Effect of surface stresses on surface waves in elastic solids

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Sadhan& Vol. 22, Part 5, October 1997, pp. 659-670. © Printed in India. Effect of surface stresses on surface waves in elastic solids PRANABES KANTI PAL t, D ACHARYA 2 and P R SENGUPTA 3 1Indian Institute of Mechanics of Continua, 201, Manicktola Main Road, Flat no 42, Calcutta 700 054, India 2 Department of Mathematics, Mahadevananda College, Burrackpore 743 101, India 3 Department of Mathematics, University of Kalyani, Kalyani 741 235, India MS received 25 July 1996; revised 19 July 1997 Abstract. This paper deals with the propagation of surface waves in homo- geneous, elastic solid media whose free surfaces or interfaces of separation are capable of supporting their own stress fields. The general theory for the prop- agation of surface waves in a medium which supports surface stresses is first deduced, and then this theory is employed to investigate the particular cases of surface waves, viz. (a) Rayleigh waves, (b) Love waves and (c) Stoneley waves. It is seen that the Rayleigh waves become dispersive in nature; and, in case of low frequency with residual surface tension, a critical wavelength exists, below which the propagation of Rayleigh waves is not possible. This critical wave length is directly proportional to the surface tension. Some numerical calcu- lations have been made in the case of Love waves and conclusions have been drawn. Keywords. Surface waves; effect of surface stresses; Rayleigh waves; Love waves; Stoneley waves; residual stress. 1. Introduction Surface waves play an important role in the science of earthquakes. To match the ac- tual situation in a given problem, three types of surface waves are generally introduced which are classified according to their nature of displacements (Dey & Sengupta 1978; Chandrasekharaiah 1986; Das et al 1992; Pal et al 1996). Again it is known that the phys- ical properties of bodies in the neighbourhood of the surface are sensibly different from those in the interior. Thus the boundary surface may be regarded as a two-dimensional elastic continuum which adheres to the body without slipping (Gurtin & Murdoch 1976; Chandrasekharaiah 1987). Different authors (Plaster 1972; Chandrasekharaiah 1987) pre- sented their research papers including surface stresses as their subject of discussion. In the 659

Transcript of Effect of surface stresses on surface waves in elastic solids

Page 1: Effect of surface stresses on surface waves in elastic solids

Sadhan& Vol. 22, Part 5, October 1997, pp. 659-670. © Printed in India.

Effect of surface stresses on surface waves in elastic solids

PRANABES KANTI PAL t, D ACHARYA 2 and P R SENGUPTA 3

1 Indian Institute of Mechanics of Continua, 201, Manicktola Main Road, Flat no 42, Calcutta 700 054, India 2 Department of Mathematics, Mahadevananda College, Burrackpore 743 101, India 3 Department of Mathematics, University of Kalyani, Kalyani 741 235, India

MS received 25 July 1996; revised 19 July 1997

Abstract. This paper deals with the propagation of surface waves in homo- geneous, elastic solid media whose free surfaces or interfaces of separation are capable of supporting their own stress fields. The general theory for the prop- agation of surface waves in a medium which supports surface stresses is first deduced, and then this theory is employed to investigate the particular cases of surface waves, viz. (a) Rayleigh waves, (b) Love waves and (c) Stoneley waves. It is seen that the Rayleigh waves become dispersive in nature; and, in case of low frequency with residual surface tension, a critical wavelength exists, below which the propagation of Rayleigh waves is not possible. This critical wave length is directly proportional to the surface tension. Some numerical calcu- lations have been made in the case of Love waves and conclusions have been drawn.

Keywords. Surface waves; effect of surface stresses; Rayleigh waves; Love waves; Stoneley waves; residual stress.

1. Introduction

Surface waves play an important role in the science of earthquakes. To match the ac- tual situation in a given problem, three types of surface waves are generally introduced which are classified according to their nature of displacements (Dey & Sengupta 1978; Chandrasekharaiah 1986; Das et al 1992; Pal et al 1996). Again it is known that the phys- ical properties of bodies in the neighbourhood of the surface are sensibly different from those in the interior. Thus the boundary surface may be regarded as a two-dimensional elastic continuum which adheres to the body without slipping (Gurtin & Murdoch 1976; Chandrasekharaiah 1987). Different authors (Plaster 1972; Chandrasekharaiah 1987) pre- sented their research papers including surface stresses as their subject of discussion. In the

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present paper, following a theory of surface stresses, the authors investigate surface wave propagation. The Rayleigh wave velocity equation has been obtained as a particular case. Following Chandrasekharaiah (1987), the effect of surface stresses on Rayleigh wave prop- agation has been discussed. Next we discuss Love wave propagation with surface stress on its free boundry, with some numerical computations and conclusions. Wave velocity equation for Stoneley waves has also been deduced.

2. Basic equations

Let us consider two homogeneous, isotropic, elastic solid media M1 (lower medium) and M2 (upper medium) with different material constants. We also consider that a two- dimensional elastic layer is present at the surface of separation of the two media. We take an orthogonal cartesian frame of axes Oxlx2x3, 0 is taken on the interface and Ox3 is positive in the downward direction. As in Bullen & Bolt (1985), here also the wave travels in the Oxl direction. The disturbances of the particles on lines parallel to Ox2 vibrate in phase, which means all partial derivatives with respect to x2 are zero.

The equation of motion in the absence of body forces is

02u #V2U + ()v +/Z) grad div u = p a t 2 . (1)

In the above Navier's equation of classical elasticity u (Ul, u2, u3) is the displacement vector; Z , / , are Lam6 elastic constants; p is mass density and t represents time. To in- vestigate plane deformation parallel to the xlx3 plane we introduce the displacement potentials P, Q related to the displacement components u l(xl , x3, t) and u3 (xl, x3, t) by the equations,

OP OQ 8P OQ Ul - - OXl OX3 U3 = ~ + 8xl (2)

Introducing (2) in (1) we obtain,

(V 2 1 02 ) aZO~ P = 0 , (3)

(V 2 1 0 2 ) b2 ~-~. Q = 0, (4)

(V 2 1 a2 ) b2 Ot 2 u 2 = 0 , (5)

where a = ()~ + 21~/p) U2 and b = ( t , /p) U2 are velocities of dilatation and distortion respectively. Befitting the actual situation of the problem, we seek solutions to (3)-(5) as

[P, Q, uz] = [/3(x3), O(x3),/~2(x3)1 e i ( o x l - g t ) . (6)

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Eflect of su$ace stresses on su$ace waves in elastic solids

Inserting (6) in (3)-(5), we get

Now, P(x3), e(x3), i2(x3) describe surface waves and as such they must be vanishingly small as x3 -+ m. Hence the solution of (5) for the medium MI may be taken as

P = A l exp(-qmlx3)e i(w-51)

where 2 112 ml = (1 - r2)Il2, m2 = (1 - s ) ,

wavelength = 2n/q, wave velocity = < / q , < being a known constant while q is an unknown constant; and, A 1, A2, A3 are arbitrary constants.

Analogous solutions with primes (for the region 0 I x3 < -00) are

P' = A; exp(qm',x3) ei(qxl-ct).

Q' =; A; exp(qm:x3) ei(qxl-Cr'.

u; = A; exp(qrn;x3) ei(q"l-Ct),

are obtained for the upper medium M2 of the material, where 12 112 f 12 112 m ' , = ( l - r ) , m 2 = ( 1 - s ) ,

3. Boundary conditions and solutions

We assume that the plane x3 = 0 is a material layer which adheres, without slipping, to the lower medium and is a two-dimensional elastic continuum. This layer is capable of supporting its own stress represented by surface stress tensor Cia, and obeys the law (Chandrasekharaiah 1 987),

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Here ~-0, #0 are the Lam6 moduli of the material boundary and a is the residual surface tension on the layer x3 = 0. Following Gurtin & Murdoch (1976) we use the surface elasticity tensor. The forces on the bounding surface are governed by surface stress tensor Ei~. Given a smooth oriented curve y in x3 = 0 with positive unit normal n i , Y~4ct n~ is the force per unit length of y by that part of the boundary into which nc~ is directed, upon that part of x3 = 0 away from which n~ points. Dimensions of )~0,/-to, a are the same (N/m).

The boundary conditions are

02Ui t (i) z'i3 + Z - P 0 - - ~ - = ri3, on x3 = 0,

i~ ,o t

where P0 is the mass per unit surface area (kg m -2) of the layer (Gurtin & Murdoch 1976), and rij and r[j are the stress tensors in the interior of the media Ml and M 2 respectively. The conventional stress tensor ri3 has the unit of force per unit area and the new stress tensor ~--~ia has the unit of force per unit length. T, i j obeys the law (Gurtin & Murdoch 1976),

rij ---- )~6ijUk, k + #(Ui.j --}- Uj,i).

The boundary conditions are

2 02P °2Q #

\ ~xl Ox3 + Ox--~l

I ( 02Pr = # 2 - - + - -

OXl 6x3

02Q) [ 02 02 ox3 + (z0 + 2.0) - P ° T

02Q ' 02Q'~

(13)

02 Q 02P~ I z 02P 21~ \ Ox---~x 3 OX 2 ] + b--g Ot--- 5-

OP OQ) OXl OX3

+ -p0V

3 v .2

tO2U~

= # -~x~"

(14)

OP OQ OP I OQ'

OXl OX3 OXl OX3' 0P 0Q 0P I 0Q t _ _ + _ _ - _ _ + _ _ OX3 OXl OX 3 OX 1 '

I U 2 = U 2 .

(14a)

at all places and times. Therefore (ii) The displacement components must be continuous on the surface of separation x3 = 0

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Applying boundary conditions (14) and (14a) to (8) and (10) the following system of equations is obtained.

(2ml + t IF )AI - i ( 2 - s 2 + r tm2F)A2

+ 2/~'mlla ' 1 + i /z ' (2 - s '2)a~ = 0. (15)

( 2 - s 2 + t l m l H ) A 1 - i(2m2 + o H ) A 2 1 !

/2 (2 - s'2)a'l ' i2~--m~2a' 2 = O.

I • I I AI - intvA9 - A 1 - t m 2 A 2 = 0,

m l A 1 - i A 2 + m q Z ' 1 + i Z ~ = 0,

~O-poC 2+~m~ a~+ m~a;=o,

A3 - A; = 0,

where we have taken

1 --(Xo + 2go - poc 2) = F,

# (16) l

- - ( O -- p0 c 2 ) = H . #

The last two equations of (15) yield

I

A3 = A 3 = 0,

which implies that there is no propagation of displacement u2. Eliminating the constants A1, A2, A ' l, A ' 2 from (15) we obtain

A = det[aij] = O, i, j = 1 .2 ,3 , 4 , (17)

where

a 1 1 = 2 m 1 + 0 F , a12 = 2 - s2 + ~lm2 F, ! !

a13 = 2/zmll , a14 = # (2 -- s'2),

a e l = 2 - - s 2 + 0 m l H , a 2 2 = 2 m 2 + 0 H , 1

a23 = - -# (2 -- s'2), #

!

a24 = - -2# m~,

a31 = 1,a32 = m2, a33 = --l , a34 = --m~,

a41 = m 1, a42 = 1, a43 = m'l, a44 = 1.

Equation (17) represents the wave velocity dispersion equation for interface waves in elastic solid media under the influence of surface stresses, where the plane of separation

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X3 = 0 is a material boundary. The equation depends on the particular value of 0 which indicates dispersive nature caused by the presence of surface stresses. If the surface of separation is free of surface stresses, F = H = 0; and at once the classical equation of general surface waves is obtained from (17).

4. Part icu lar cases

4.1 Rayleigh waves

As a particular case of the general surface wave discussed in the previous article we may study Rayleigh waves under the influence of surface stresses in the light of the investigation done by Chandrasekharaiah (1987). Here the upper medium (/142) is replaced by vacuum. Applying the boundary conditions

02u 1 +

1~,~

02U3 333 + -po- =o,

3c~,c~

we get

(2ml + oF)A1 + ( 2 - s 2 + om2F)A2 = 0 ,

( 2 - s 2 + omlH)A1 + (2m2 + oH)A2 = 0 .

Eliminating the constants A 1, A2 the Rayleigh wave velocity equation may be obtained as

2 2 m l + o F 2 - s 2 + o m 2 H = 0 . - s 2 + om1H 2m2 + oH

The determinantal equation on simplification gives

(1 - m l m 2 ) F H o 2 + ( m l H + m 2 F ) s 2 0 + 4 m l r n 2 - ( 2 - s 2 ) 2 = O . (18)

This equation is in agreement with the corresponding equation obtained by Chandrasekhara- iah (1987) in the absence of voids. Again in the case of conventional stress-free boundary, (18) becomes

4mlm2 - (2 - s2) 2 = 0. (19)

When surface s t r e s se s Y~ia arise from surface tension, we have as a special case the conditions )~0 = #0 = Po = 0. In such a situation F = 0, H = a//z and hence the equation (18) becomes

0~rs2(1 - $ 2 r 2 ) 1/2 = / z [ ( 2 - $2) 2 - 4(1 - s 2 ) 1 / 2 ( 1 - $2r2)1/2 , ] , (20)

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where

r 2 = b2/a 2. (21)

This equation is in agreement with the corresponding equation obtained by Chandrasekharaiah (1987) in the absence of voids. In the absence of residual surface tension, we take ~r = 0 to obtain the classical Rayleigh wave velocity equation (19). In this case, (20) has one root s = so in the open interval (0, 1 ). If ~ ~ 0, (20) has a real root in the interval (so, 1), provided 0 < 0c where ~/c = /z/[a(1 - r2)1/2]. Again if r/ = ~/c we see that s = 1 is a root of (20). Lastly, the said equation has no real root if r/ > r/c. Thus we have a critical wavelength, Lc = 2rC/rlc, below which Rayleigh waves cannot propagate at all under the influence of surface stresses. The relation.

(/z/27r)Lc = ~r(1 - (b2/a2)) 1/2,

reveals that critical wavelength varies directly with residual surface tension which is a factor of surface stress,

4.2 Love waves

In order to consider Love waves we shall assume that the upper medium (M2) is of finite thickness H and the lower medium (M1) is semi-infinite. Let the origin O of the orthogonal cartesian frame Oxlx2x3 be on the interface, Oxl and Ox3 are along the interface and vertically downwards into Ml respectively. For Love wave propagation along xl axis (see figure 1 ),

U I = U 3 = 0 ,

u 2 = u 2 ( x l , x 3 , t).

Here equations of motion are

V 1 02 ) b2 at 2 u2=0,

V 1 0 2 ) b~ 20 t 2 u~=O.

(22)

x 2

0

/ B 2

B 1

I H

D x 1

×3 Figure 1. Love waves and their propagation.

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The solutions of (22) are

where

u2 = A1 exp(--t /m2x3)e i(oxl-~t), u~ = {a2 exp(-r/m~x3) + A3 exp(r/m~x3)} e i¢°xt-ft),

m 2 = ( 1 - -s2) 1/2,

' = (1 - St2) I/2, m 2 ~' C , C

C = - , s = ~ - , s b'

The boundary conditions are:

(23)

(24)

(i) u2 is continuous on the boundary surface of separation x3 = 0;

(ii) 1:23 is continuous on the boundary surface of separation x3 = 0;

(iii) since the boundary surface x3 = - H is free of external loads

we have (Gurtin & Murdoch 1974-75)

02u f t 2 for x3 = - H .

20~,~t

Applying the above boundary conditions to (23) and then eliminating the constants A l, A2, A3 we get the wave velocity equation for Love waves under the influence of surface

- 1 -1 I f f !

# m 2 --/z m 2

/ / , N m 2 , e ~mzH (N0 - p0c 2) e -°m2H 0

stresses in determinantal form as,

0{ /z m 2 1 ~m2

! f

+ (/-tO - - p0 c2) 7/

= 0 .

This determinantal equation on simplification gives

1

{(c/b') 2 - 1}1/2

{(c2/b t2) -- l }l/2{(#/p')[1 -- (c2/b2)]1/2 + (rl/#')(I-to -- p0c2)}]

× tan-1 ~ 2 ) ~ 1 ~ ~ (c2/b2)]1/2 : ~ ~ - - - - P O - - ~ J"

o H =

(25)

when the surface stress effect is neglected (/x0 = P0 = 0), (25) reduces to

1 r (#t/#){ 1 - - c2/b 2} I/2 ~IH = {(c2/b,2 ) _ 1}l/2 tan -1 L { ( - ~ ' ~ ~1-72 , (26)

which is the classical Love wave velocity equation. From (25) we observe that Love wave propagation is possible if

1 < (c /b t) < [ (# /p ) / ( l . f f /p ' ) ] 1/2. (27)

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Table 1. Values of oH.

c/b' r/ 1.048 1.096 1.144 1.192 1.240 1.288 1.336 1.384 1.432

1 6.933 4.081 2.858 2.147 1.671 1.325 1.057 0.838 0.648 2 7.444 4.576 3.333 2.602 2.104 1.733 1.439 1.193 0.973 3 7.623 4.757 3.517 2.788 2.291 1.922 1.628 1.381 1.159 0* 2.975 1.630 1.078 0.771 0.571 0.428 0.317 0.225 0.139

* Denotes the classical case where the surface stresses are not present

4.3 Numerical calculation of Love waves

For numerical calculations we take

Ix = 3.00 x 106N/cm 2, Ix' = 5.00 x 106N/cm 2, Ix0 = 6.47 × 106 N/cm,

p = 2.72 g /cm 3, p! = 9.89 g /cm 3, P0 = 3.40 g /cm 2.

Table 1 gives the values of 0H for different values of C/b' taking 0 = 1, 2, 3. It also gives the values of oH for different values of C/b t in the absence of surface stresses (denoted

by 0 in the first column).

We observe that the Love wave velocity equation is independent of ~r and depends solely upon Ix0 and P0. It is also observed that for a particular value of 77, wave velocity decreases with increase of 0H. Again for a particular wave velocity, 0H increases with increase of 0. For comparison we give the values of oH in table 1 for the classical case (denoted by 0) where the surface stresses are not present.

4.4 Stoneley waves

Stoneley waves are a generalized form of Rayleigh waves propagating along the common boundary of M1 and M2. Equation (17) represents the wave velocity equation for Stoneley waves in elastic media with surface stresses. This equation after a little manipulation may be obtained in the form

where

02CD(1 - ST)(1 - S!T ')

+s 2 (CT + DS)(1 - S'T') + ~---r (CT' + DS')(1 - ST) O - A(s) = 0, Ix

(28)

A(s) = ( 1 - SITI) { (2 - s2)2 - 4 S T - 411I(1- s 2 - ST)} #

{ ' ] + (1 - S T ) (2 - r ~ s 2 ) 2 - 4s'r' - 4 i x - ( 1 - r ~ s 2 - S'T') #

!

-- r2 s4 ~---(2 + ST' + S'T), (29) #

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and

s = c/b, C = a*/pb 2, or* = cr - po c2,

F* D -- F* = 1-" - poc 2, 1-" = ~.0 + 2#0,

pb 2'

S = (1 - $2) 1/2, T = (1 - Z'?S2) 1/2,

S' = (1 - z ' 2 s 2 ) 1 / 2 , T t = (1 - z ' 2 s 2 ) 1 / 2 .

rl = b/a, T2 = b/b f, r3 = b/a t. (30)

For the classical case, i.e., when surface stress is absent, we take a = F = P0 = 0, so that C = D = 0, (28) reduces to A(s) = 0 which is equivalent to the classical Stoneley wave velocity equation. It is observed that the Stoneley waves under the influence of

surface stress are dispersive in contrast with the classical situation for which waves of all

frequencies propagate uniformly at the same speed. The equation A(s) = 0 was solved numerically by Koppe (1948) who concluded that the velocity of the interface wave falls

between the values of the velocity of Rayleigh waves and of the transverse waves in the medium with greater acoustic density. Taking #I __+ 0 in (28) we get the Rayleigh wave velocity equation under the influence of surface stress as

r/2CD(1 - ST) + s2(CT + DS)rl - g(s) = 0, (32)

where

g(s) ---- (2 - s 2 ) - 4ST. (33)

This result is in agreement with the result obtained in (18) and also that by Murdoch (1976).

Further, when there is no surface stress, this equation reduces to the classical Rayleigh wave velocity equation g(s) = 0. This equation has one real root s = so, in the interval (0, 1). If s = s I satisfies the equation A(s) = 0, then so < sl < b× transverse wave velocity in the medium with greater acoustical density. From (28) when CD # 0 we have

#f ST)] rl= l - s 2 [(CT + D S ) ( 1 - S'T') + --f r2(CT' + DS')(1 -

-}- S 4 (CT + DS)(1 - S'T') + - - r 2 ( C T ' + DS')(1 - ST) #

-] 1/2 } + 4A(s)CD(m - ST)(m - S'T') I + {2CD(1 - ST)(1 - S'T')}.

(34)

If C = 0, i.e. in the absence of residual surface tension for a specific value of s we have from (28)

#r

#

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Effect of surface stresses on surface waves in elastic solids 669

Again when D = 0 i.e. in the absence of surface tension at some value of s we have

#

If both C and D vanish at some value s', we have A(s t) = 0 so that Stoneley waves exist. Otherwise there is no propagation of Stoneley waves. The case when ~, I" > p0b 2, C and D will remain positive in (0, l). Since 17 is positive, C < b, r l , r2, r3 < 1 we discard the solution of (34) which is negative for some s in (0, 1). Thus we see that Stoneley wave velocity under the influence of surface stresses may be less than or greater than the classical Stoneley wave velocity but always remains greater than the Rayleigh wave velocity. Moreover, in the case when 0 < ~r < F < pob ~, C and D will vanish exactly at one point {each on (0, 1)}, say s2 and s3 on (0, 1), so that s 2 = ~/po b2, s~ = I'/po b2 and hence 0 < s2 < s3 < 1, where C is positive on (0, Sl) and negative on (Sl, 1) and D is positive on (O, s2) and negative on (s2, 1) Again when ~r, F lie in (0, pob2), CT + DS and CT' + DS' vanish at say s4 and s5 in (s2, s3). We observe that CT + DS is positive on (0, s4) and negative on (s4, 1) while CT' + DS' is positive on (0, ss) and negative on (ss, 1). Thus the number of positive values of r/which satisfy (28) for a particular value of s depends upon the location of S l related to s2, s3, s4, and s5, as well as on the value of Q(s) and zeros of Q(s) where

{ ' Q(s) = s 4 (CT + DS)(I - S'T') + ~ r ~ ( c r ' + DS')(1 - ST)

+ 4 A ( s ) C D ( 1 - S T ) ( 1 - S ' T ' ) } . (37)

Further discussion in the light of Murdoch (1976) is not pursued in this paper due to its complicated nature and cumbersome calculation.

5. Conclusion

Stoneley waves under the influence of surface stresses may be discussed in a manner similar to Rayleigh waves. It is seen that the propagation of Stoneley waves under the influence of surface stresses is not always possible. Under certain restricted conditions such a propagation is possible. Moreover, Stoneley wave velocity under the influence of surface stresses may be less or greater than the classical Stoneley wave velocity, but always remains greater than the Rayleigh wave velocity. We point out here that Stoneley waves are dispersive in character in contrast with the classical situation. Rayleigh waves have been deduced as a particular case of Stoneley waves. In case of Love waves we have shown that the wave velocity equation does not depend on residual surface tension. Some numerical calculations highlight the effect of surface stresses on Love wave as described in the paper.

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