HAL Id: jpa-00224132
https://hal.archives-ouvertes.fr/jpa-00224132
Submitted on 1 Jan 1984
HAL is a multi-disciplinary open access archive for the deposit and dissemination of sci- entific research documents, whether they are pub- lished or not. The documents may come from teaching and research institutions in France or abroad, or from public or private research centers.
L’archive ouverte pluridisciplinaire HAL, est destinée au dépôt et à la diffusion de documents scientifiques de niveau recherche, publiés ou non, émanant des établissements d’enseignement et de recherche français ou étrangers, des laboratoires publics ou privés.
THEORY OF BRILLOUIN SCATTERING BY AN ISOTROPIC ELASTIC PLATE
D. Tilley, E. Albuquerque, M. Oliveros
To cite this version:
D. Tilley, E. Albuquerque, M. Oliveros. THEORY OF BRILLOUIN SCATTERING BY AN ISOTROPIC ELASTIC PLATE. Journal de Physique Colloques, 1984, 45 (C5), pp.C5-103-C5-107.
�10.1051/jphyscol:1984514�. �jpa-00224132�
JOURNAL DE PHYSIQUE
Colloque
C5, supplkmentau
n04,Tome
45,avril
1984 page C5-103THEORY OF B R I L L O U I N SCATTERING
BY AN
I S O T R O P I C E L A S T I C P L A T ED.R.
T i l l e y , E.L. Albuquerque* and M.C. Oliveros*Department o f Physics, U n i v e r s i t y of Essex, Colchester COQ
3SQ,U.K.
* ~ e ~ a r t a m e n t o de Fisica, Universidade Federal do Rio Grande do Norte, 59.000-Natal-RN, Brazil
RLsumL
-
Nous p r d s e n t o n s une t h s o r i e de l a d i f f u s i o n de l a lumiPre p a r l e s ondes s u p e r f i c i e l l e s d'une plaque L l a s t i q u e r 6 s u l t a n t d e s modes d e t o r s i o n( o n d u l a t i o n ) e t d e s modes l o n g i t u d i n a u x ( p d r i s t a l t i q u e s ) . Les r g s u l t a t s s o n t i l l u s t r L s p a r des c a l c u l s numgriques.
A b s t r a c t
-
The theory of s u r f a c e - r i p p l e l i g h t - s c a t t e r i n g by t h e bending ( u n d u l a t i o n ) and l o n g i t u d i n a l ( p e r i s t a l t i c ) modes of an e l a s t i c p l a t e i s p r e s e n t e d , t o g e t h e r w i t h r e s u l t s of i l l u s t r a t i v e numerical c a l c u l a t i o n s .The propagating modes i n an e l a s t i c p l a t e of g e n e r a l t h i c k n e s s a r e c a l l e d Lamb waves;
both t h e d e r i v a t i o n of t h e Lamb wave spectrum and i t s d e s c r i p t i o n a r e r e l a t i v e l y complicated./l/ I n t h e l i m i t of t h i c k n e s s L much l e s s than a c o u s t i c wavelength Xa t h e equations of motion can be g r e a t l y s i m p l i f i e d . / 2 / I t i s then found t h a t t h e modes c o n s i s t of a bending, o r u n d u l a t i o n a l , mode i n which t h e two i n t e r f a c e s move
i n phase, and a l o n g i t u d i n a l , o r p e r i s t a l t i c mode i n which t h e i n t e r f a c e s move i n a n t i p h a s e . These a r e i n f a c t t h e lowest o r d e r Lamb waves. / 3 / The bending mode of an i s o t r o p i c p l a t e of d e n s i t y p ' supported on an i d e a l l i q u i d of d e n s i t y p has d i s - p e r s i o n e q u a t i o n
where Qx i s t h e wave v e c t o r i n t h e p l a n e of t h e p l a t e , and
E i s Young's modulus, o P o i s s o n ' s r a t i o and vT t h e b u l k t r a n s v e r s e sound v e l o c i t y . The l o n g i t u d i n a l mode of an unsupported p l a t e has d i s p e r s i o n e q u a t i o n
w = v Q
P x
where v 2 = ~ / ~ ( l - o ~ ) , s o t h a t v < v <
v
where v i s t h e bulk l o n g i t u d i n a l soundP T P - L' L
v e l o c i t y .
Green f u n c t i o r ~ s and f l u c t u a t i o n power s p e c t r a a r e found by means of l i n e a r response t h e o r y and t h e f l u c t u a t i o n - d i s s i p a t i o n theorem. For t h e bending mode t h e s e q u a n t i - t i e s a r e
Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphyscol:1984514
C5-104 JOURNAL DE PHYSIQUE
and
where
2
i s t h e s u r f a c e a r e a of t h e f i l m and w i s t h e frequency g i v e n by eqn. ( 1 ) .Q
The r e s u l t s a r e g i v e n i n terms of u t h e displacement of t h e median p l a n e i n t h e z'
normal d i r e c t i o n , s i n c e a l l s t r a i n and displacement components can b e found from u
.I2/
The main q u a l i t a t i v e f e a t u r e s of eqn. (5) a r e t h e p r o p o r t i o n a l i t i e s t o Q - ~X
and L - ~ .
For t h e l o n g i t u d i n a l mode of an unsupported f i l m we f i n d
and
The t h e o r y of B r i l l o u i n s c a t t e r i n g by Lamb modes has been t r e a t e d i n a g e n e r a l way by B o r t o l a n i e t a1./4/ They i n c l u d e coupling v i a t h e "bulk" acousto-optic mechanism a s w e l l a s by t h e s u r f a c e r i p p l e mechanism. I n p r i n c i p l e t h e r e s u l t s f o r t h e c r o s s s e c t i o n f o r s c a t t e r i n g by t h e bending and l o n g i t u d i n a l modes should be o b t a i n a b l e a s l i m i t i n g cases of t h e i r e x p r e s s i o n s . I n p r a c t i c e , however, i t i s much simpler t o d e r i v e t h e r e s u l t s d i r e c t l y w i t h t h e u s e of t h e power s p e c t r a of eqns. (5) and ( 7 ) . We r e t a i n only t h e s u r f a c e r i p p l e mechanism, which a s w i l l b e seen, i s dominant f o r s c a t t e r i n g by t h e bending mode of a supported p l a t e , and f o r s c a t t e r i n g by t h e l o n g i t u d i n a l mode whether t h e p l a t e i s supported o r n o t .
S c a t t e r i n g by t h e r i p p l e s on a s i n g l e i n t e r f a c e was t r e a t e d by Marvin e t a l . , / 5 / a n d t h e method i s r e a d i l y g e n e r a l i s e d f o r two i n t e r f a c e s . P a r t i c u l a r importance a t t a c h e s t o t h e asymptotic forms of t h e s c a t t e r e d f i e l d s f o r small L. We f i n d t h a t f o r an unsupported p l a t e b o t h t h e back s c a t t e r e d and t h e forward s c a t t e r e d f i e l d s a r e of o r d e r L f o r s c a t t e r i n g by t h e bending mode b u t independent of L f o r s c a t t e r i n g by t h e l o n g i t u d i n a l mode. These r e s u l t s hold f o r both s and p ~ o l a r i z a t i o n ; they a r i s e , l o o s e l y speaking, because t h e i n t e r f e r e n c e between l i g h t s c a t t e r e d o f f t h e two i n t e r - f a c e s i s d e s t r u c t i v e f o r t h e bending mode but c o n s t r u c t i v e f o r t h e l o n g i t u d i n a l mode.
For a supported p l a t e , i n which t h e r e f r a c t i v e i n d i c e s on e i t h e r s i d e of t h e p l a t e a r e d i f f e r e n t , t h e s c a t t e r e d f i e l d s a r e independent of L i n a l l c a s e s . This f a c t s u b s t a n t i a t e s t h e a s s e r t i o n t h a t t h e r i p p l e mechanism i s dominant f o r s c a t t e r i n g by a supported p l a t e , s i n c e t h e acousto-optic c o n t r i b u t i o n i s of o r d e r L.
Given t h e s c a t t e r e d f i e l d s , t h e c a l c u l a t i o n of t h e d i f f e r e n t i a l c r o s s s e c t i o n i s s t a n d a r d . / 6 / We c o n s i d e r i n p a r t i c u l a r s c a t t e r i n g by an unsupported f i l m i n s p o l a r i z a t i o n when t h e p l a n e of s c a t t e r i n g c o i n c i d e s w i t h t h e p l a n e of incidence.
For a n g l e of i n c i d e n c e OI and angle of s c a t t e r i n g €is t h e frequency s h i f t Aw f o r Stokes s c a t t e r i n g o f f t h e bending mode i s given by
and t h e d i f f e r e n t i a l c r o s s s e c t i o n i s
d20 cos2e
- a - S
lr,I2
dCldwS cose S(w-0
I L(sin0 I
-
s i n e S ) 4Q
where wI i s t h e i n c i d e n t frequency and
TS
i s a slowly varying f u n c t i o n of €IS and 8 I' The corresponding r e s u l t s f o r t h e l o n g i t u d i n a l mode a r eI I
cAw/vTwI = 2 ' / ( ~ - 0 ) ' l s i n e ~
-
s i n e SI
( 10)and
The c r o s s s e c t i o n s a r e i l l u s t r a t e d i n Figs. 1 and 2 which show t h e i n t e g r a t e d i n t e n - s i t i e s i n each case. As i s s e e n from eqn. (9) and Fig. 1, t h e c r o s s s e c t i o n f o r s c a t t e r i n g o f f t h e bending mode i s dominated by t h e s t r o n g s i n g u l a r i t y due t o t h e term ( s i n 0
-
i n t h e denominator, and i t i n c r e a s e s w i t h d e c r e a s i n g L.I
Both t h e s e f e a t u r e s stem from t h e Q ~ ~ L - ~ dependence of t h e power spectrum noted under eqn. ( 5 ) . The c r o s s s e c t i o n f o r s c a t t e r i n g o f f t h e l o n g i t u d i n a l mode, con- v e r s e l y , d e c r e a s e s w i t h d e c r e a s i n g L. The f a c t o r L i n eqn. (11) i s t h e product of t h e L-' shown i n eqn. (9) w i t h L2 due t o t h e conversion of t h e power spectrum from
Acknowledgements
We thank N. A. Clark, R. Loudon and J. F. S c o t t f o r h e l p f u l d i s c u s s i o n s , and t h e B r i t i s h Council, CNPq and UFRN f o r f i n a n c i a l support.
JOURNAL
DE PHYSIQUE
F i g . 1
-
I n t e g r a t e d i n t e n s i t y v e r s u s s c a t t e r i n g a n g l e €IS f o r B r i l l o u i n s c a t t e r i n g o f f t h e bending mode of a n unsupported f i l m w i t h o p t i c a l d i e l e c t r i c c o n s t a n t E = 1.5 a t a n g l e o f i n c i d e n c e '81 = a / 4 . The c u r v e s c o r r e s p o n d t o d i f f e r e n t v a l u e s of LwIfC:- - - 0 . 1 ; - . - . - .
0.2; - .. - .. -
0 . 3 ;- ... - ,.. 0 . 4 ;
- .... -
0 . 5 , t h e l a s t 3 b e i n g i n d i s t i n g u i s h a b l e o v e r p a r t of t h e range. The v e r t i c a l s c a l e i s l i n e a r .Fig. 2
-
As F i g . 1 f o r t h e l o n g i t u d i n a l mode.References
/1/ MEEKER T.R. and MEITZLER A.H., P h y s i c a l A c o u s t i c s I A (ed. W.P. MASON, pub.
Academic P r e s s , New York 1964) 112.
/2/ LANDAU L.D. and LIFSHITZ E.M., Theory o f E l a s t i c i t y (Pergamon, Oxford 1970).
/3/ AULD B.A., A c o u s t i c F i e l d s and Waves i n S o l i d s , Vol. I1 (John Wiley, London 1973).
/4/ BORTOLANI V., MARVIN A.M., NIZZOLI F. a n d SANTORO G . , J. Phys. C: S o l i d S t a t e Phys. l&( 1 9 8 3 ) 1 7 5 7 .
/ 5 / MARVIN A . , TOIGO F. a n d CELL1 V . , Phys. Rev. ( 1 9 7 5 ) , 2 7 7 7 .
/ 6 / ALBUQUERQUE E.L., J. Phys. C: S o l i d S t . Phys.