• Nenhum resultado encontrado

Lat. Am. j. solids struct. vol.11 número12

N/A
N/A
Protected

Academic year: 2018

Share "Lat. Am. j. solids struct. vol.11 número12"

Copied!
30
0
0

Texto

(1)

Abstract

The paper concentrates on the study of reflection and transmission characteristics of waves at the interface of a thermoelastic-diffusive solid half-space underlying an inviscid liquid. The analytic expressions for amplitude ratios, reflection and transmission coefficients, in terms of incident angles and material parameters have been obtained for quasi-longitudinal (

qP

) and quasi-transverse (

qSV

) wave incidence. The normal and grazing incidence cases have also been derived and discussed. The total reflection phenomenon has also been discussed. The energy law has been shown to be obeyed by the incidence, reflected and transmitted waves by deriving energy equation and its simulation. The numerical computations of reflection and transmission coefficients have been carried out for copper material half-space in contact with water at the interface by using MATLAB software. The computer simulated results have been presented graphically in order to bring out clear comparison of various situations.

Keywords

Thermoelastic Diffusion, Inviscid fluid, Reflection, Transmission, Energy Ratios, Critical angle.

Study of reflection and transmission of plane waves

at thermoelastic-diffusive solid/liquid interface

1 INTRODUCTION

Diffusion is defined as a movement of the particles from a region of high concentration to the low concentration. Thermal diffusion utilizes the transfer of heat across a thin liquid or gas to accomplish isotope separation. Today, the study of thermal diffusion phenomenon got a great deal of interest due to its wide ranging applications in geophysics and industrial applications. The concentration obeys the famous Fick’s law, which does not take into consideration the mutual interaction between the solvent and the solute or the effect of temperature on this interaction.

J.N. Sharma a R. Kaur b

Department of Mathematics, National Institute of Technology

Hamirpur-177005, India a

jnsnith@gmail.com         b

kaur.rajbir22@gmail.com 

(2)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

However, there is a certain degree of coupling with temperature and temperature gradients as temperature speeds up the diffusion process. The thermo-diffusion in elastic solids is due to coupling of temperature, mass diffusion and strain fields addition to heat and mass exchange with the environment. Nowacki (1974, 1976) developed the theory of coupled thermoelastic diffusion. The recent development of generalized theory of thermoelastic diffusion by Sherief et al. (2004) allows the finite speed of propagation of thermo-diffusive waves. Sharma (2007) discussed the propagation of plane harmonic waves in generalized thermo-elasto-diffusive solid. Kumar et al. (2014) studied the propagation of Rayleigh waves in a homogeneous isotropic micro-stretch generalized thermoelastic diffusion solid half-space.

The phenomenon of wave reflection and refraction is a fundamental topic in many fields such as seismology, geophysics, earthquake engineering, non-destructive evaluation, etc. Jeffreys (1930) and Gutenberg (1944) considered the reflection of elastic plane waves at a solid half space. Knott (1899) derived the general equations for reflection and refraction of waves at plane boundaries. Singh (2005) discussed the reflection of

P

and

SV

waves from the free surface of an elastic solid with generalized thermo-diffusion. Singh (2006) studied the reflection of SV waves from the free surface of an elastic solid in generalized thermo-elastic diffusion. Sharma and Sharma (2010) investigated the reflection characteristics of acousto-diffusive waves from the surface of a semiconductor half-space which is subjected to stress free, isoconcentrated and stress free, impermeable conditions. Kumar and Kansal (2012) considered the reflection and refraction of plane waves at the interface of an elastic solid space and a thermoelastic diffusive solid half-space. Bijarnia and Singh (2012) investigated the propagation of plane waves in a transversely isotropic generalized thermoelastic solid half-space with diffusion and they also studied the reflection of these plane waves from a thermally insulated free surface. Kumar et al. (2013) studied the reflection and refraction phenomenon due to plane wave’s incident obliquely at a plane interface between uniform elastic solid half-space and microstretch thermoelastic diffusion solid half-space.

(3)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

underlying an inviscid liquid. Sharma and Bhargava (2014) investigated the reflection and transmission of thermoelastic plane waves at an imperfect interface between a thermal conducting viscous-liquid and generalized thermoelastic solid half-space. Sharma, et al. (2008) studied the generalized Rayleigh waves in thermoelastic solids under viscous fluid loading.

Keeping in view the above state facts and applications of reflection/transmission phenomenon in thermoelastic-diffusive solid under the interaction of fluid, the present paper is devoted to discuss the reflection and transmission of plane waves at the interface between such continua. The effects of incident angles, material parameters and fluid loading on reflection and transmission coefficients of various possible waves due to the incident

qP

and

qSV

waves have been considered. The analytical results so obtained have been verified numerically and are illustrated graphically.

2 FORMULATION OF THE PROBLEM

We consider a homogeneous isotropic, thermoelastic-diffusive solid in the undeformed state initially at uniform temperature

T

0, underlying an inviscid liquid half-space. We take origin of the rectangular Cartesian co-ordinate system

Oxyz

at any point on the plane surface (interface) with

z

-axis directed normally into the solid half-space, which is thus represented by

z

0

as shown in Figure 1. We choose the x-axis along the direction of propagation of waves in such a way that all the particles on the line parallel to the y-axis are equally displaced. Therefore, all the field quantities are independent of

y

-co-ordinate. Further, the disturbances are assumed to be confined to the neighborhood of the interface

z

0

and hence vanish as

z

.

Liquid

Solid

Figure 1: Geometry of the problem.

1

2

3

4

5

qP or qSV  (incident) 

qSV (reflected)

T‐mode (reflected) qP (reflected) qP (transmitted) 

X

(4)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

The basic governing field equations of motion, heat conduction equation, mass equation and constitutive relations for a solid medium, in the absence of heat sources and body forces, are given by Sherief et al. (2004)

u

C

T

u

u



2



1

2

)

(

(1)

0

)

(

)

.(

)

(

0 1 0 0 0 0

2

T

C

T

t

T

T

u

t

u

aT

C

t

C

K

e









(2)

0

)

.

(

)

(

1

2 2 2

1

2

T

b

a

u

b

C

t

C

Db

C



(3)

ij ij

ij ij

kk

ij

e

e

T

C

2

1

2 (4)

3

,

2

,

1

,

,

,

2

e

bC

aT

i

j

k

P

kk (5) where

1

(

3

2

)

T,

2

(

3

2

)

C,

Here

u

(

x

,

y

,

z

,

t

)

(

u

,

v

,

w

)

,

T

(

x

,

y

,

z

,

t

)

and

C x y z t

( , , , )

are the displacement vector, temperature change and mass concentration respectively. Here

T,

C are coefficients of linear

thermal expansion and linear diffusion expansion;

,

are Lame’s parameters;

is the mass density;

K

is the thermal conductivity;

D

is the mass diffusion coefficient;

a

and

b

are thermo-diffusive and thermo-diffusive constants;

t

0 and

t

1 are thermal and mass flux relaxation times and

C

e is

the specific heat at constant strain. The quantity

ij is the Kronecker’s delta with

j

1

for Lord

and Shulman (LS) theory (1967) and

j

2

for Green and Lindsay (GL) theory (1972). The superposed dot notation is used for time differentiation.

The basic governing equations for inviscid fluid (liquid) medium are given by

L L L L L

L

u

T

u





(6)

L V L

L

L

u

C

T

T

0

.

  

(7)

where

L

3

L

;

L is the bulk modulus;

L and

 are the density and coefficient of volume thermal expansion;

u

L

(

u

L

,

0

,

w

L

)

is the velocity vector and

T

L is the temperature deviation in the liquid temperature from its ambient temperature

T

0.

In order to facilitate the analysis, we define the following dimensionless quantities

,

,

,

,

,

,

0 0

0 1

1

T

T

C

C

T

T

t

c

z

Z

c

x

X

L

L

(5)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

,

,

,

,

0 1 1 0 1 1 0 1 1 0 1 1

T

w

c

W

T

u

c

U

T

w

c

W

T

u

c

U

L L L L









   

(8)

,

,

,

,

,

0 0 1 1

2 1 2 2 2 1 2 2 2 0 1

t

t

c

c

c

c

T

L L ij ij  

,

,

)

2

(

,

)

2

(

0 2 2 2 0 2 1 L V L L L C e T

c

T

b

C

T

1 0 1 0 2 0 0

0

,

,

,

 

L e

T

C

C

b

aT

b

C

aC

a

where L L L b

e

c

c

c

Db

c

w

K

C

2

2

2 2

1 2

1

,

2

,

,

~

,

)

2

(

.

Here

 is the characteristic frequency,

Tand

C are thermo-mechanical coupling constant and mass concentration of the solid respectively,

c

1

,

c

2 are respectively the longitudinal and

shear wave velocities in the solid half-space,

L is the thermomechanical coupling and

c

L is the

velocity of sound in the fluid.

Upon using quantities (8) in equations (1)-(7), we obtain

U

U

U





2

(

1

2

)

(9)

0

)

(

)

(

)

(

0 0 0

2



T

U



U



a



(10)

0

)

(

)

(

~

2 2

1

2

w

b c

U

b



(11) ij ij i j j i ij

ij

U

U

U



(

1

2

2

)

2

(

,

,

)

(12)

U

b

P

C

ij

(13)

L L L

L

U

U



(6)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

where

L and the operator

and

2

are again designated to have their usual meaning in

the changed variables

The scalar point potential functions

and

L and vector point potential functions

and

L have been defined through the relations given below:

0

.

,

U

0

.

,

L L L

L

U

(16)

where

U

(

U

,

0

,

W

)

,

U

L

(

U

L

,

0

,

W

)

In case

(

0

,

,

0

)

and

L

(

0

,

L

,

0

)

, the above equations provide us

Z X

U

,

,

,

W

,

Z

,

X

X L L

U

,

,

W

L

L

,

Z (17)

Upon introducing expressions (17) in equations (9)-(15), and noting that

L

0

for inviscid fluid, one obtains

2



2

1

(18)



2

(19)

0

)

(

)

(

)

(

0 0

2 0

2



T



a



(20)

0

)

(

~

4 2

1

2

w

b



C

b

(21)

0

)

1

(

2

2

L L

L

L



(22)

L L L

L



)

1

(

(23)

The equation (18) corresponds to decoupled shear motion which remains independent of temperature and mass concentration changes.

3 BOUNDARY CONDITIONS

The boundary conditions to be satisfied at the solid-liquid interface (

Z

0

) are given by

p

ZZ

,

XZ

0

,

W

W

L (24)

0

)

(

,

Z

h

L (25)

0

,z

(26)

(7)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

where

h

is Biot's constant,

h

0

corresponds to the thermally insulated boundary and

h

refers to the isothermal one and the pressure (

p

) of the liquid is given

by

p

L

L





2

4 SOLUTION OF THE PROBLEM

We assume wave solutions of the form

)}

cos

sin

(

exp{

}

,

,

,

,

{

}

,

,

,

,

{

L

A

B

C

D

E

ik

X

Z

c

(27)

where





1

c

c

c

,

 

,

 

1

c

k

k

are the non-dimensional phase velocity, frequency

and wave number of waves respectively. The primes have been suppressed for convenience. Upon using solution (27) in equations (18)-(23), one obtains a system of algebraic equations in unknowns A, B, C, D and E. The condition for the existence of non-trivial solution of this system of equations on simplification, provides us

)

5

,

4

,

3

,

2

,

1

(

2 2

2

j

a

k

j j

(28)

where

)

1

/(

)

)(

1

(

)

1

)(

1

[(

~

1

1 0

2

1

w

b

a

b

a

b

T a C

a

(29)

)

1

/(

)]

1

(

1

[

~

)

1

(

1 0

0 2 2 2

1

a

a

b

w

b T C

a

)

1

/(

~

1 0 2 3 2 2 2

1

a

a

w

b C

a

2 2 4

1

a

,

)

1

(

1

2 2 5

L L

a

1 0 0

i

, 1

1 1

i

,

a

C

b

In the absence of mass diffusion

a

0

2, the quantities

a

i2

(

i

1

,

2

,

3

,

4

,

5

)

defined in equation

(29) become

0 2 3 2 1 0

2 3 2 1 1 2

2

,

1

(

1

)

,

~

w

a

a

a

a

a

b T , 2

2 4

1

a

,

)

1

(

1

2 2 5

L L

a

(30)

(8)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170 0 2 3 1 2 2 2 1

,

~

,

1

a

w

a

a

b , 2 2

4

1

a

, 52 2

1

L

a

(31)

The equation (30) and (31) will be used for reductions in the following analysis.

5 REFLECTION AND TRANSMISSION AT SOLID-LIQUID INTERFACE

In this section we shall discuss reflection and transmission of waves at the interface of thermo-elasto-diffusive solid and inviscid fluid for

qP

-wave and

qSV

-wave incidence cases.

5.1. Quasi longitudinal

(

qP

)

-wave incidence

Suppose that a

qP

-wave is incident at the interface from the solid half-space. Then the total wave fields after reflection and transmission of waves from the interface are given by

)

exp(

)}

cos

sin

(

exp{

)}

cos

sin

(

exp{

3 1 1 1



i

Z

X

ik

A

Z

X

ik

A

j j j j rj i r i

 (32)

exp{

4

(

sin

4

cos

4

)}

exp(

)

4



r

A

r

ik

X

Z

i

(33)

)

exp(

)}

cos

sin

(

exp{

)}

cos

sin

(

exp{

3 1 1 1 1



i

Z

X

ik

A

S

Z

X

ik

A

S

j j j j r j i r i j

 (34)

)

exp(

)}

cos

sin

(

exp{

)}

cos

sin

(

exp{

3 1 1 1 1



i

Z

X

ik

A

V

Z

X

ik

A

V

j j j j r j i r i j

 (35)

5

exp{

5

(

sin

5

cos

5

)}

exp(



)

Lt

A

ik

X

Z

i

(36)

S

L

A

5

exp{

ik

5

(

X

sin

5

Z

cos

5

)}

exp(

i



)

Lt

(37)

where

S

j

S

j

2

,

V

j

V

j

2

,

S

L

S

L

2

)

1

(

2j

j

j

V

a

(9)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

)

1

(

L

L L

S

3

,

2

,

1

],

)

1

[(

/

]

)

1

(

1

[

2 2 1

2

b

a

a

b

a

w

j

V

j j

a j

j

b (38)

In the absence of mass diffusion(

a

0

2), we have

2

,

1

3

,

1

,

0

j

j

V

j ,



2

,

0

3

,

1

),

1

(

2

j

j

a

S

j j (39)

In the absence of mass diffusion and thermal variations

(

a

0

2

,

T

0

)

, we have

2

,

1

3

,

1

,

0

j

j

V

j ,

2

,

1

,

0

3

),

1

(

0

j

j

S

j

(40)

Upon using equations (32)-(37) and employing the boundary conditions (24)-(26), one obtains a system of five coupled algebraic equations (A.1)-(A.5) given in the Appendix.

Since all the waves, incident, reflected or transmitted must be in phase at the interface

Z

0

for all values of

X

and

, therefore the equations (A.1)-(A.5), lead to

sin

1

k

k

1

sin

1

k

2

sin

2

k

3

sin

3

k

4

sin

4

k

5

sin

5 (41)

The equation (41) with the help of equation (28) implies that

sin

1

a

a

1

sin

1

a

2

sin

2

a

3

sin

3

a

4

sin

4

a

5

sin

5 (42)

This is the modified form of the Snell’s law, which in the absence of thermal, mass diffusion, viscosity and fluid fields

(

0

,

L

0

L

,

a

0

2

,

L

0

)

, becomes

4 1

sin

sin

This implies that

2 4 1

1

sin

sin

c

c

(43)

(10)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

The system of equations (A.1)-(A.5) with the help of equation (41) can be expressed as

B

AZ

p

(44) where

A

,

Z

p and

B

are defined in the Appendix.

Solving the system of equations (44), the amplitude ratios

R

kqP

(

k

1

,

2

,

3

,

4

)

and

qP

T

1 are obtained as

1

1

qP

R

,

2

2

qP

R

,

3

3

qP

R

,

4 4

qP

R

,

5

1

qP

T

(45)

where

A

has been defined in equation (A.9) of Appendix and

i

(

i

1

,

2

,

3

,

4

,

5

)

can be obtained from

by replacing first, second, third, fourth and fifth column by

51 1 41 1 31 21

11

a

a

S

a

V

a

a

, respectively.

For the normal

(

0

0

1

5

)

and grazing

(

90

0

1

)

incidence, the relation (45) reduces to

1

1

qP

R

,

2

2

qP

R

,

3

3

qP

R

,

4 4

qP

R

,

5

1

qP

T

and

1

1

qP

R

,

R

qP

R

qP

R

qP

T

qP

1 4 3

2

0

(46)

respectively. The quantities

 and

i

(

i

1

,

2

,

3

,

4

,

5

)

have been defined in equation (A.9) of Appendix.

Thus for the grazing incidence, the reflected

qP

wave annihilates the incident

qP

wave and there is no reflection or transmission of other waves through the interface.

In the absence of mass diffusion

(

a

0

2

)

, the non vanishing amplitude ratios are

ˆ

ˆ

1 1

qP

R

,

ˆ

ˆ

2 3

qP

R

,

ˆ

ˆ

3 4

qP

R

,

ˆ

ˆ

4 1

qP

T

(47)

Here the quantities

ˆ

,

ˆ

i

(

i

1

,

2

,

3

,

4

)

are defined by equation (A.9) in the Appendix.

In the absence of mass diffusion and thermal fields

(

a

0

2

,

T

0

)

, the non vanishing amplitude ratios at normal

(

0

0

1

)

and grazing

(

90

0

1

)

incidence of

qP

wave, are given by

1 1 1

c

c

c

c

R

L L

L L qP

, qP qP

R

R

3

0

4 ,

1 1

2

c

c

c

T

L L

L qP

(11)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

1

1

qP

R

, qP qP qP

T

R

R

3

4

0

1

(48)

respectively. The relations (48) are in complete agreement with the corresponding equations of Achenbach (1973). Clearly

qP

wave is reflected as well as transmitted in case of normal incidence, however, for grazing incidence the reflected

qP

-wave annihilates the incident one.

5.1.1 Quasi longitudinal

(

qP

)

-wave incidence at free surface

In case the liquid media is absent

(

L

0

)

, the amplitude ratios for stress free, insulated and stress free, isothermal thermoelastic half-space are, respectively, given by

L

qP

S

i

a

a

a

R

3 3 3 11 24

1

cos

2

1

L

qP

S

i

a

a

a

R

1 1 1 11 24 3

cos

2

(49)

L

qP

a

i

S

a

a

a

S

a

a

a

R

2

11

{

1 1

cos

1 41 23 3 3

cos

3 43 21

}

4

and

L

qP

S

a

a

a

a

S

a

a

R

1 13 24 23 14 3 11 24

1

)

(

2

1

L

qP

S

a

a

R

1 21 14

3

2

(50)

L

qP

S

a

a

S

a

a

R

4

2

1 21 13 3 11 21

where

)

(

cos

)

(

cos

1 13 24 23 14 3 3 3 11 24 21 14

1

1

i

a

a

a

a

a

S

i

a

a

a

a

a

S

L

(51)

)

(

)

(

13 24 23 14 3 11 24 21 14

1

a

a

a

a

S

a

a

a

a

S

L

(52)

In the absence of mass diffusion, fluid and thermal fields

(

a

0

2

,

T

0

L

)

, the non-vanishing amplitude ratios are

4 2 4 1

2

4 2 4 1

2 1

2

cos

2

sin

2

sin

2

cos

2

sin

2

sin

qP

(12)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

4 2 4 1

2

4 1

2 4

2

cos

2

sin

2

sin

2

cos

2

sin

2

qP

R

(53)

Relations (53) are in complete agreement with the corresponding equations as in Achenbach (1973). In case of both normal

(

0

0

1

)

and grazing

(

90

0

1

)

incidence, the relations (53) provide us

1

1

qP

R

,

R

4qP

0

(54) Thus, the incident

qP

-wave is reflected as

qP

-wave without change in phase in case of normal incidence and the reflected

qP

-wave annihilates the incident

qP

-wave for grazing incidence one. It may be noted from the above analytical expressions for the reflection/transmission coefficients that the characteristics of reflected and transmitted waves depends on material parameters and incidence angle in addition to thermal variation and fluid loading effects.

5.2 Quasi transverse

qSV

-wave incidence

Now consider the reflection and transmission of a plane

qSV

-wave for similar conditions on the boundary as in Section 5.1 above. The total displacement field in this case is given by

exp{

(

sin

cos

)}

exp(

)

)}

cos

sin

(

exp{

4 4

4 4

4

4



i

Z

X

ik

A

Z

X

ik

A

i

r

i

r

,

r

,

r

,

L

Lt

,

L

Lt (55)

where

r

,

r

,

r

,

Lt

,

Lt are defined in equations (32)-(37).

Upon using expressions (55) in the boundary conditions (24)-(26), at the surface

Z

0

and assuming that all the incident, reflected or transmitted waves are in phase at this surface for all values of

X

and

, so that

sin

4

k

k

1

sin

1

k

2

sin

2

k

3

sin

3

k

4

sin

4

k

5

sin

5 (56)

we obtain a system of five coupled algebraic equations given as

1

B

AZ

s

(57)

Where

* 1 51

41

1 34 24 14

1

a

a

a

S

a

V

a

B

,

qSV qSV qSV qSV qSV

s

R

R

R

R

T

Z

1

,

2

,

3

,

4

,

1

(13)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

1

1

~

qSV

R

,

2

2

~

qSV

R

,

3 3

~

qSV

R

,

4

4

~

qSV

R

,

5

1

~

qSV

T

(58)

where

1

( 1, 2, 3, 4)

k

r qSV k

i

A

R k

A

  and

1

5 1

qSV

i

A

T

A

are amplitude ratios of the reflected and

transmitted waves. Here, the quantities

~

i

(

i

1

,

2

,

3

,

4

,

5

)

used in equation (58) can be obtained

from

by replacing first, second, third, fourth and fifth column by

1 51

* 41 1 34 24

14

a

a

S

a

V

a

a

respectively.

In case of both normal

(

0

0

4

5

)

and grazing

(

90

0

4

)

incidence, the relation (58) reduces to

1

4

qSV

R

,

qSV qSV

qSV qSV

T

R

R

R

1

2

3

0

1 (59) Thus the shear (

qSV

) wave is reflected as

qSV

-wave in case of normal incidence and the

reflected (

qSV

) wave annihilates the incident wave for grazing incidence.

In the absence of mass diffusion

(

a

0

2

)

, the non vanishing amplitude ratios are



ˆ

ˆ

1 1

qSV

R

,



ˆ

ˆ

2 3

qSV

R

,



ˆ

ˆ

3 4

qSV

R

,



ˆ

ˆ

4 1

qSV

T

(60)

Here, the quantities



ˆ

i

(

i

1

,

2

,

3

,

4

)

used in equation (60) can be obtained from

ˆ

by replacing

first, second, third and fourth column by

*

41 1 34 24

14

a

a

S

a

a

respectively.

In the absence of mass diffusion and thermal fields

(

a

0

2

,

T

0

)

, the amplitude ratios at normal

(

0

0

1

)

and grazing

(

90

0

1

)

incidence of

qSV

wave, are given by

qSV qSV

qSV

T

R

R

1

3

0

1 , 4

1

qSV

R

(61)

Thus only shear (

qSV

) wave is reflected as

qSV

-wave in case of normal incidence and the reflected (

qSV

) wave annihilates the incident wave for grazing incidence case. The other waves do not reflect or transmit in either case.

5.2.1 Quasi transverse

qSV

-wave incidence at the free surface

In case

(

L

0

)

, the amplitude ratios for stress free, insulated and stress free, isothermal thermoelastic half-space are, respectively, given by

L

qSV

i

S

a

a

a

a

a

S

a

a

a

R

1 1 1 13 24 23 14 3 3 3 14 24 1

cos

2

)

(

cos

(14)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

L

qSV

i

S

a

a

a

S

a

a

a

a

a

R

2

1 1

cos

1 14 24 1 1

cos

1

(

11 24 21 14

)

3

L

qSV

i

S

a

a

a

S

a

a

a

S

a

a

a

a

a

R

1

2

1 1

cos

1 13 24

2

3 3

cos

3 11 24 1 1

cos

1

(

11 23 21 13

)

4

(62)

and

L

qSV

S

a

a

a

a

S

a

a

R

1 13 24 23 14 3 14 24

1

2

)

(

L

qSV

S

a

a

S

a

a

a

a

R

2

1 24 14 1

(

11 24 21 14

)

3 (63)

L

qSV

S

a

a

S

a

a

S

a

a

a

a

R

1

2

1 24 13

2

3 11 24 1

(

11 23 21 13

)

4

where

L and

Lare defined in equations (51) and (52) respectively.

In the absence of mass diffusion, fluid and thermal fields

(

a

0

2

,

T

0

L

)

, the non vanishing amplitude ratios are

3 2 3 1

2

3 1

2

cos

2

sin

2

sin

4

sin

qSV

R

3 2 3 1

2

3 2 3 1 2

4

2

cos

2

sin

2

sin

2

cos

2

sin

2

sin

qSV

R

(64)

Equations (64) are in agreement with the corresponding equations as in Achenbach (1973). In case of both normal

(

0

0

4

)

and grazing

(

90

0

4

)

incidence of

qSV

wave, the expressions for reflection coefficients in equation (63) provide us

0

1

qSV

R

,

R

4qSV

1

(65) Thus only shear wave is reflected as

qSV

wave without any change of phase in case of normal incidence and reflected

qSV

-wave annihilates the incident

qSV

wave in case of grazing incidence. It is noticed that the reflection/transmission characteristics of waves depends upon material parameters and incidence angle in this case too.

6 TOTAL REFLECTION

(15)

Latin American Journal of Solids and Structures 11 (2014) 2141-2170

sin

4

k

k

i

sin

i

(

i

1

,

2

,

3

,

4

)

(66)

Here the quantities

a

i2

(

i

1

,

2

,

3

,

4

)

are complex and so does at the wave numbers

)

4

,

3

,

2

,

1

(

2

i

k

i are also complex. Thus the phase velocities

(

c

i

(

/

k

i

)

i

1

,

2

,

3

,

4

)

of these

waves are complex and the waves becomes attenuated in space. If we take

4

,

3

,

2

,

1

,

1 1

1

j

Q

i

V

c

j j

j (67)

where

k

j

j

iQ

j

,

j

/

V

j and

Q

j

(

j

1

,

2

,

3

,

4

)

are real quantities. Then

V

j,

Q

j

respectively represent phase speed and attenuation coefficients of these waves. Upon using relations (67) in equation (66), we get

4

sin

1

sin

1

2

sin

2

3

sin

3

4

sin

4

1 1

sin

Q

Q

2

sin

2

Q

3

sin

3

0

(68)

Because

Q

4

0

, therefore

4 4

k

,

4 ,

V

4

c

4, 4

1 4 1

sin

sin

V

V

j j

Now upon using equations (66)-(68), the potential function

r given in equation (32) can be rewritten as

3

1

2 2 2

4

(

sin

sin

)}

exp(

)

exp{

}

exp{

j

j j

rj

r

A

Q

Z

i

k

X

Z

V

i



Now for

qP

and

qSV

waves

V

2

V

1

2 2 2 2 1

2 

V

V

and

sin

increases to the value 1 1

V

first for

2

0

. If

sin

V

1

sin

c

1

, then

c is called critical angle. For

cthe

factor

2 2

1

2

sin

V

becomes purely imaginary. In the absence of thermal field the critical angle

c for elastic wave is obtained when

V

1

1

, so that

1

sin

c . Thus in the presence of

thermal field, the value of critical angle increases as

V

1

1

or

1

. For 1 2 1 1

sin

V

V

 , we have

2

1

4 2

2 2

4

sin

}

]

exp{

(

sin

)}

{

exp[

j

j j

rj

r

A

Q

k

V

Z

i

k

X



(69)

Thus the thermal part and elastic part of reflected P-wave propagates horizontally in

X

-direction and these quantities decay exponentially with depth.

Moreover, we have also considered the relation

a

1

sin

1

sin

, which shows that

1is real

only if

c, where

 

1

1

sin

a

c

, this equals to 1

 

0

29

sin

Imagem

Figure 1: Geometry of the problem.
Figure 2:  qP -wave incidence at the interface in case of thermoelastic-diffusion (TED)
Figure 4:  qP -wave incidence at the interface in case of thermoelasticity (TE).
Figure 6:  qP -wave incidence at the free surface in case of thermoelasticity (TE).
+5

Referências

Documentos relacionados

This paper dealt with free vibration analysis of thick double curved composite sandwich panels with simply supported or fully clamped boundary conditions based on a new

[r]

An investigation on the effect of uniform tensile in plane force on the radially symmetric vibratory characteristics of functionally graded circular plates of linearly

From these figures, it is clear that as the clay content is increased, there is increase in damping factor which is due to the presence of the additional medium (clay) in

[r]

The implementation of this signal processing algorithm in the damage detection method permits the identification of small frequency changes, and consequently

[r]

In present study, the stress function approach is modified to reconstruct the residual stress and eigenstrain field form experimental residual stress measurements in surface