Jtam-A4.dvi JOURNAL OF THEORETICAL AND APPLIED MECHANICS 55, 4, pp. 1369-1380, Warsaw 2017 DOI: 10.15632/jtam-pl.55.4.1369 THERMOELASTIC STRAIN AND STRESS FIELDS DUE TO A SPHERICAL INCLUSION IN AN ELASTIC HALF-SPACE Kuldip Singh, Renu Muwal Guru Jambheshwar University of Science and Technology, Department of Mathematics, Hisar, Haryana, India e-mail: renumuwal66@gmail.com In this paper, closed form analytical expressions for thermoelastic strain and stress compo- nents due to a spherical inclusion in an elastic half-space are obtained. These expressions are derived in the context of steady-state uncoupled thermoelasticity using thermoelastic displacement potential functions. The thermal strain and stress fields are generated due to differences in the coefficients of linear thermal expansion between a subregion and the surrounding material. The strain and stress components for exterior points of the spheri- cal inclusion are same as those of the center of dilatation. Variations of strain and stress components for exterior and interior points of the spherical inclusion are shown graphically. Keywords: uncoupled thermoelasticity, strain and stress fields, potential functions, spherical inclusion 1. Introduction Thermoelasticity is an extension of theory of elasticity to include thermal effects. Theory of thermoelasticity is concerned with the interaction between the thermal field and elastic bodies. Comprehensive treatises on the topics of thermoelasticity have been covered in the classical texts (Nowinski, 1978; Truesdell, 1984; Nowacki, 1986; Boley and Weiner, 1997; Boresi et al., 2011; etc.). The study of thermoelasticity has begunwith Duhamel (1837) andNeumann (1885), who postulated equations of linear thermoelasticity for isotropic bodies. Goodier (1937) studied the static problem of uncoupled thermoelasticity by employing the method of superposition using displacement potential functions.With the help ofGoodier’smethod,Mindlin andCheng (1950) obtained the thermal stress in a semi-infinite elastic solid with the traction free surface for the centre of dilatation using Galerkin’s vector stress function. The result was then applied to the case of a spherical inclusion in a semi-infinite medium. Nowacki (1957) considered the problem of an instantaneous source of heat in an infinite isotropic elastic space and determined the state of stress using the potential of thermoelastic strain. Also, stress components in a semi-infinite elastic space due to an instantaneous source of heatwas obtained using themethod ofGalerkin’s displacement function and the Fourier integral under stress free surface boundary conditions. Sen (1957) presented a direct method for solving problems of circular holes in an isotropic elastic plate having prescribed displacements on the edge. The problem of deformation in an infinite isotropic plate due to the centre of dilatation in the form of a nucleus of thermoelastic strain at a finite distance from the holewas also discussed. Sharma (1957) obtained deformation and stress fields due to a nucleus of thermoelastic strain in an infinite solid having a spherical cavity using interior and exterior spherical harmonics. Another problem of a solid sphere at zero temperature having a heated nucleus inside was also discussed. Biharmonic solutions to steady state thermoelastic problems in three dimensions were derived by Nowinski (1961). Nowinski (1963) proved amean value theorem for an arbitrary steady-state thermoelastic problem for an 1370 K. Singh, R. Muwal isotropic elastic solid sphere. The stress components at the center of the sphere were expressed in terms of temperature on the surface of the sphere. Guell andDundurs (1967) obtained elastic fields due to a subregion between two joined half- -spaces by differentiation from the corresponding fields for the whole space using the solutions for the center of dilatation. The Papkovich-Neuber displacement potentials were used when the interface between two joined half-spaces was a smooth interface and perfectly bonded. Those resultswere then applied to a spherical inclusion.The case of the force on the center of dilatation was also discussed. Hu (1989) considered the problem of a parallelepipedic thermal inclusion in a three-dimensional half-space and derived analytical solution using Goodier’s method of the nucleus of thermal strain or the center of dilatation. Wang and Huang (1991) studied some thermoelastic problems in the half-space by using Goodier’s thermoelastic potential functions and general solutions of elasticity based on theBoussinesq solutions (consisting of different har- monic functions). Yu et al. (1992) and Yu and Sanday (1992), respectively, derived analytical solutions for thermoelastic displacements and stresses due to an inclusion in adissimilarmedium consisting of two joined semi-infinite elastic solids and for the centre of dilatation in a plate. The stress-deformation state of an elastic half-space due to an inhomogeneous spheroidal ther- mal inclusion in the form of a prolate or oblate ellipsoid of revolution under stress-free surface boundary conditions was discussed by Kolesov et al. (1992) using thermoelastic displacement potential functions and theTeredzavemethod.Yu et al. (2002) calculated thermal stresses indu- ced by an ellipsoidal inclusion with uniform dilatational eigenstrains in one of the two perfectly bonded semi-infinite solids using the method of dilatation centres and potential functions. Da- vies (2003) derived the elastic field due to a non-uniform temperature or a coherentlymisfitting inclusion in a semi-infinite region from the corresponding field in an infinite region. Using Green’s function method and series expansion techniques, closed form solutions for displacement and stress fields due to a hemispherical inclusion with a uniform eigenstrain in a semi-infinite isotropic elastic medium were obtained by Linzhi (2003). Liu and Wang (2005) obtained the elastic field caused by eigenstrains in a half-space using two types of numerical techniques – discrete correlation and fast Fourier transform as well as discrete convolution and fast Fourier transform. To obtain that field, analytical solutions for influence coefficients were expressed in terms of derivatives of four key integrals. Zhou et al. (2009) introduced a fast me- thod for solving the problem of three-dimensional arbitrarily shaped inclusions in an isotropic half-space using a combination of 2D and 3D fast Fourier transform. A fast method for solving contact problems for a half-space containing multiple inhomogeneities such as voids, cavities, inclusions and fibers was presented by Leroux et al. (2010). The displacement and stress fields due to eigenstrains of all spherical inclusion were obtained using Eshelby’s equivalent inclusion method along with 2D and 3D fast Fourier transforms. Itou (2014) derived basic equations for thermoelastic plane stress conditions and thermoelastic plane strain conditions. Two problems were solvedusing thermoelastic displacementpotential functions: (i) axisymmetric thermal stres- ses for a hollow thin disk, (ii) thermal stresses for an infinite thin platewith a circular hole under uniform heat flow. Kumagai et al. (2014) presented different representations of a seismic sphe- rical source. Those different representations consisted of a spherical source (S1), spherical crack source (S2), isotropic source of threemutually perpendicular vector dipoles (S3) or threemutu- ally perpendicular tensile cracks (S4), Eshelby’s spherical source with stress-free strain (S5) and Eshelby’s spherical source with strain-free stress (S6). Static displacement fields due to those sources in an infinite medium and in a half-space were also derived. In the present paper,we obtain thermoelastic strain and stress fields due to a spherical inclu- sion in an elastic half-space in the context of steady-state uncoupled thermoelasticity. Following the method opted by Davies (2003), we derive thermoelastic strain and stress components for an infinite region fromwhich corresponding fields can be derived in the semi-infinite region. The expressions for these fields are obtained for the axisymmetric problem in cylindrical coordinates Thermoelastic strain and stress fields due to a spherical inclusion... 1371 using thermoelastic displacement potential functions. These results are in good agreement with the results found byMindlin and Cheng (1950). 2. Theory In the linear theory of thermoelasticity, the total strain can bewritten as the sumofmechanical and thermal strains (Goodier, 1937; and Nowinski, 1978) eij = e (M) ij +e (T) ij (2.1) inwhich for an isotropicmaterial, the thermal strain takes the form e (T) ij =αTδij, whereα is the coefficient of linear thermal expansion, T is temperature difference, δij is Kronecker delta. Then in the context of uncoupled linear thermoelasticity, the displacement-temperature equation of equilibrium in the absence of body forces can be written as ∇2u+ 1 1−2ν ∇(∇·u)= 2(1+ν) 1−2ν α∇T (2.2) where eij are components of the strain tensor; u is the displacement vector and ν is Poisson’s ratio. The uncoupled heat conduction equation for a steady state temperature field T with Q as the heat supply and λ0 as the thermal conductivity can be written as ∇2T = −Q λ0 (2.3) The solution to inhomogeneous equation (2.2) can be expressed as u=uc+up (2.4) whereuc is the complementary function satisfying the homogeneous equation of (2.2) andup re- presents the particular solution to the displacement field generated by the temperature field T . According to Goodier’s method (Timoshenko andGoodier, 1951), the displacement u(∞)(r) for an infinite solid is given by u(∞) = ∇ϕ, where the potential function ϕ satisfies Poisson’s equation ∇2ϕ= 1+ν 1−ν αT(r) (2.5) Then the function ϕ is obtained as ϕ(r) = −1 4π 1+ν 1−ν α ∫ T(r′) |r−r′| d3(r′) (2.6) where |r− r′| = |(x,y,z)− (ξ,η,ς)| = √ (x− ξ)2+(y−η)2+(z− ς)2 is the distance between the points (x,y,z) and (ξ,η,ς). Then the displacement, strain and stress components in the cylindrical polar coordinates (r,θ,z) are expressed in terms of the potential function ϕ as (Barber, 2002; Sadd, 2005) ur = ∂ϕ ∂r uθ = 1 r ∂ϕ ∂θ uz = ∂ϕ ∂z (2.7) and err = ∂ur ∂r eθθ = 1 r ( ur+ ∂uθ ∂θ ) erθ = 1 2 (1 r ∂ur ∂θ + ∂uθ ∂r − uθ r ) ezz = ∂uz ∂z eθz = 1 2 (∂uθ ∂z + 1 r ∂uz ∂θ ) ezr = 1 2 (∂ur ∂z + ∂uz ∂r ) (2.8) 1372 K. Singh, R. Muwal and 1 2µ σrr = ∂2ϕ ∂r2 −∇2ϕ 1 2µ σθθ = 1 r ∂ϕ ∂r + 1 r2 ∂2ϕ ∂θ2 −∇2ϕ 1 2µ σzz = ∂2ϕ ∂z2 −∇2ϕ 1 2µ σrθ = ∂ ∂r (1 r ∂ϕ ∂θ ) 1 2µ σθz = 1 r ∂2ϕ ∂θ∂z 1 2µ σzr = ∂2ϕ ∂z∂r (2.9) where the Laplacian operator in the cylindrical polar coordinates (r,θ,z) is given by ∇2ϕ= ( ∂2 ∂r2 + 1 r ∂ ∂r + 1 r2 ∂2 ∂θ2 + ∂2 ∂z2 ) ϕ (2.10) 3. Formulation and solution of the problem We consider an axisymmetric problem of a spherical inclusion in the upper half-space (z ­ 0) having a different coefficient of thermal expansion to that of the half-space but the same elastic constants as in Wang and Huang (1991). Due to this difference in the coefficients of thermal expansion between the sub region and its surrounding material, say η0, a thermoelastic stress field is generated. Let radius of the spherical inclusion be a and center of it be located at the point r=0 and z= h, where h>a, as shown in Fig. 1. The surface z =0 is taken as traction free surface. We take the axis of symmetry as the z axis, then for the axisymmetric problem in the cylindrical coordinates (r,θ,z), all quantities are independent of θ. Then using Eq. (2.7), the displacement vector u has the form u=(ur,0,uz). Therefore, the components of the strain and stress tensor can be written in the following form, see equations (2.8) and (2.9) err = ∂ur ∂r eθθ = u r ezz = ∂uz ∂z ezr = 1 2 (∂ur ∂z + ∂uz ∂r ) erθ =0 eθz =0 (3.1) and 1 2µ σrr = ∂2ϕ ∂r2 −∇2ϕ 1 2µ σθθ = 1 r ∂ϕ ∂r −∇2ϕ 1 2µ σzz = ∂2ϕ ∂z2 −∇2ϕ 1 2µ σzr = ∂2ϕ ∂z∂r σrθ =0 σθz =0 (3.2) where ∇2ϕ= ( ∂2 ∂r2 + 1 r ∂ ∂r + ∂2 ∂z2 ) ϕ (3.3) Fig. 1. A spherical inclusion in a thermoelastic half-space Thermoelastic strain and stress fields due to a spherical inclusion... 1373 Then according toWang and Huang (1991), the thermoelastic potential function ϕ satisfies the followingPoisson’s equations,when temperature of the semi-infinite region increases up toT0 ∇2ϕ=    1+ν 1−ν αT = 1+ν 1−ν η0T0 for R1 ¬ a 0 for R1 >a (3.4) whereR21 = r 2+(z−h)2 is the distance of the point (r,z) from (0,h). Then, the functionϕ for this problem is taken as (Wang and Huang 1991) ϕ=        1 6 KR21 for R1 ¬ a 1 6 K ( 3a2−2a 3 R1 ) for R1 >a (3.5) where K = 1+ν 1−ν η0T0 (3.6) Considering the boundary conditions, we assume that the boundary z=0 of the half-space is traction free surface i.e. σzz =σrz =0 at z=0 (3.7) Now according to Davies (2003), the strain and stress components within the semi-infinite region z ­ 0 with the traction free surface in terms of strain and stress components for an infinite region for the axisymmetric problem in the rz-plane can be reduced to the form err = e (∞) rr +(3−4ν)e (∞) rr +2z ∂ ∂z e(∞)rr eθθ = e (∞) θθ +(3−4ν)e (∞) θθ +2z ∂ ∂z e (∞) θθ ezz = e (∞) zz − (1−4ν)e (∞) zz +2z ∂ ∂z e(∞)zz erz = e (∞) rz −e (∞) rz −2z ∂ ∂z e(∞)rz erθ =0= eθz (3.8) and σrr =σ (∞) rr +(3−4ν)σ (∞) rr −4νσ (∞) zz +2z ∂ ∂z σ(∞)rr σθθ =σ (∞) θθ +(3−4ν)σ (∞) θθ −4νσ(∞)zz +2z ∂ ∂z σ (∞) θθ σrθ =0=σθz σzz =σ (∞) zz −σ (∞) zz +2z ∂ ∂z σ(∞)zz σrz =σ (∞) rz −σ (∞) rz −2z ∂ ∂z σ(∞)rz (3.9) Then the displacement, strain and stress fields in the infinite region and those at the image point for exterior points (R1 >a) of the spherical inclusion (where∇ 2ϕ=0) are obtained using u(∞) =∇ϕ and equations (3.1)-(3.3) u(∞)r = ∂ϕ ∂r = 1 3 Ka3 ( r R31 ) u (∞) θ = 1 r ∂ϕ ∂θ =0 u(∞)z = ∂ϕ ∂z = 1 3 Ka3 (z−h R31 ) (3.10) e(∞)rr = ∂2ϕ ∂r2 = 1 3 Ka3 ( 1 R31 − 3r2 R51 ) e (∞) θθ = ur r = 1 3 Ka3 ( 1 R31 ) e (∞) rθ = e (∞) θz =0 e(∞)zz = ∂2ϕ ∂z2 = 1 3 Ka3 ( 1 R31 − 3(z−h)2 R51 ) e(∞)rz = e (∞) zr = ∂2ϕ ∂r∂z =−Ka3 r(z−h) R51 (3.11) 1374 K. Singh, R. Muwal 1 2µ σ(∞)rr = 1 3 Ka3 ( 1 R31 − 3r2 R51 ) 1 2µ σ (∞) θθ = 1 3 Ka3 ( 1 R31 ) σ (∞) rθ =0=σ (∞) θz 1 2µ σ(∞)zz = 1 3 Ka3 ( 1 R31 − 3(z−h)2 R51 ) 1 2µ σ(∞)rz =−Ka 3r(z−h) R51 (3.12) u(∞)r = 1 3 Ka3 ( r R32 ) u (∞) θ =0 u(∞)z = −1 3 Ka3 (z+h R32 ) (3.13) e(∞)rr = 1 3 Ka3 ( 1 R32 − 3r2 R52 ) e (∞) θθ = 1 3 Ka3 ( 1 R32 ) e (∞) rθ = e (∞) θz =0 e(∞)zz = 1 3 Ka3 ( 1 R32 − 3(z+h)2 R52 ) e(∞)rz =Ka 3r(z+h) R52 (3.14) 1 2µ σ(∞)rr = 1 3 Ka3 ( 1 R32 − 3r2 R52 ) 1 2µ σ (∞) θθ = 1 3 Ka3 ( 1 R32 ) σ (∞) rθ =0=σ (∞) θz 1 2µ σ(∞)zz = 1 3 Ka3 ( 1 R32 − 3(z+h)2 R52 ) 1 2µ σ(∞)rz =Ka 3r(z+h) R52 (3.15) where (0,−h) is the image of point (0,h) and R22 = r 2 +(z+h)2 is the distance of the point (r,z) from (0,−h). Substituting equations (3.11), (3.14) and (3.12), (3.15) into (3.8) and (3.9), respectively, the strain and stress components in the thermoelastic half-space for exterior points (R1 >a) of the spherical inclusion can be expressed as err = 1 3 Ka3 [ 1 R31 + 3−4ν R32 − 6z(z+h) R52 −3r2 ( 1 R51 + 3−4ν R52 − 10z(z+h) R72 )] eθθ = 1 3 Ka3 ( 1 R31 + 3−4ν R32 − 6z(z+h) R52 ) ezz = 1 3 Ka3 ( 1 R31 − 1−4ν R32 − 18z(z+h) R52 − 3(z−h)2 R51 + 3(1−4ν)(z+h)2 R52 + 30z(z+h)3 R72 ) erz =−Ka 3r (z−h R51 + 3z+h R52 − 10z(z+h)2 R72 ) (3.16) and σrr =2µ Ka3 3 [ 1 R31 + 3−8ν R32 − 6z(z+h) R52 + 12ν(z+h)2 R52 −3r2 ( 1 R51 + 3−4ν R52 − 10z(z+h) R72 )] σθθ =2µ Ka3 3 ( 1 R31 + 3−8ν R32 − 6z(z+h) R52 + 12ν(z+h)2 R52 ) σzz =2µ Ka3 3 ( 1 R31 − 1 R32 − 18z(z+h) R52 − 3(z−h)2 R51 + 3(z+h)2 R52 + 30z(z+h)3 R72 ) σrz =−2µKa 3r (z−h R51 + 3z+h R52 − 10z(z+h)2 R72 ) (3.17) Further, from equation (3.17), we can see that σzz = σrz =0 at the boundary z =0 of the half-space, which is in accordance with the boundary conditions as in equation (3.7). Also, for the interior points (R1 ¬ a) of the spherical inclusion, as in Mindlin and Cheng (1950) uint =uext+ a3KR1 3 ( 1 a3 − 1 R31 ) (3.18) Thermoelastic strain and stress fields due to a spherical inclusion... 1375 Using this, the following relations between the strain components of the exterior points (R1 >a) and the interior points (R1 ¬ a) of the spherical inclusion are given by eintrr = e ext rr + Ka3 3 ( 1 a3 − 1 R31 ) +Ka3 r2 R51 eintθθ = e ext θθ + Ka3 3 ( 1 a3 − 1 R31 ) eintzz = e ext zz + Ka3 3 ( 1 a3 − 1 R31 ) +Ka3 (z−h)2 R51 eintrz = e ext rz +Ka 3r(z−h) R51 (3.19) Also, the relations between the stress components of the exterior points (R1 > a) and the interior points (R1 ¬ a) of the spherical inclusion are given below, seeGuell andDundurs (1967) σintrr =σ ext rr −2µK ( 2 a3 + 1 R31 − 3r2 R51 ) σintθθ =σ ext θθ −2µK ( 2 a3 + 1 R31 ) σintzz =σ ext zz −2µK ( 2 a3 + 1 R31 − 3(z−h)2 R51 ) σintrz =σ ext rz +6µK r(z−h) R51 (3.20) Substituting equations (3.16) and (3.17) into (3.19) and (3.20), respectively, the strain and stress components in the thermoelastic half-space for the interior points (R1 ¬ a) of the spherical inclusion can be expressed as err = 1 3 Ka3 [ 1 a3 + 3−4ν R32 − 6z(z+h) R52 −3r2 (3−4ν R52 − 10z(z+h) R72 )] eθθ = 1 3 Ka3 ( 1 a3 + 3−4ν R32 − 6z(z+h) R52 ) ezz = 1 3 Ka3 ( 1 a3 − 1−4ν R32 − 18z(z+h) R52 + 3(1−4ν)(z+h)2 R52 + 30z(z+h)3 R72 ) erz =−Ka 3r (3z+h R52 − 10z(z+h)2 R72 ) (3.21) and σrr =2µ Ka3 3 [−2 a3 + 3−8ν R32 − 6z(z+h) R52 + 12ν(z+h)2 R52 −3r2 (3−4ν R52 − 10z(z+h) R72 )] σθθ =2µ Ka3 3 (−2 a3 + 3−8ν R32 − 6z(z+h) R52 + 12ν(z+h)2 R52 ) σzz =2µ Ka3 3 (−2 a3 − 1 R32 − 18z(z+h) R52 + 3(z+h)2 R52 + 30z(z+h)3 R72 ) σrz =−2µKa 3r (3z+h R52 − 10z(z+h)2 R72 ) (3.22) The results obtained above are in good agreement to those of Mindlin and Cheng (1950) for the spherical inclusion in the interior of a thermoelastic semi-infinite solid using the usual thermoelastic relation. 4. Numerical results and discussion In this Section, graphical representations of the strain and stress components at the points (0,0) and (0,h− a) just outside the spherical inclusion in the thermoelastic half-space are obtained using MATLAB software programming. The numerical computations are carried out for Poisson’s ratios ν = 0.1 to 0.5. Figures 2a and 2b respectively show the variation of strain 1376 K. Singh, R. Muwal components err(= eθθ) and ezz at the point (0,0) for exterior points of the spherical inclusion along the distance and varyingPoisson’s ratio from 0.1 to 0.5. FromFig. 2a, we observe that the strain err(= eθθ) decreases smoothly with increasing values of the distance h/a, and it vanishes at infinitely large values of h/a. Also, as Poisson’s ratio ν increases from 0.1 to 0.5, this strain increases quantitatively. From Fig. 2b, we observe that the strain ezz assumes negative values for all the values of Poisson’s ratio ν ranging from 0.1 to 0.5. Further, it continuously increases with the increasing distance h/a assuming the value of zero at infinitely large values of h/a. In Figs. 3a and 3b, respectively, the variation of strain components err(= eθθ) and ezz at the point (0,h−a) just outside the spherical inclusion are presented for exterior points. From Fig. 3b, it can be seen that the strain ezz first increases and thendecreases continuously as the distanceh/a increases. Further, this strain approaches a finite negative value (depending on Poisson’s ratio) at infinitely large values of the distance h/a. Fig. 2. (a) Strain component err(= eθθ) at the point (0,0) for exterior points of the spherical inclusion, (b) strain component ezz atthe point (0,0) for exterior points of the spherical inclusion Fig. 3. (a) Strain component err(= eθθ) at the point (0,h−a) just outside the spherical inclusion for exterior points, (b) strain component ezz at the point (0,h−a) just outside the spherical inclusion for exterior points Figure 4 shows thevariation of the stress componentσrr(=σθθ) at thepoint (0,0) for exterior points of the spherical inclusion in the thermoelastic half-space. FromFig. 4, we observe that the stress component σrr(= σθθ) decreases gradually as the distance h/a increases and it vanishes at infinitely large of h/a. Also, as Poisson’s ratio ν increases from 0.1 to 0.5, this stress increases Thermoelastic strain and stress fields due to a spherical inclusion... 1377 quantitatively as shown in the figure. Figures 5a and 5b, respectively, show the variation of the stress component σrr(= σθθ) and σzz at the point (0,h−a) just outside the spherical inclusion in the thermoelastic half-space. From Fig. 5a, we observe that the stress component σrr(=σθθ) also decreases gradually with the increasing distance h/a but it assumes finite positive values (depending on Poisson’s ratio) at infinitely large values of the distance h/a. From Fig. 5b, we observe that as Poisson’s ratio increases from 0.1 to 0.5, the stress decreases more rapidly with increasing values of the distance h/a and tends to finite negative values (depending on Poisson’s ratio) at infinitely large values of the distance h/a. Fig. 4. Stress component σrr(=σθθ) at the point (0,0) for exterior points of the spherical inclusion Fig. 5. (a) Stress component σrr(=σθθ) at the point (0,h−a) just outside the spherical inclusion for exterior points, (b) stress component σzz at the point (0,h−a) just outside a spherical inclusion for exterior points Figures 6a and 6b, respectively, show the variation of strain components err(= eθθ) and ezz at the point (0,h) for interior points of the spherical inclusion. As observed from Fig. 6a, the strain err(= eθθ) increases continuously with the increasing distance h/a and with increasing values of Poisson’s ratio ν from0.1 to 0.5. FromFig. 6b, we observe that the strain ezz decreases gradually for all values ofPoisson’s ratio ν =0.1 to 0.5 as thedistanceh/a increases. It is noticed from Figs. 6a and 6b that these strains assume finite positive values (depending on Poisson’s ratio) at infinitely large values of the distance h/a. Figures 7a and 7b, respectively, show the variation of stress components σrr(= σθθ) and σzz at the point (0,h) for interior points of the spherical inclusion. It is noticed from Figs. 7a and 7b that the stresses decrease continuously 1378 K. Singh, R. Muwal as the distance h/a increases and these assume finite negative values (depending on Poisson’s ratio) at infinitely large values of distance h/a. Fig. 6. (a) Strain component err(= eθθ) at the point (0,h) for interior points of the spherical inclusion, (b) strain component ezz at the point (0,h) for interior points of the spherical inclusion Fig. 7. (a) Stress component σrr(=σθθ) at the point (0,h) for interior points of the spherical inclusion, (b) stress component σzz at the point (0,h) for interior points of the spherical inclusion 5. Conclusion In this paper, closed form analytical expressions for thermoelastic strain and stress components due to a spherical inclusion in a thermoelastic half-space are obtained. These expressions are derived in axisymmetric cylindrical coordinates in the context of steady-state uncoupled ther- moelasticity using thermoelastic displacement potential functions. The thermoelastic strain and stress components for the exterior points of the spherical inclusion are the same as those of the center of dilatation. The variations of the thermoelastic strain and stress components for the exterior and interior points of the spherical inclusion are also shown graphically for different values of Poisson’s ratios. It is observed that the strain and stress components at the points (0,h−a) and (0,h) approach finite values depending on Poisson’s ratio at infinitely large values of the distance h/a, whereas at the point (0,0) these quantities tend to zero as h/a tends to infinity. Thus, Poisson’s ratio has a significant effect on the strain and stress components due to the spherical inclusion in the thermoelastic half-space. Thermoelastic strain and stress fields due to a spherical inclusion... 1379 Acknowledgement We are thankful to the University Grants Commission, New Delhi, for financial support. We also thank the reviewer for useful suggestions in the improvement of our paper. References 1. Barber J.R., 2002,Elasticity, Second Edition, Kluwer Academic Publishers, Dordrecht 2. 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