
0.86
0.01
103
22.39
21.76
0.80
0.79
0.01
167
22.39
21.76
0.80
0.79
0.01
168
22.37
21.76
0.88
0.86
0.01
169
22.34
21.76
0.95
0.93
0.01
170
22.32
21.76
1.01
1.00
0.01
171
22.29
21.76
1.07
1.05
0.02
172
22.26
21.76
1.11
1.10
0.02
173
22.23
21.77
1.14
1.12
0.02
174
22.21
21.77
1.15
1.13
0.02
175
22.18
21.77
1.13
1.11
0.02
176
22.15
21.78
1.09
1.07
0.02
177
22.13
21.78
1.01
0.99
0.02
178
22.10
21.79
0.90
0.88
0.02
179
22.08
21.79
0.76
0.74
0.01
180
22.06
21.80
0.59
0.58
0.01
Quotients of the scattering coefficients belong to the (0.1 ; 10) range; the difference of the quotients calculated with and without rotational contributions is more than 0.01.
Table 5
Comparison of Hypersonica and Ultrasonicb Values of the Elastic Constants for the crystal
Constant
Experimental Frequency of Acoustic Wave or Range of Frequencies (GHz)