Reflection of quasi-p and quasi-sv waves at the free and rigid boundaries of a fibre-reinforced medium

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Sādhan ā Vol. 7 Part 6 December 00 pp. 63 630. Printed in India Reflection of quasi-p and quasi-sv waves at the free and rigid boundaries of a fibre-reinforced medium A CHATTOPADHYAYRLKVENKATESWARLU and S SAHA Department of Applied Mathematics Indian School of Mines Dhanbad 86 004 India e-mail: c amares@yahoo.com MS received 5 May 00; revised 8 August 00 Abstract. The propagation of plane waves in fibre-reinforced media is discussed. The expressions of phase velocities of quasi-p (qp) and quasi-sv (qsv) waves propagating in plane symmetry are obtained in terms of propagation vectors. We have established a relation from which the displacement vector can be obtained in terms of the propagation vector. Expressions for the reflection coefficients of qp and qsv waves are obtained. Numerical results of reflection coefficients are obtained and presented graphically. The partition of energy between qp and qsv waves reflected on free and rigid boundaries due to incident qp and qsv waves are also obtained and presented graphically. Keywords. Reflection of waves; quasi-p waves; quasi-sv waves; quasi-sh waves; fibre-reinforced media; reflection coefficients. Introduction Fibre-reinforced composite materials have become very attractive in many engineering applications recently due to their superiority over other structural materials in applications requiring high strength and stiffness in lightweight components. Consequently the characterisation of their mechanical behaviour is of particular importance for structural design using these materials. Effects of earthquakes on artificial structures are of prime importance to engineers and architects. During an earthquake and similar disturbances a structure is excited into a more or less violent vibration with resulting oscillatory stresses which depend both upon the ground vibration and physical properties of the structure (Richter 958). Most concrete construction includes steel reinforcing at least nominally. Thus wave propagation in a reinforced medium plays a very important role in civil engineering and geophysics. The propagation of body waves in anisotropic media is fundamentally different from their propagation in isotropic media although the differences may be comparatively subtle and difficult to observe (Crampin 975). In general for any type of anisotropy there are always three types of body waves propagating with three different velocities. Choosing the three components of displacement adequately they are called quasi-p(qp) quasi-sv(qsv) and quasi-sh 63

64 A Chattopadhyay et al (qsh) waves. The velocities of these three waves change according to the type of symmetry present in the medium. Owing to these properties anisotropy is detected by observations of change in P-wave velocity along two perpendicular directions and by observations of S-wave splitting. For both these effects it is not necessary that the whole medium be anisotropic; only some part of it need be so (Udias 999). Generally particle motion is neither purely longitudinal nor purely transverse. For this reason the three types of body waves in an anisotropic medium are referred as qp qsv and qsh instead of P SV and SH. The problem of reflection and refraction of elastic have been discussed by several authors. Without going into the details of the research work in this field we mention the papers by Knott (899) Gutenberg (944) Thapliyal (974) Keith & Crampin (977) Dey & Addy (979) Tolstoy (98) Norris (983) Pal & Chattopadhyay (984) Achenbach (976) Henneke (97) Chattopadhyay et al (995) and Singh et al (00) as giving a broad picture of the work done so far. Crampin & Taylor (97) studied surface wave propagation in examples of unlayered and multi-layered anisotropic media which is examined numerically with a program using an extension of the Thompson-Haskell matrix formulation. They studied some examples of surface wave propagation in anisotropic media to interpret a possible geophysical structure. Crampin (975) showed that the surface waves have distinct particle motion when propagating in a structure having a layer of anisotropic material with certain symmetry relations. Chattopadhyay & Saha (996) have studied the problem of reflection of qsv-wave at free and rigid boundary in a medium of monoclinic type. The above mentioned authors have not studied the reflection behaviour at a free and rigid boundaries of a fibre-reinforced medium. The reflection of qp and qsv waves in a fibre-reinforced medium is discussed. In this paper we have computed the reflection coefficients of qp and qsv waves at the free and rigid boundary of a fibre-reinforced medium. It is well known that in an anisotropic medium the direction of particle motion is neither perpendicular nor parallel to the direction of propagation. Considering this fact a relation has been established to calculate the displacement vector in terms of propagation vector. The expressions for phase velocity of qp and qsv waves are obtained in terms of the propagation vector. The partition of energy between qp and qsv waves reflected for qp and qsv waves incident on a free and rigid boundaries have been derived and presented graphically.. Formulation of the problem The constitutive equations for fibre-reinforced linearly elastic medium whose preferred direction is that of a are (Spencer 97) τ ij = λe kk δ ij + µ T e ij + α(a k a m e km δ ij + e kk a i a j ) + (µ L µ T )(a i a k e kj + a j a k e ki ) + β(a k a m e km a i a j ) where τ ij are components of stress e ij are components of infinitesimal strain a j are components of a all referred to cartesian coordinates. The vector a may be a function of position. The coefficients λ µ L µ T αand β are elastic constants with the dimension of stress. If a is so chosen that its components are (00). The stress components () become τ = (λ + α + 4µ L µ T + β)e + (λ + α)e + (λ + α)e 33 τ = (λ + α)e + (λ + µ T )e + λe 33 ()

The reflection of quasi-p and quasi-sv waves 65 τ 33 = (λ + α)e + λe + (λ + µ T )e 33 τ = µ L e τ 3 = µ L e 3 τ 3 = µ T e 3 () where e ij = u ij + u ji and u i (i = 3) are the displacement components. We take the plane of symmetry of the fibre-reinforced medium as the x x -plane and x - axis vertically upwards. For the plane wave propagation in x x -plane we have / x 3 = 0. The non-vanishing equations of motion without body forces are τ + τ = ρ u x x t τ + τ x x = ρ u t (3) τ 3 + τ 3 x x = ρ u 3 t The stress equations of motion (3) with the help of () become (λ + α + 4µ L µ T + β) u x + µ L u x + (λ + α + µ L ) u x x = ρ u t (4) µ L u x + (λ + µ T ) u x + (λ + µ L + α) u x x = ρ u t (5) µ L u 3 x + µ T u 3 x = ρ u 3 t. (6) From (4) to (6) it is obvious that qsh wave which is represented by u 3 motion in (6) is decoupled from (u u )motion representing qp and qsv waves. The phase velocity of qsh wave is ρc n = µ L{p (n) } + µ T {p (n) } (7) where p (p (n) p(n) 0) denote the unit propagation vector c n is the phase velocity and k n is the wave number of plane waves propagating in the x x -plane. We consider plane wave solutions of (4) and (5) as ( ) ( u d (n) ) = A u d (n) exp [ ik n (x p c n t) ] (8) where d (d (n) d(n) 0) is the unit displacement vector. Using the expressions of (8) for u and u in the equations of motion (4) and (5) we obtain where d (n) d (n) = S ρcn R = ρc n T (9) S R = (λ + α + 4µ L µ T + β){p (n) } + µ L {p (n) } S = (λ + α + µ L )p (n) p(n) T = µ L {p (n) } + (λ + µ T ){p (n) }. (0)

66 A Chattopadhyay et al Equation (9) may be used to find the d in terms of p. From the above equation we have ρ c 4 n (R + T)ρc n +(RT S ) = 0. The solutions of the above equation are ρc n = (R + T)±[(R T) +4S ] /. Velocities of qp wave and qsv waves are ρc L = (R + T)+( (R T) +4S ) / () ρc T = (R + T) ( (R T) +4S ) / () From (4) and (5) we obtain [(λ + α + 3µ L µ T + β)d (n) d(n) {p(n) } ] + (µ L λ µ T )d (n) d(n) {p(n) } + (λ + α + µ L )[{d (n) } {d (n) } ]p (n) p(n) = 0. (3) Pure longitudinal and shear waves can propagate only in certain specific directions. Longitudinal and transverse specific directions are found by taking d = p and d perpendicular to p. In the anisotropic case no such relations can be considered between the displacement vector and the propagation vector. We consider a homogeneous fibre-reinforced half-space occupying the region x 0 and the plane of symmetry is taken as the x x -plane. Plane qp wave is incident at the tractionfree boundary x = 0 and will generate reflected qp and qsv waves. Let n = 0 be assumed for incident qp reflected qp and reflected qsv waves respectively. We consider the plane strain problem and hence u = u (x x t) u = u (x x t) u 3 = 0. The displacement field may be represented by u = A j d (j) eiη j u = A j d (j) eiη j (4) where j=0 j=0 η n = k n (x p (n) + x p (n) c n t). (5) For incident qp wave which makes an angle θ 0 wehave p (0) =sin θ 0 p (0) =cos θ 0 c 0 =c L. In the plane x = 0 the displacement and stress components due to incident qp-wave may be written as u (0) = d (0) eiη 0 u (0) = d (0) eiη 0 τ (0) = ik 0 [(λ + α)d (0) sin θ 0 + (λ + µ T )d (0) cos θ 0 ]e iη 0 (6) τ (0) = ik 0 µ L [d (0) cos θ 0 + d (0) sin θ 0 ]e iη 0 where η 0 = k 0 (x p (0) c L t). (7)

The reflection of quasi-p and quasi-sv waves 67 For a reflected qp wave which makes an angle θ we have p () = sin θ p () = cos θ c =c L. In the plane x = 0 the displacement and stress components due to reflected qp-wave may be written as where u () = A d () eiη u () =A d () eiη τ () = ia k [(λ + α)d () sin θ (λ + µ T )d () cos θ ]e iη τ () = ia k µ L [ d () cos θ + d () sin θ ]e iη (8) η = k (x p () c L t). If the reflected qsv wave makes an angle θ wehave p () =sin θ p () = cos θ c =c T. In the plane x = 0 the displacement and stress components due to reflected qsv-wave may be written as where u () = A d () eiη u () =A d () eiη τ () = ia k [(λ + α)d () sin θ (λ + µ T )d () cos θ ]e iη τ () = ik A µ L [ d () cos θ + d () sin θ ]e iη (9) η = k (x p () c T t). 3. Boundary conditions and solution of the problem for incident qp-waves Case : Reflection reflection of qp-wave at a free boundary. When x = 0 is a free surface the sum of the three tractions must vanish at x = 0 and we can write the boundary conditions as: and τ (0) + τ () + τ () = 0 τ (0) + τ () + τ () = 0. (0) Substituting in (0) the values of τ (n) obtain: τ(n) (for n = 0 ) from (6) (8) and (9) we ik 0 [(λ + α)d (0) sin θ 0 + (λ + µ T )d (0) cos θ 0 ]exp(iη 0 ) + ik A [(λ + α)d () sin θ (λ + µ T )d () cos θ ]exp(iη ) + ik A [(λ + α)d () sin θ (λ + µ T )d () cos θ ]exp(iη ) = 0 ()

68 A Chattopadhyay et al and ik 0 [d (0) cos θ 0 + d (0) sin θ 0 ]exp(iη 0 ) + ik A [ d () cos θ + d () sin θ ]exp(iη ) + ik A [ d () cos θ + d () sin θ ]exp(iη ) = 0. () Equations () and () must be valid for all values of x and t hence which means This gives and η 0 = η = η (3) k 0 (x sin θ 0 c L t) = k (x sin θ c L t) = k (x sin θ c T t). k 0 sin θ 0 = k sin θ = k sin θ = φ k 0 c L = k c L = k c T = ω (4) where φ is the apparent wave number and ω is the circular frequency. From the above relations we have and k k 0 = c L c L = sin θ 0 sin θ k k 0 = c L c T = sin θ 0 sin θ. (5) Equations () and () after using (3) may be written as where P 0 + P A + P A = 0 P 3 + P 4 A + P 5 A = 0 (6) P 0 = k 0 [(λ + α)d (0) sin θ 0 + (λ + µ T )d (0) cos θ 0 ] P = k [(λ + α)d () sin θ (λ + µ T )d () cos θ ] P = k [(λ + α)d () sin θ (λ + µ T )d () cos θ ] P 3 = k 0 [d (0) cos θ 0 + d (0) sin θ 0 ] P 4 = k [ d () cos θ + d () sin θ ] P 5 = k [ d () cos θ + d () sin θ ]. (7) Solving the above two equations we have A = a b a b a b A = a b a b a b (8)

The reflection of quasi-p and quasi-sv waves 69 where d (i) /d(i) a = P P 0 a = P P 0 b = P 4 P 3 b = P 5 P 3. (i = 0 ) can be calculated from (9) and are as under: d (0) /d(0) = (ρcl T )/S (9) where R S and T can be calculated after putting p = p (0) = sin θ 0 and p = p (0) = cos θ 0 in (0). d () /d() = (ρc L T )/S (30) where R S and T can be calculated after putting p = p () = sin θ and p = p () cos θ in (0). = d () /d() = (ρc T T )/S (3) where R S and T can be calculated after putting p = p () = sin θ and p = p () = cos θ in (0). From () and () the velocities of incident qp reflected qp and reflected qsv may be defined by ρc L = (R + T)+( (R T) +4S ) / ρc L = (R + T ) + ( (R T ) + 4S) / ρct = (R + T ) ( (R T ) + 4S) / (3) where RR R SS S TT and T are defined in (9) to (3). Using the following values of reinforced-free medium µ L = µ T = µ α = β = 0 equations (8) reduce to A = sin θ 0 sin θ K cos θ sin θ 0 sin θ + K cos θ (33) where A = K sin θ 0 cos θ sin θ 0 sin θ + K cos θ (34) K = [(λ + µ)/µ] / which are the reflection coefficients of P and SV waves respectively for free boundary in isotropic case (Achenbach 976 p. 75). The partition of energy between reflected qp and qsv waves for incident qp wave is given by ( ) ( A c L A c / L m cos θ m 0 cos θ 0 + ) c L c T m cos θ m 0 cos θ 0 = (35)

60 A Chattopadhyay et al where m 0 = (ap (0) d(0) + bp (0) d (0) ) sin θ 0d (0) + µ L (d (0) p(0) + d (0) p(0) ) (d (0) cos θ 0 + d (0) sin θ 0 ) + (bd (0) p(0) + cd (0) p(0) )d(0) cos θ 0 m = (ap () d() + bp () d () ) sin θ d () + µ L (d () p() + d () p() ) ( d () cos θ + d () sin θ ) (bp () d() + cp () d () )d() cos θ m = (ap () d() + bp () d () ) sin θ d () + µ L (d () p() + d () p() ) ( d () cos θ + d () sin θ ) (bp () d() + cp () d () )d() cos θ. a = λ + α + 4µ L µ T + β b = λ + α c = λ + µ T. For an isotropic case (35) becomes ( A ) + ( A ) c T c L cos θ cos θ 0 = which is same as that of Achenbach (976 p. 8). The velocity of surface wave can be obtained from (8) by equating the denominator to zero. It has been observed that the surface wave velocity at θ = 8.8 in the case of a fibrereinforced medium is.58 times more than the Rayleigh wave in the classical case (values of λ α β µ T and µ L are defined in (6). Case : Reflection of qp -wave at a rigid boundary. Since the boundary x = 0 is bounded by a rigid layer the boundary conditions may be taken as and u (0) + u () + u () = 0 u (0) + u () + u () = 0. (36) Substituting the values of u (n) u(n) for n = 0 from (6) (8) and (9) in (36) we get d (0) exp(iη 0 ) + A d () exp(iη ) + A d () exp(iη ) = 0 (37) d (0) exp(iη 0 ) + A d () exp(iη ) + A d () exp(iη ) = 0. (38) Solving the above two equations we have A = d() d(0) d () d () d() d () d(0) d() A = d(0) d() d () d () d () d() d(0) d(). (39) The above equations are the reflection coefficients of qp and qsv waves for rigid boundaries.

The reflection of quasi-p and quasi-sv waves 6 4. Reflection of qsv waves at a free boundary Incident qsv wave will generate reflected qp and qsv waves. Let n = 0 be assumed for incident qsv reflected qp and reflected qsv waves respectively. For incident qsv wave which makes an angle θ 0 wehave p (0) =sin θ 0 p (0) =cos θ 0 c 0 =c T. (40) In the plane x = 0 the displacement and stress components of incident wave and reflected waves are same as in (6) (8) and (9). Equation (7) to be replaced by η 0 = k 0 (x p (0) c T t). (4) 5. Boundary conditions and solution of the problem for qsv waves 5. Reflection of qsv wave at a free boundary Substituting in (0) the values of τ (n) τ(n) (for n = 0 ) from (4) (8) and (9) we obtain the same expressions as () and () except that c L is replaced by c T. The ratio d (0) /d(0) is mentioned in (43) other ratios are the same as (30) and (3). Equations () and () must be valid for all values of x and t hence k 0 sin θ 0 = k sin θ = k sin θ = φ and k 0 c T = k c L = k c T = ω (4) where φ and ω are defined in (4). Solving () and () we have the same sets of equations as (6) with some changes as mentioned below: (i = 0 ) may be calculated from (9) and are as under. d (i) /d(i) d (0) /d(0) = (ρc T T )/S (43) where R S and T can be calculated after taking p = p 0 = sin θ 0 and p = p (0) = cos θ 0 in (0). d (i) /d(i) (i = ) are defined in (30) and (3). From () and () the velocity of incident qsv may be defined by ρc T = (R + S) ( (R S) + 4T ) /. (44) Reflected qp and qsv waves velocities are already defined in (3). Using the following values of reinforced- free medium (values are mentioned in section 3) we obtain the reflection coefficients for isotropic case as A Ksin 4θ 0 = sin θ 0 sin θ + K cos θ 0 A = sin θ 0 sin θ K cos θ 0 (45) sin θ 0 sin θ + K cos θ 0 where K = [(λ + µ)/µ] /.

6 A Chattopadhyay et al The partition of energy between reflected qp and qsv waves due to incident qsv wave is given by ( A ) c T c L m cos θ m 0 cos θ 0 + where all definitions are as in (35). ( A ) c T c T m cos θ m 0 cos θ 0 = (46) 5. Reflection of qsv wave at a rigid boundary Since the boundary x = 0 is a rigid layer the boundary conditions are the same as for (36). After substituting the values of u (n) u(n) for n = 0 from (4) (8) and (9) in (36) and solving we have the same sets of equations as in (39) for reflection coefficients of qp and qsv waves. Here d (i) (i = 0 ) are as defined in (43) (30) and (3). /d(i) 6. Numerical calculations and discussions The material constants for fibre-reinforced medium have been considered as per Markham (970). µ T =.46 0 9 N/m µ L =5.66 0 9 N/m λ = 5.65 0 9 N/m β=0.90 0 9 N/m α =.8 0 9 N/m ρ=7800 kg/m 3. 6. Reflection of qp waves In figure curve II corresponds to reflection coefficient of qp-wave in fibre-reinforced medium. All the values of curve II are negative except from 0 to 0 and from 83 to 90.In Figure. Amplitude ratios of qp waves due to incident qp waves.

The reflection of quasi-p and quasi-sv waves 63 Figure. Amplitude ratios of qsv waves due to incident qp waves. the isotropic case (curve I) the values of (A / ) are all negative except from θ 0 = 57 to 78. Significant differences of values exist from 0 to 5 and from 80 to 90 in fibre-reinforced case compared to isotropic case. The values from to 80 are greater in the isotropic case compared to those in the fibre-reinforced case. In figure the reflection coefficients of qsv waves for a free boundary of fibre-reinforced medium at different angles of incidence have plotted along with the curve for isotropic medium. The values of (A / ) are all positive and equal for curves I and II at θ 0 = 0 5 and 90. The difference in values at θ 0 = 50 in isotropic case is significantly more compared to fibre-reinforced medium. Figure 3 shows the comparison of partition of energy between reflected P and qp waves for incident qp waves. In this case A / = 0 for angle of incidence at 60 and 78 and A / = for angle of incidence at 0 and 90 in case of isotropic media. For fibre-reinforced medium (curve II) A / = at0 only. Figure 3. Partition of energy of qp waves due to incident qp waves.

64 A Chattopadhyay et al Figure 4. Partition of energy of qsv waves due to incident qp waves. Figure 4 shows the comparison of partition of energy between reflected SV and qsv waves for incident qp waves. In this case A / = 0at0 for both isotropic and fibre-reinforced (curve II) media. The critical point exists at 3. In figure 5 the values of reflection coefficients of qp-wave for isotropic (curve I) and fibre-reinforced media (curve II) have been plotted for rigid boundaries. The values of A / for fibre-reinforced media sharply increase from 0 to 8 and then remain constant from 9 to 90. The value of A / at 90 is significantly more in case of a fibre-reinforced medium compared to the isotropic case and at 0 the value in the isotropic case is more compared to that in the fibre-reinforced case. The critical point exists at 8. In figure 6 the values of reflection coefficient of qsv (A / ) have been plotted for rigid boundary in curves II and I. It has been observed that all the values of the reflection Figure 5. Amplitude ratios of qp waves due to incident qp waves in rigid boundary.

The reflection of quasi-p and quasi-sv waves 65 Figure 6. Amplitude ratios of qsv waves due to incident qp waves in rigid boundary. coefficients of qsv are negative except those at 0 and 90. The values are greater in case of fibre-reinforced media as compared to isotropic media from 5 to 89. The maximum difference exists at 0. The critical point exists at 5. Figures 7 and 8 show the partition of energy between reflected qp and qsv waves for incidence of a qp wave in a rigid boundary. 6. Reflection of qsv waves In figure 9 curve I corresponds to isotropic medium and agrees with the result of Achenbach (976). Curve II corresponds to fibre-reinforced medium. The value of A / in a fibrereinforced medium is greater compared to that in isotropic medium but the difference is greater at 33. In figure 0 the reflection coefficient of qsv-waves (curve II) for reinforced medium for different values of θ 0 ranging from 0 to 33 have been plotted which are permissible of θ 0 Figure 7. Partition of energy of qp waves due to incident qp waves in rigid boundary.

66 A Chattopadhyay et al Figure 8. Partition of energy of qsv waves due to incident qp waves in rigid boundary. for A / in fibre reinforced medium and compared with those in isotropic media (curve I). In this case due to the effect of fibre-reinforced medium the values of A / are greater compared to the isotropic case. This rigid boundary plays a very important role in case of reflection phenomena. All the values of A / (figure 3) in case of fibre-reinforced material in a rigid boundary are less compared to the isotropic case. Figure 4 shows the reflection coefficient A / for qsv wave. The values of A / for fibre-reinforced media with rigid boundaries coincide with the values of A / for isotropic media at 3. This is the critical point. The values for fibre-reinforced media (curve II) are less compared to those for isotropic media from 5 to 3. Figures 5 and 6 show the partition of energy for incident qsv waves due to free and rigid boundaries. Figure 9. Amplitude ratios of qp waves due to incident qsv waves.

The reflection of quasi-p and quasi-sv waves 67 Figure 0. Amplitude ratios of qsv waves due to incident qsv waves. Figure. Partition of energy of qp waves due to incident qsv waves. Figure. Partition of energy of qsv waves due to incident qsv waves.

68 A Chattopadhyay et al Figure 3. Amplitude ratios of qp waves due to incident qsv waves in rigid boundary. Figure 4. Amplitude ratios of qsv waves due to incident qsv waves in rigid boundary. Figure 5. Partition of energy of qp waves due to incident qsv waves in rigid boundary.

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