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Submitted on 1 Jan 1984

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BRILLOUIN SCATTERING AT INTERFACES AND LONGWAVELENGTH ACOUSTIC PHONONS

V. Bortolani, F. Nizzoli, G. Santoro

To cite this version:

V. Bortolani, F. Nizzoli, G. Santoro. BRILLOUIN SCATTERING AT INTERFACES AND LONG-

WAVELENGTH ACOUSTIC PHONONS. Journal de Physique Colloques, 1984, 45 (C5), pp.C5-45-

C5-53. �10.1051/jphyscol:1984505�. �jpa-00224113�

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JOURNAL DE PHYSIQUE

Colloque C5, supplgment au n04, Tome 45, avril 1984 page C5-45

BRILLOUIN SCATTERING A T INTERFACES AND LONGWAVELENGTH ACOUSTIC PHONONS

V . B o r t o l a n i , F. N i z z o l i and G. Santoro

Dipartimento di Fisica and GNSM-CNR, Universita di Modem, 41100 Modem, I t a l y

Resume

-

Nous pr@sentons l a theorie de l a diffusion Brillouin pour une i n t e r - face entre un milieu semi-infini e t un film. Suivant 1'6paisseurdu film e t l a nature des deux milieux, l a section efficace de diffusion presente d i f f e r e n t s aspects interessants. Dans l e s experiences de diffusion vers l ' a r r i G r e que nous considerons, on trouve des s t r u c t u r e s correspondant aux ondes de

Rayleigh, Sezawa e t Lamb, polariseesdans l e plan s a g i t t a l . En considerant des films transparents suffisamment epais, on peut obtenir des informations sur l e mode d ' i n t e r f a c e , ou onde de Stoneley. Ce mode donne l i e u & u n maximum dans l a

section e f f i c a c e Brillouin. Lorsque l l @ p a i s s e u r du film tend vers l ' i n f i n i , l e s modes de Lamb donnent l a densite d ' 6 t a t s du milieu support6 semi-infini.

Abstract

-

We present the theory of Brillouin scattering f o r an i n t e r f a c e com posed by a semiinfinite medium and a f i n i t e slab. According t o the thickness- of the s l a b and the nature of the two systems various i n t e r e s t i n g features a r e present in t h e scattering cross section. In backward s c a t t e r i n g experi- ments, t o which we r e f e r , a r e present s t r u c t u r e s corresponding t o the

Rayleigh, Sezawa and Lamb modes polarized in the s a g i t t a l plane. By conside- ring transparent thick films of s u f f i c i e n t l y high thickness i t i s possible t o obtain information on the i n t e r f a c e mode, the Stonely wave. This mode gives r i s e t o a maximum in the Brillouin cross section. In the l i m i t i n which the thickness of t h e s l a b goes t o i n f i n i t y , the Lamb modes give r i s e t o t h e densi- t y of s t a t e s of the supported semiinfinite medium.

1

-

INTRODUCTION

The study of surface excitations i n the longwavelength l i m i t i s becoming of considera ble i n t e r e s t i n connection with the developements of the experimental techniques. T h e ultrasonic measurements / I / allow t o investigate s i n g l e surface excitations by using an i n t e r d i g i t a l transducer technique. The Brillouin s c a t t e r i n g /2-4/ gives informa- tion on the phonon f i e l d in thermal equilibrium present a t the surface of a s o l i d . In the range of frequencies investigated by t h i s high-resolution technique (GHz re- gion) the scattering cross section e x i b i t s i n t e r e s t i n g features associated with surfa ce and bulk phonons. For a coated system, formed by a semiinfinite medium covered with a film of a d i f f e r e n t material, i t i s possible /5/ t o observe peaks associated with Rayleigh, Sezawa, Lamb and Love modes and, f o r a s u f f i c i e n t l y high thick film, the interface mode, the so called Stonely wave / 6 / .

In t h i s paper we study the properties of the Brillouin cross section of a coated sys- tem as a function of the thickness d of the film, in order t o investigate the r e l a t i - ve importance of these excitations. We review i n Sect. 2 the theory of surface Brillouin scattering f o r a supported film. The theory i s applied to systems of inte- r e s t and the calculations a r e presented and discussed in Sect. 3 f o r various thicknes ses of the film.

In the case of transparent films of s u f f i c i e n t l y high thickness we show t h a t i t i s possible t o detect with backward in-plane TM-TM Brillouin s c a t t e r i n g experiments the Stonely wave. For opaque coatings the Brillouin cross section i s dominated by the Rayleigh, Sezawa and Lamb waves and f o r high thickness of the film the Sezawa wave becomes the Stonely mode. In the l i m i t of the film thickness going t o i n f i n i t y , the contribution of the Lamb modes t o the cross section becomes t h a t of the continuum of mixed modes of the semiinfinite medium of film material.

Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphyscol:1984505

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C5-46 JOURNAL DE PHYSIQUE

2 - BRILLOUIN SCATTERING CROSS SECTION

I t has been previously shown /5,7-9/ t h a t t h e s u r f a c e B r i l l o u i n c r o s s s e c t i o n i s de- termined by two d i f f e r e n t s c a t t e r i n g mechanisms. The f i r s t one i s t h e e l a s t o - o p t i c coupling due t o t h e modulation of t h e d i e l e c t r i c t e n s o r caused by t h e thermally exci- t e d phonons p r e s e n t i n t h e medium. The second mechanism, t h e r i p p l e coupling, i s due t o t h e dynamical corrugation of t h e s u r f a c e t h a t a c t s a s a g r a t i n g w i t h r e s p e c t t o t h e incoming l i g h t . In order t o account f o r both i n t e r a c t i o n s , t h e d i e l e c t r i c t e n s o r i n t h e whole space can be w r i t t e n i n t h e form:

where f r e f e r s t o t h e f i l m , s t o t h e s u b s t r a t e and d i s t h e thickness of t h e f i l m . c m ( $ , z , t ) i s t h e dynamical corrugation of t h e s u r f a c e r e l a t i v e t o t h e medium m . E:

i s t h e r e l a t i v e d i e l e c t r i c c o n s t a n t and B ( z ) i s t h e usual s t e p f u n c t i o n .

By expanding t o f i r s t order i n t h e phonon displacement f i e l d t h e corrugation function cm becomes simply t h e normal component of t h e phonon f i e l d u:(d,z,t) and 61:@ can be w r i t t e n a s :

1

6c:D = - k:gyb{ +-

2 ax, ax

Y

km i s t h e e l a s t o - o p t i c t e n s o r of t h e medium m .

To determine t h e c r o s s s e c t i o n we solve p e r t u r b a t i v e l y t o f i r s t o r d e r i n t h e d i s p l a - cements t h e Maxwell equations together with E q . ( 1 ) i n t h e two media. We impose t h e a p p r o p r i a t e boundary conditions a t t h e two r i p p l e d s u r f a c e s z=O and z=d f o r t h e f i e l d s sketched i n Fig. 1 .

f i l m

s u b s t r a t e

Fig. 1 - Propagation vectors and a s s o c i a t e d EM f i e l d s f o r a r i p p l e d coated s u r f a c e . The f i e l d s BO, B 1 , B2, B3 and B4 a r e zeroth-order i n t h e displacements and s a t i s f y t h e Fresnel equations. B5, B6, B 7 , B8 and Bg a r e of f i r s t - o r d e r . B5 and B7 a r e r e l a - t i v e t o t h e p o l a r i z a t i o n c u r r e n t s due t o t h e modulation of t h e d i e l e c t r i c t e n s o r i n t h e two media. Bg i s t h e s c a t t e r e d f i e l d d e t e c t e d i n t h e experiments.

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The cross s e c t i o n i s given by t h e thermal average on t h e phonon f i e l d o f t h e normal component o f t h e Poynting v e c t o r o f the s c a t t e r e d f i e l d Bg d i v i d e d by the normal corn ponent o f t h e Poynting v e c t o r o f the i n c i d e n t f i e l d BO. The d e t a i l s o f t h e c a l c u l a - t i o n a r e given i n r e f . / 5 / . For t h e case o f TM-TM i n - p l a n e backward s c a t t e r i n g geomg t r y t h e cross s e c t i o n i s :

1

- - -hN( l a - w o I )

( w / c ) ~ C O S ~ x 2pS

1

w-W,

1

where:

N(R) i s the Bose occupation number, pS i s the mass d e n s i t y o f t h e substrate. w o and KO are the frequency and t h e l a t e r a l component o f the momentum o f t h e incoming l i g h t , w and K r e f e r t o t h e same q u a n t i t i e s f o r t h e s c a t t e r e d l i g h t . We have used t h e f o l l o - wing d e f i n i t i o n s :

p , qm, a', B', E', D a r e s i m i l a r l y d e f i n e d whithout t h e s u p e r s c r i p t "O".

I n t h e expression o f D (Eq. 4) i s contained t h e phonon displacement f i e l d o f t h e coated medium. I n o r d e r t o evaluate the displacements we consider a s e m i i n f i n i t e

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C5-48 J O U R N A L D E PHYSIQUE

medium i n t h e h a l f space z<O and t h e f i l m i n t h e r e g i o n O<z<d.

The equations o f motion i n t h e two media

,

i n t h e e l a s t i c approximation, are:

where cm i s the e l a s t i c tensor. The eigenvectors

Gm

can be w r i t t e n i n t h e Bloch form:

4

i s t h e l a t e r a l component o f t h e phonon momentum and q: i s t h e normal component. The

L

I;" a r e t h e p o l a r i z a t i o n vectors o f t h e two media.

The s e c u l a r problem reduces t o :

m m m

det

11

P~~~~~~ + CyaB69aq6

11

= O ( 7 )

where 6m=($,q;). By s o l v i n g Eq. ( 7 ) a t f i x e d R one o b t a i n e i t h e r r e a l o r complex q:, l a b e l l e d w i t h q:". The p o l a r i z a t i o n v e c t o r o f t h e coated system can be w r i t t e n as a l i n e a r combination o f "Bloch type1' s o l u t i o n s Eq. (6) r e t a i n i n g o n l y those q ; 9 b h i c h g i v e r i s e t o t r a v e l l i n g o r evanescent waves t o z+--. We w r i t e :

The index j l a b e l s t h e independent s o l u t i o n s o f Eq. (5) and t h e unknown c o e f f i c i e n t s a j can be determined by imposing t h e boundary c o n d i t i o n s a t t h e f r e e surface z=d:

m,X

and a t t h e i n t e r f a c e z=O:

According t o t h e frequency fi considered, t h e p o l a r i z a t i o n vectors Eq. (8) can repre- sent d i f f e r e n t modes.

For nodes p o l a r i z e d i n t h e s a g i t t a l plane,defined by t h e l a t e r a l component o f the wavevector and by t h e normal t o t h e surface, we have t h e Rayleigh wave decaying away from t h e surface, t h e Sezawa and Lamb modes which a r e l o c a l i z e d o n l y i n t h e s u b s t r a t e and t h e Stonely wave l o c a l i z e d a t t h e i n t e r f a c e and t h e mixed modes c o n t a i n i n g l o c a l i z e d and t r a v e l l i n g waves i n b o t h media and a l s o b u l k modes.

The Love modes, p o l a r i z e d normal t o t h e s a g i t t a l plane, do n o t e n t e r i n t h e TM-TM in-plane backward s c a t t e r i n g B r i l l o u i n cross s e c t i o n t h a t we are considering.

The amplitude o f t h e Rayleigh, Stonely and a p a r t i c u l a r Lamb mode as a,function o f z a r e presented i n F i g . 2 f o r t h e system N i on fused s i l i c a f o r d=20000 A.

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F i g . 2

-

A m p l i t u d e o f t h e t h e r m a l l y averaged normal component o f t h e phonon d i s p l a c e - ment as a f u n c t i o n o f z .

Heavy l i n e : A m p l i t u d e o f t h e R a y l e i g h wave L i g h t l i n e : A m p l i t u d e o f t h e S t o n e l y wave Dashed l i n e : Amplitude o f t h e t h i r d Lamb wave 3

-

CALCULATIONS AND DISCUSSION

I n t h i s s e c t i o n we a p p l y t h e t h e o r y t o t h e case o f an i n t e r f a c e between an opaque and a t r a n s p a r e n t m a t e r i a l . F o r s m a l l t h i c k n e s s d o f t h e f i l m , t h e shape o f t h e spectrum i s r e l a t e d t o t h e i n t e r f e r e n c e between t h e r i p p l e and e l a s t o - o p t i c c o u p l i n g s i n t h e two media and can g i v e u s e f u l i n f o r m a t i o n on t h e components o f t h e e l a s t o - o p t i c t e n s o r o f t h e s u p p o r t e d f i l m .

T h i s i s t h e case,of t h e i n t e r f a c e Au-Si. I n F i g . 3 a r e r e p o r t e d t h e e x p e r i m e n t a l d a t a /11/ f o r d=1500 A. V a r i o u s peaks a r e p r e s e n t due t o R a y l e i g h , Sezawa and Lamb modes.

The r e l a t i v e h e i g h t o f t h e s e peaks i s r e l a t e d t o t h e d i e l e c t r i c and e l a s t o - o p t i c p r o p e r t i e s o f t h e two media. By knowning t h e e l a s t o - o p t i c p r o p e r t i e s o f t h e s u b s t r a - t e i n t h e f r e q u e n c y range o f v i s i b l e l i g h t i t i s p o s s i b l e w i t h Eqs. ( 3 ) and ( 4 ) t o p e r f o r m a b e s t f i t t o t h e e x p e r i m e n t a l d a t a . I n t h i s manner one o b t a i n t h e e l a s t o - o p t i c t e n s o r o f Au i n t h i s f r e q u e n c y range where t h e s t a n d a r d t e c h n i q u e s a r e n o t a p p l i c a b l e . The c a l c u l a t e d v a l u e s a r e :

W i t h these v a l u e s , t h e c r o s s s e c t i o n ( f u l l l i n e i n F i g . 3) i s i n q u a n t i t a t i v e agreement w i t h t h e e x p e r i m e n t a l d t a o v e r t h e whole f r e q u e n c y range.

The sane c a l c u l a t i o n s f o r d=1000

1

a r e r e p o r t e d i n F i g . 1 and compared w i t h e x p e r i - ments.

F o r t h i s system, i t i s n o t p o s s i b l e t o d e t e c t t h e S t o n e l y wave because t h e e l a s t i c c o n s t a n t s o f t h e two media do n o t f u l f i l l t h e e x i s t e n c e c o n d i t i o n /12/ f o r t h i s wave.

We pass now t o c o n s i d e r t h e system N i - f u s e d s i l i c a where t h e S t o n e l y wave e x i s t s . F i r s t o f a l l we s t u d y t h e case o f a f i l m o f f u s e d s i l i c a on a p o l y c r i s t a l l i n e N i s u b s t r a t e .

I n F i g . 5 i s drawn t h e d i s p e r s i o n o f t h e v e l o c i t y o f t h e s u r f a c e mode as a f u n c t i o n o f t h e t h i c k n e s s d. F o r s m a l l d, t h e v e l o c i t y o f t h e l o c a l i z e d mode appraches t h e v e l o c i t y o f t h e R a y l e i g h wave o f c l e a n N i , f o r d>2000

a

t h e l o c a l i z e d mode becomes t h e S t o n e l y wave o f t h e system. I n f a c t f o r s m a l l d t h e mode i s m a i n l y l o c a l i z e d a t

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JOURNAL DE PHYSIQUE

Fig. 3 - B r i l l o u i n s c a t t e r i n g c r o s s s e c t i o n of Au on S i . Dots r e p r e s e n t t h e experi- mental d a t a of Sandercock ( p r i v a t e communication and paper a t t h i s onference). The experiments where performed w i t h a l a s e r beam of wavelength h=5l45

1

and t h e inciden- ce angle was =70°. The c a l c u l a t i o n s a r e represented by t h e continuous l i n e . The dashed l i n e i s r e l a t e d t o t h e r i p p l e c a l c u l a t i o n .

Fig. 4 - Caption a s i n Fig. 3

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t h e f r e e s u r f a c e of s i l i c a and has a small secondary maximum a t t h e i n t e r f a c e . By increasing d, t h e l o c a l i z a t i o n decreases a t t h e s u r f a c e and i n c r e a s e s a t t h e i n t e r - f a c e .

Fig. 5 - Velocity of t h e s u r f a c e wave f o r Si02 on Ni a s a f u n c t i o n of t h e Si02 f i l m thickness d. vs i s t h e v e l o c i t y of t h e Stonely wave. The two l i g h t horizontal l i n e s r e p r e s e n t t h e shear v e l o c i t i e s of N i and Si02.

The evaluated c r o s s s e c t i o n s f o r d=500

1

and D=5000

8

a r e drawn i n Fig. 6 t o g e t h e r with t h e c r o s s s e c t i o n of clean s i l i c a .

Fig. 6

-

B r i l l o u i n s c a t t e r i n g c r o ~ s ~ s e c t i o n f o r s i l i c a on n i c k e l . Heavy l i n e : c a l c u l a t i o n f o r d=500 A.

Light l i n e : c a l c u l a t i o n f o r d=5000 A Dashed l i n e : c a l c u l a t i o n f o r clean s i l i c a

In both cases t h e c r o s s s e c t i o n i s dominated by t h e e l a s t o - o p t i c coupling i n t h e f i l m and t h e r i p p l e a t t h e i n t e r f a c e . We have neglected i n t h e c a l c u l a t i o n t h e e l a s t o - o p t i c couplin9 i n t h e Ni s u b s t r a t e because t h e very small p e n e t r a t i o n depth

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C5-52 JOURNAL DE PHYSIQUE

o f t h e l i g h t i n t h i s medium.

One observesa peak associated w i t h a l o c a l i z e d mode and a continuum o f mixed and b u l k modes. For d=500

fi

t h e peak i s due t o t h e Rayleigh wave w h i l e f o r d=5000 A i t i s associated w i t h t h e Stonely wave. Even f o r very l a r g e d t h e cross s e c t i o n o f t h i s system r e m a i n s d i s t i n c t from t h e Si02 cross s e c t i o n because o f the d i f f e r e n t boundary c o n d i t i o n s o f t h e two systems.

F i g . 7

-

D i s p e r s i o n o f t h e v e l o c i t i e s o f t h e l o c a l i z e d modes f o r the system Ni on s i l i c a as a f u n c t i o n o f t h e Ni f i l m thickness. H o r i z o n t a l l i n e s as i n Fig. 5. The dashed curves a r e resonances associated w i t h t h e Sezawa and Lamb modes.

Fig. 8

-

B r i l l o u i n s c a t t e r i n g cross 2 e c t i o n f o r N i on Si02 L i g h t l i n e : c a l c u l a t i o n f o r d=5000 A

Heavy l i n e : c a l c u l a t i o n f o r d=10000

1

Dashed l i n e : c a l c u l a t i o n f o r clean Ni

The system N i on fused s i l i c a i s a l s o o f i n t e r e s t . I n t h i s case t h e main s c a t t e r i n g mechanism i s t h e r i p p l e a t t h e f i l m surface. As i t can be seen from F i g . 7 t h e r e a r e many l o c a l i z e d modes and resonances. The lowest mode i s t h e Rayleigh wave o f t h e system. For small d i t s v e l o c i t y approaches t h e Rayleigh wave o f clean s i l i c a and

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f o r f a r e d becomes t h a t of pure nickel. The second localized mode, resonant f o r d<1900

!

i s the Sezawa wave. This mode becomes the Stonely wave f o r 6,7500

8;

The

other localized modes a r e the Lamb waves of t h i s system. Their number increases as the thickness of the film increases.

The crogs sections f o r two d i f f e r e n t values of d a r e presented i n Fig. 8. For d=5000 A ( l i g h t l i n e ) i s present the Rayleigh peak, the small shoulder on the r i g h t of i t related t o the Sezawa wave and the other maxima associated with the f i r s t Lamb mode and t o t h e otber resonant Lamb modes.

In the case of d=10000 A the number of o s c i l l a t i o n s i n t h e cross section increases, t h e i r amplitude decreases and t h e cross section approaches t h a t of clean Ni (dashed l i n e i n Fig. 8 ) . We notice t h a t f o r t h i s system t h e Stonely wave does notproduce any s i g n i f i c a n t structure in the Brillouin cross section. This i s due t o the small ampli- tude of the ripple a t the film surface caused by the Stonely wave.

In conclusion we have shown t h a t the Brillouin s c a t t e r i n g can be conveniently used i n studying the i n t e r f a c e modesof supported transparent films.

ACKNOWLEDGFIENTS

We l i k e t o thank J.R.Sandercock f o r useful discussions and f o r making available t o us his preliminary unpublished measurements f o r the Au-Si system.

REFERENCES

1

-

AULD B.A., "Acoustic f i e l d s and waves in solids" vol . I 1 (New York: Wiley- Interscience 1973)

2

-

SANDERCOCK J.R., Solid S t a t e Commun. 26 (1978) 547

3

-

HARTLEY R.T. and FLEURY P . A . , 3.Phys.T: Solid S t a t e Phys.

12

(1979) L863 4

-

MISHRA S. and BRAY R . , Phys.Rev.Lett. 39 (1977) 222

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BORTOLANI V . , MARVIN M . , NIZZOLI F. anTSANTOR0 G . , J.Phys. C: Solid S t a t e Phys.

16 (1983) 1757

6

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mRNELL G.W. and ADLER E.L., Physical Acoustic Principle and Methods vol. 9 ed.

MASON W.P. and THURSTON R.N. (New York: Academic Press 1972) p.35 7

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SUBBASWAMY K . R . and MARADUDIN A . A . , Phys.Rev. B18 (1978) 4181 8

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ROWELL N.L. and STEGEMAN G . I . , Phys.Rev. B18 ( m 8 ) 2598 9

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LOUDON R . , J.Phys. C: Solid S t a t e Phys. lTTl978) 2623

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BORTOLANI V . , NIZZOLI F . , SANTORO G . andTANDERCOCK J .I?.

,

Phys.Rev. B25 (1982)

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12

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DJAFARI-ROUHANI B . , DOBRZYNSKI L. and MASRI P . , Ann.Phys. FR - 6 (1981) 859

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