<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">ENG</journal-id><journal-title-group><journal-title>Engineering</journal-title></journal-title-group><issn pub-type="epub">1947-3931</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/eng.2011.36074</article-id><article-id pub-id-type="publisher-id">ENG-5343</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject></subj-group></article-categories><title-group><article-title>
 
 
  Fibre-Reinforced Generalized Thermoelastic Medium under Hydrostatic Initial Stress
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>raveen</surname><given-names>Ailawalia</given-names></name><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Shilpy</surname><given-names>Budhiraja</given-names></name><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><author-notes><corresp id="cor1">* E-mail:<email>praveen_2117@rediffmail.com(RA)</email>;<email>shilpy.budhiraja@gmail.com(SB)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>23</day><month>06</month><year>2011</year></pub-date><volume>03</volume><issue>06</issue><fpage>622</fpage><lpage>631</lpage><history><date date-type="received"><day>February</day>	<month>22,</month>	<year>2011</year></date><date date-type="rev-recd"><day>June</day>	<month>1,</month>	<year>2011</year>	</date><date date-type="accepted"><day>June</day>	<month>10,</month>	<year>2011</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  The present problem is concerned with the deformation of an infinite fibre-reinforced generalized thermoe-lastic medium with hydrostatic initial stress under the influence of mechanical force. The normal mode analysis is used to obtain the analytical expressions of the displacement components, force stress and temperature distribution. The numerical results are given and presented graphically for Green -Lindsay [4] theory of thermoelasticity. Comparisons are made in the presence and absence of hydrostatic initial stress and anisotropy.
 
</p></abstract><kwd-group><kwd>Generalized Thermoelastic</kwd><kwd> Hydrostatic Initial Stress</kwd><kwd> Fibre-Reinforced</kwd><kwd> Temperature 
Distribution</kwd><kwd> Normal Mode</kwd><kwd> Anisotropy</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The classical theories of thermo-elasticity involving infinite speed of propagation of thermal signals, contradict physical facts. During the last three decades, nonclassical theories involving finite speed of heat transportation in elastic solids have been developed to remove this paradox. In contrast to the conventional coupled thermo-elasticity theory which involves a parabolic-type heat transport equation, these generalized theories involving a hyperbolic-type heat transport equation are supported by experiments exhibiting the actual occurrence of wave-type heat transport in solids, called sound effect. The extended thermo-elasticity theory proposed by Lord and Shulman [<xref ref-type="bibr" rid="scirp.5343-ref2">2</xref>] incorporates a flux-rate term into Fourier’s law of heat conduction, and formulates a generalized form that involves a hyperbolic-type heat equation admitting finite speed of thermal signals. Muller [<xref ref-type="bibr" rid="scirp.5343-ref3">3</xref>] in a review of the thermodynamics of a thermoelastic solid, proposed an entropy production inequality, with the help of which he considered restrictions on a class of constitutive equations. A generalization of this inequality was proposed by Green and Laws [<xref ref-type="bibr" rid="scirp.5343-ref4">4</xref>]. Green and Lindsay [<xref ref-type="bibr" rid="scirp.5343-ref4">4</xref>] developed temperaturetype-dependent thermo-elasticity (TRDTE) theory by introducing relaxation time factors that does not violate the classical Fourier’s law of heat conduction and this theory also predicts a finite speed for heat propagation.</p><p>Barber [<xref ref-type="bibr" rid="scirp.5343-ref5">5</xref>] studied thermoelastic displacements and stresses due to a heat source moving over the surface of a half plane. Sherief [<xref ref-type="bibr" rid="scirp.5343-ref6">6</xref>] obtained components of stress and temperature distributions in a thermoelastic medium due to a continuous source. Dhaliwal et al. [<xref ref-type="bibr" rid="scirp.5343-ref7">7</xref>] investigated thermoelastic interactions caused by a continuous line heat source in a homogeneous isotropic unbounded solid. Chandrasekharaiah and Srinath [<xref ref-type="bibr" rid="scirp.5343-ref8">8</xref>] studied thermoelastic interactions due to a continous point heat source in a homogeneous and isotropic unbounded body. Sharma et al. [<xref ref-type="bibr" rid="scirp.5343-ref9">9</xref>] investigated the disturbance due to a time-harmonic normal point load in a homogeneous isotropic thermoelastic half-space. Sharma and Chauhan [<xref ref-type="bibr" rid="scirp.5343-ref10">10</xref>] discussed mechanical and thermal sources in a generalized thermoelastic half-space. Sharma et al. [<xref ref-type="bibr" rid="scirp.5343-ref11">11</xref>] investigated the steady-state response of an applied load moving with constant speed for infinite long time over the top surface of a homogeneous thermoelastic layer lying over an infinite half-space. Deswal and Choudhary [<xref ref-type="bibr" rid="scirp.5343-ref12">12</xref>] studied a two-dimensional problem due to moving load in generalized thermoelastic solid with diffusion.</p><p>Fibre-reinforced composites are used in a variety of structures due to their low weight and high strength. A continuum model is used to explain the mechanical properties of such materials. In the case of an elastic solid reinforced by a series of parallel fibres it is usual to assume transverse isotropy. In the linear case, the associated constitutive relations, relating infinitesimal stress and strain components, have five materials constants. The analysis of stress and deformation of fibrereinforced composite materials has been an important subject of solid mechanics for last three decades. Pipkin [<xref ref-type="bibr" rid="scirp.5343-ref13">13</xref>] and Rogers [14,15] did pioneer works on the subject. Craig and Hart [<xref ref-type="bibr" rid="scirp.5343-ref16">16</xref>] studied the stress boundary-value problem for finite plane deformation of a fibre-reinforced material. Sengupta and Nath [<xref ref-type="bibr" rid="scirp.5343-ref17">17</xref>] discussed the problem of surface waves in a fibre-reinforced anisotropic elastic media.. Singh and Singh [<xref ref-type="bibr" rid="scirp.5343-ref18">18</xref>] discussed the reflection of plane waves at the free surface of a fibre-reinforced elastic half-space. Singh [<xref ref-type="bibr" rid="scirp.5343-ref19">19</xref>] discussed the wave propagation in an incompressible transversely isotropic fibrereinforced elastic media. Singh [<xref ref-type="bibr" rid="scirp.5343-ref20">20</xref>] studied the effects of anisotropy on reflection coefficients of plane waves in fibre-reinforced thermoe-lastic solid. Kumar and Gupta [<xref ref-type="bibr" rid="scirp.5343-ref21">21</xref>] investigated a source problem in fibre-reinforced anisotropic generalized thermo-elastic solid under acoustic fluid layer.</p><p>The development of initial stresses in the medium is due to many reasons, for example, resulting from differences of temperature, process of quenching, shot pinning and cold working, slow process of creep, differential external forces, gravity variations, etc. The earth is assumed to be under high initial stresses. It is, therefore, of much interest to study the influence of these stresses on the propagation of stress waves. Biot [<xref ref-type="bibr" rid="scirp.5343-ref22">22</xref>] showed the acoustic propagation under initial stress, which is fundamentally different from that under a stress-free state. He has obtained the velocities of longitudinal and transverse waves along the co-ordinates axis only.</p><p>The wave propagation in solids under initial stresses has been studied by many authors for various models. The study of reflection and refraction phenomena of plane waves in an unbounded medium under initial stresses is due to Chattopadhyay et al. [<xref ref-type="bibr" rid="scirp.5343-ref23">23</xref>], Sidhu and Singh [<xref ref-type="bibr" rid="scirp.5343-ref24">24</xref>] and Dey et al. [<xref ref-type="bibr" rid="scirp.5343-ref25">25</xref>]. Montanaro [<xref ref-type="bibr" rid="scirp.5343-ref26">26</xref>] investigated the isotropic linear thermoelasticity with hydrostatic initial stress. Singh et al. [<xref ref-type="bibr" rid="scirp.5343-ref27">27</xref>], Singh [<xref ref-type="bibr" rid="scirp.5343-ref28">28</xref>] and Othman and Song [<xref ref-type="bibr" rid="scirp.5343-ref29">29</xref>] studied the reflection of thermoelastic waves from a free surface under a hydrostatic initial stress in the context of different theories of generalized thermoelasticity. Ailawalia et al. [<xref ref-type="bibr" rid="scirp.5343-ref30">30</xref>] investigated deformation in a generalized thermoelastic medium with hydrostatic initial stress. Ailawalia [<xref ref-type="bibr" rid="scirp.5343-ref31">31</xref>] obtained the components of displacement, stresses, temperature distribution of thermoelastic solid half-space under hydrostatic initial stress subjected to ramp-type heating and loading for G-N theory (type III).</p><p>The present paper is concerned with the investigations related to effect of hydrostatic initial stress in fibrereinforced generalized thermoelastic medium. Effects of hydrostatic initial stress and anisotropy are shown graphically on normal displacement, normal force stress and temperature distribution for Green-Lindsay [<xref ref-type="bibr" rid="scirp.5343-ref1">1</xref>] theory of thermoelasticity.</p></sec><sec id="s2"><title>2. Basic Equations and Their Solutions</title><p>We consider a homogeneous thermally conducting transversely fibre-reinforced medium with hydros-tatic initial stress of infinite extent with cartesian coordinates system<img src="9-8101378\0c9be6ff-bc99-411d-a54d-1c5c5fed8c49.jpg" />. To analyze the displacement components, stresses and temperature distribution at the interior of the medium, the continuum is divided into two half spaces defined by</p><p>1) half space I<img src="9-8101378\f226db18-a578-4926-a27c-41587f50f997.jpg" />, <img src="9-8101378\e5f67f7e-8eb6-4cee-8c10-cb716ac407a4.jpg" />, <img src="9-8101378\9d5b4580-7343-42d8-852b-1485cf1dfded.jpg" /></p><p>2) half space II<img src="9-8101378\4aab2599-2bc3-416a-8774-6526d55ad24a.jpg" />, <img src="9-8101378\ec9eca69-d2ee-40cc-a3b1-9f7d721e9ce5.jpg" />, <img src="9-8101378\ecb9cab1-71af-42c1-a79c-ac720edd81ad.jpg" /></p><p>if we restrict our analysis to the plane strain parallel to <img src="9-8101378\24e4161d-a58f-45f8-b465-b0ba55ced44f.jpg" />-plane with displacement vector<img src="9-8101378\2e39b75d-4483-470c-9912-c411eb6104ce.jpg" />, then the field equations and constitutive relations for such a medium in the absence of body forces and heat sources are written as,</p><disp-formula id="scirp.5343-formula154295"><label>(1)</label><graphic position="anchor" xlink:href="9-8101378\d9f5af87-58c6-490e-adbc-ead24f425398.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154296"><label>(2)</label><graphic position="anchor" xlink:href="9-8101378\57556a0d-4c8b-4d03-bdf9-a8b27f961155.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154297"><label>(3)</label><graphic position="anchor" xlink:href="9-8101378\0529dbf0-ff99-4cc2-8adb-e5af2d786490.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154298"><label>(4)</label><graphic position="anchor" xlink:href="9-8101378\d300596a-393b-4a9c-bab8-e5302df370ae.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154299"><label>(5)</label><graphic position="anchor" xlink:href="9-8101378\d28065ca-6438-4a53-8e87-7b6188cb1c89.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154300"><label>(6)</label><graphic position="anchor" xlink:href="9-8101378\fd4f9b32-485b-4fc9-ae50-4f24ab79eb02.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154301"><label>(7)</label><graphic position="anchor" xlink:href="9-8101378\a83c3c91-de9b-4b57-afa9-12e34815123e.jpg"  xlink:type="simple"/></disp-formula><p>where</p><p><img src="9-8101378\e64d200d-7e79-4918-a12f-f46574072489.jpg" /></p><p>and <img src="9-8101378\910c1389-968c-4fca-a520-68daed9b1ecd.jpg" /> are material constants, <img src="9-8101378\2480f372-3067-4327-a2ee-53734e9dbb57.jpg" />are coefficients of thermal conductivity, <img src="9-8101378\7ee2c6d7-0793-43b3-b714-41478b250915.jpg" />are coefficients of linear expansion, <img src="9-8101378\0ce5c4de-9a1c-404c-a80a-716a9539f8f2.jpg" />are thermal relaxation times, <img src="9-8101378\ba8cb7de-1c51-47b1-9ce9-b5811fd7345e.jpg" />are the components of displacement vector, <img src="9-8101378\8fdfbd19-6dbe-4feb-bd53-abed0e017ff9.jpg" />is the the mass density, <img src="9-8101378\e87fb783-5950-458f-8954-59a75d4fb2f0.jpg" />is the temperature change of a material particle, <img src="9-8101378\257f3788-0cd2-4050-8147-814bfb6b7654.jpg" />is the reference uniform temperature of the body and <img src="9-8101378\91cade8c-7a4d-4789-930f-9010c541293b.jpg" /> is the specific heat at constant strain.</p><p>For simplification, we shall use the following nondimensional variables</p><p><img src="9-8101378\f8346fb3-c3a8-4b35-8dc5-91c09b503082.jpg" /><img src="9-8101378\aa5c1217-9211-4b75-a779-2966ce9b2f09.jpg" />(8)</p><p>where</p><p><img src="9-8101378\c4574a8c-47df-443f-b668-70241cbd4cec.jpg" /></p><p>Substituting non-dimensional variables into Equations (1)-(3), we obtain (after dropping the primes)</p><disp-formula id="scirp.5343-formula154302"><label>(9)</label><graphic position="anchor" xlink:href="9-8101378\36e731d2-0596-4eb1-8762-17fe656f84b6.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154303"><label>(10)</label><graphic position="anchor" xlink:href="9-8101378\505bfc25-8234-480f-b13a-8088d4c3570a.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154304"><label>(11)</label><graphic position="anchor" xlink:href="9-8101378\c86dc1d8-2411-42f6-a51d-e4e162e0f3fc.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s3"><title>3. Normal Mode Analysis</title><p>The solution of the considered physical variable can be decomposed in terms of normal modes as the following form</p><disp-formula id="scirp.5343-formula154305"><label>(12)</label><graphic position="anchor" xlink:href="9-8101378\c4b22fa3-7f50-40d7-bd2e-3549cb3604a2.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="9-8101378\2d857748-9efc-497e-83d9-77b443650c33.jpg" /> is the complex time constant and <img src="9-8101378\8706b78b-b8c6-4274-9626-5f1d56b2dae8.jpg" /> is the wave number in <img src="9-8101378\3a6c0505-f313-4257-8e4f-e47f2d017089.jpg" />-direction.</p><p>Using (12), Equations (9)-(11) take the form</p><disp-formula id="scirp.5343-formula154306"><label>(13)</label><graphic position="anchor" xlink:href="9-8101378\64feae94-9daf-447c-8acb-f0330941e2f5.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154307"><label>(14)</label><graphic position="anchor" xlink:href="9-8101378\b1fa05c6-bbb4-4962-bcad-a21d48e2a99f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154308"><label>(15)</label><graphic position="anchor" xlink:href="9-8101378\3a7bc4d2-2378-46e9-9fc2-d609c0358f05.jpg"  xlink:type="simple"/></disp-formula><p>where</p><p><img src="9-8101378\b2a36341-7851-48d0-bcfa-0033a8021953.jpg" /><img src="9-8101378\ee7721a2-6ead-4b9a-978b-af46b00fe24f.jpg" /> (16)</p><p>Eliminating <img src="9-8101378\ab964775-a300-4eca-8c00-d2af3c4f5417.jpg" /> and <img src="9-8101378\77a7faf0-f991-4c94-826c-9c800d79abbf.jpg" /> from Equations (13)-(15), we obtain</p><disp-formula id="scirp.5343-formula154309"><label>(17)</label><graphic position="anchor" xlink:href="9-8101378\92dd2945-92e2-4bb9-b66f-3ddf62cf3266.jpg"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.5343-formula154310"><label>(18)</label><graphic position="anchor" xlink:href="9-8101378\68469c09-97d8-441a-b80a-605447856b89.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154311"><label>(19)</label><graphic position="anchor" xlink:href="9-8101378\865c5857-7b02-4765-b163-e9a7c9a5c92d.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154312"><label>(20)</label><graphic position="anchor" xlink:href="9-8101378\863fb904-e055-43ae-92ac-a149a4bfdc2f.jpg"  xlink:type="simple"/></disp-formula><p><img src="9-8101378\c6acd2e7-8012-4cef-8fd3-8ee1d58dba4a.jpg" /></p><disp-formula id="scirp.5343-formula154313"><label>(21)</label><graphic position="anchor" xlink:href="9-8101378\2f0111f7-0324-412f-adba-6c4af5fd01b6.jpg"  xlink:type="simple"/></disp-formula><p>The solution of Equation (17) has the form</p><disp-formula id="scirp.5343-formula154314"><label>(22)</label><graphic position="anchor" xlink:href="9-8101378\4ed54927-6226-46c5-8e21-b1a09f294217.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154315"><label>(23)</label><graphic position="anchor" xlink:href="9-8101378\f1f3fecd-8c90-4304-9f0d-971d2ac8afbb.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154316"><label>(24)</label><graphic position="anchor" xlink:href="9-8101378\7cf2929a-541c-47a3-8404-88b138f034f7.jpg"  xlink:type="simple"/></disp-formula><p>where<img src="9-8101378\9884eedd-5ae8-480c-8ff7-f507b29fd801.jpg" />, <img src="9-8101378\de917511-8cd0-40df-9f78-dd5ac972e104.jpg" />are some parameters depending on <img src="9-8101378\0e9511ed-747a-4103-b2ed-6f8e3483bdeb.jpg" /> and<img src="9-8101378\5aff7f8e-6b5b-4fd4-8470-e43d735c7648.jpg" />. <img src="9-8101378\1a83b1f9-9fb9-4ca4-9955-f685933e56ee.jpg" />are the roots of the characteristic equation (17).</p><p>Substituting from Equations (22)-(24) into (13)-(15), we obtain the following relations</p><disp-formula id="scirp.5343-formula154317"><label>(25)</label><graphic position="anchor" xlink:href="9-8101378\7e424f34-0400-4b4d-8da9-cdb1d50ef87e.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154318"><label>(26)</label><graphic position="anchor" xlink:href="9-8101378\4516e435-0bb1-42c7-bdd7-2e4da3b2148b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154319"><label>(27)</label><graphic position="anchor" xlink:href="9-8101378\160ffd11-40f2-4be0-8b65-2b1da7b5c7f5.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154320"><label>(28)</label><graphic position="anchor" xlink:href="9-8101378\180790ad-ebbe-4ad9-8426-ae2fffdeffae.jpg"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.5343-formula154321"><label>(29)</label><graphic position="anchor" xlink:href="9-8101378\d9e74fc7-60bc-48d5-9bd8-762a3a0b9f16.jpg"  xlink:type="simple"/></disp-formula><p>Thus the solution of Equations (1)-(3) are</p><disp-formula id="scirp.5343-formula154322"><label>(30)</label><graphic position="anchor" xlink:href="9-8101378\1e248440-25bd-4a12-a40b-3916c64dfa90.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154323"><label>(31)</label><graphic position="anchor" xlink:href="9-8101378\9027c402-2969-4397-9eae-ceb553ea7950.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154324"><label>(32)</label><graphic position="anchor" xlink:href="9-8101378\acf7da4f-f19f-4771-8598-a4a40d108ec3.jpg"  xlink:type="simple"/></disp-formula><p>Normal mode analysis of the stress yields the following,</p><disp-formula id="scirp.5343-formula154325"><label>(33)</label><graphic position="anchor" xlink:href="9-8101378\01cd9be0-fe2c-4bfa-ad05-04ca2bd60774.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154326"><label>(34)</label><graphic position="anchor" xlink:href="9-8101378\86b8b9a0-a3d8-41a2-97ea-ce9b37552542.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154327"><label>(35)</label><graphic position="anchor" xlink:href="9-8101378\6e72adba-37db-456f-b8bb-498546c1f631.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154328"><label>(36)</label><graphic position="anchor" xlink:href="9-8101378\10ca2eed-51b4-4ce6-a4ad-2ad5c3d83815.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. Boundary Conditions</title><p>In order to determine the parameters <img src="9-8101378\128bc5e2-02ef-485d-a15b-f99414ac7eb0.jpg" /> and<img src="9-8101378\8500b1e6-e9a5-4de3-9bc6-01d9e8ef5c82.jpg" />, we consider the following boundary conditions at <img src="9-8101378\56b7d8ad-1b18-4fde-8ad8-76ef7f09eecf.jpg" /></p><disp-formula id="scirp.5343-formula154329"><label>(37)</label><graphic position="anchor" xlink:href="9-8101378\33cee489-007d-4782-934f-c534a08c8fca.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="9-8101378\eccf7352-8709-47b3-ac0a-6542a4892ef4.jpg" /> is the magnitude of mechanical force.</p><p>Using Equations (30)-(34) in boundary condition (37), we get six equations with six unknown parameters <img src="9-8101378\ca5a28ae-26d0-4230-b437-8c8a8f29b4b4.jpg" /> and <img src="9-8101378\b57219da-c0ec-499b-9447-3d71af12fe5e.jpg" /> as</p><disp-formula id="scirp.5343-formula154330"><label>(38)</label><graphic position="anchor" xlink:href="9-8101378\a93648dc-f476-48fe-9d6a-64946d7b306b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154331"><label>(39)</label><graphic position="anchor" xlink:href="9-8101378\df307e7b-75f9-4e94-a0bc-28f6c030fd9e.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154332"><label>(40)</label><graphic position="anchor" xlink:href="9-8101378\7fa013ad-2737-494d-99b2-c3a36a2efce7.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154333"><label>(41)</label><graphic position="anchor" xlink:href="9-8101378\407bc780-6048-48f6-b216-130d58fb8908.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154334"><label>(42)</label><graphic position="anchor" xlink:href="9-8101378\6b611ec6-3524-4f43-8a8b-e0bbd4caeaef.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.5343-formula154335"><label>(43)</label><graphic position="anchor" xlink:href="9-8101378\56bc3c06-f61a-42c5-8ce7-fd39b5e79a78.jpg"  xlink:type="simple"/></disp-formula><p>Solving equations (38)-(43), the parameters <img src="9-8101378\81f9d059-5e29-4c79-8a3a-94baab27a86d.jpg" /> and <img src="9-8101378\053e524d-77de-4d0d-bccc-6f1e22ef6bdd.jpg" />are derived as follows:</p><p><img src="9-8101378\1de8efd7-dbd9-4713-af0f-14c6f892df5c.jpg" /></p><p>where <img src="9-8101378\24eca160-d5a8-4745-8b14-abd2010672ce.jpg" /> are defined in the appendix.</p></sec><sec id="s5"><title>5. Particular Cases</title><sec id="s5_1"><title>5.1. Isotropic Generalized Thermoelastic Medium with Hydrostatic Initial Stress</title><p>Substituting<img src="9-8101378\a0b0fc00-1aca-43ba-a951-d1d8f99a832a.jpg" />, <img src="9-8101378\fc13c864-56ef-4d22-9224-b0b0814a9513.jpg" />, <img src="9-8101378\c475cc5a-3d92-4796-ba9d-0fe71fd900c8.jpg" /> and<img src="9-8101378\cf688da3-f3da-4069-b239-a2d3c4109e48.jpg" />, <img src="9-8101378\1075f36b-a502-47e9-8173-d264771c92b8.jpg" />in Equations (30)-(36), we obtain the corresponding expressions of displacement, stress, and temperature distribution in isotropic generalized thermoelastic medium with hydrostatic initial stress.</p></sec><sec id="s5_2"><title>5.2. Fibre-Reinforced Generalized Thermoelastic Medium</title><p>Letting<img src="9-8101378\1bc31dc2-d949-4f2f-86c3-cdabc4977ab8.jpg" />, the expressions (30)-(36) reduce to the case of fibre-reinforced generalized thermoelastic medium.</p></sec><sec id="s5_3"><title>5.3. Isotropic Generalized Thermoelastic Medium</title><p>Substituting<img src="9-8101378\b34a56d9-b0ff-4de7-a26c-b6202807af4a.jpg" />, <img src="9-8101378\bc152675-48d5-4789-b999-925487cacdd9.jpg" />, <img src="9-8101378\058ea37d-5a39-429e-a5cc-f28057d14302.jpg" /> and<img src="9-8101378\240c1392-0ee4-42d9-8832-d952adcdf390.jpg" />, <img src="9-8101378\a45028bd-d71c-430d-b443-0f51096dd034.jpg" />and letting<img src="9-8101378\8991ab63-ace8-4642-9607-ed1dd68f7e2a.jpg" />, the expressions (30)-(36) reduce to an isotropic generalized thermoelastic medium.</p><p>For all the cases discussed above the components of displacement, stresses and temperature distribution for the region<img src="9-8101378\6b199ec9-f81e-4172-9f62-f00b7b1170ba.jpg" />, are obtained by inserting <img src="9-8101378\531ba667-e084-42d5-8abf-d06254c40aa8.jpg" /> in Equations (30)-(36).</p><p>Similarly in the region<img src="9-8101378\182beb87-daa4-450d-b2cf-99420c08b4f8.jpg" />, the components are obtained by inserting <img src="9-8101378\5f75a6ff-4f44-4b7b-9368-115ed0dec0e8.jpg" /> in Equations (30)-(36).</p></sec></sec><sec id="s6"><title>6. Special Cases of Thermoelastic Theory</title><sec id="s6_1"><title>6.1. Equation of Coupled Thermoelasticity</title><p>The equations of the coupled thermoelasticity (C-T theory) are obtained when</p><disp-formula id="scirp.5343-formula154336"><label>(44)</label><graphic position="anchor" xlink:href="9-8101378\6c528902-0742-4b37-9c65-347d84f1cdbf.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s6_2"><title>6.2. Lord-Shulman Theory</title><p>For the Lord-Shulman (L-S theory)</p><disp-formula id="scirp.5343-formula154337"><label>(45)</label><graphic position="anchor" xlink:href="9-8101378\09b86b96-a78e-434e-a5c9-cc35e7022952.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s6_3"><title>6.3. Green-Lindsay Theory</title><p>For Green-Lindsay(G-L theory),</p><disp-formula id="scirp.5343-formula154338"><label>(46)</label><graphic position="anchor" xlink:href="9-8101378\76e9cb6b-1f3a-4d54-aa53-69423d6204b0.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="9-8101378\c9f7688b-1e14-4dab-a38c-a8e2a8501102.jpg" /> are the two relaxation times.</p></sec><sec id="s6_4"><title>6.4. Equations of Generalized Thermoelasticity</title><p>The equations of the generalized thermoelasticity without energy dissipation (the linearized G-N theory of type II ) are obtained when</p><disp-formula id="scirp.5343-formula154339"><label>(47)</label><graphic position="anchor" xlink:href="9-8101378\a89cd48a-af9c-49b8-acf1-ad8f997d4034.jpg"  xlink:type="simple"/></disp-formula><p>Equations (1) and (2) are the same and equation (3) takes the form</p><disp-formula id="scirp.5343-formula154340"><label>(48)</label><graphic position="anchor" xlink:href="9-8101378\cd38946d-d1b6-48e3-8631-242564874444.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="9-8101378\6f7ec68a-22fe-4449-8556-985a76e39be9.jpg" /> is constant with the dimension of <img src="9-8101378\c95a64d4-1a01-4920-8918-2326f3c104b5.jpg" /> and <img src="9-8101378\a526c204-9017-4f48-be1b-d44d613f7d08.jpg" />are characteristic constants of this theory.</p></sec></sec><sec id="s7"><title>7. Numerical Results</title><p>With a view to illustrating the analytical procedure presented earlier, we now consider a numerical example for which computational results are given. The results depict the variations of normal displacement, normal force stress and temperature distribution in the context of G-L theory. For this purpose, we take the following values of physical constants as Singh [<xref ref-type="bibr" rid="scirp.5343-ref20">20</xref>]</p><p><img src="9-8101378\bf114bf1-7c6d-4b0f-a2b5-9dda273c6667.jpg" /></p><p><img src="9-8101378\743fcb33-0b98-4049-8e55-e915325ca48b.jpg" /></p><p><img src="9-8101378\8e6a49c9-7f4b-4256-bcbc-c4eb63219133.jpg" /></p><p><img src="9-8101378\46f28cc3-b37f-4530-b98d-badaecedb3cc.jpg" /></p><p>The computations are carried out on the surface <img src="9-8101378\b3d8d0cb-89b2-4247-8d60-8e4b5a7b3970.jpg" /> at<img src="9-8101378\7c1ba6a7-f317-405c-a26c-2eddd6eb2892.jpg" />. The graphical results for normal displacement<img src="9-8101378\24b20309-b6b9-4439-8a6a-54b3fdd9c390.jpg" />, normal force stress <img src="9-8101378\0cb6ab13-23ae-4308-976a-2c5f8970a5d1.jpg" /> and temperature distribution <img src="9-8101378\1bda6f2e-9fa8-4fd8-a629-df9fd232f647.jpg" /> are shown in Figures 1-3 with<img src="9-8101378\da4ea1d0-9aff-4f0d-93d3-8a26b19a6579.jpg" />, <img src="9-8101378\46d53914-0aba-4943-9200-e983797b07dd.jpg" />, <img src="9-8101378\2ae7e93a-fa09-459b-bdff-b0c21c039a3f.jpg" />, <img src="9-8101378\51f879a0-d449-47e6-9c7a-8cf28d3fade5.jpg" />, <img src="9-8101378\4f55952d-cc5e-4f1a-b1ed-bef08c688125.jpg" />for a</p><p>1) Fibre-reinforced generalized thermoelastic medium with hydrostatic initial stress (FRGTEHIS) by solid line.</p><p>2) Fibre-reinforced generalized thermoelastic medium without hydrostatic initial stress (FRGTEW-HIS) by solid line with centered symbol (*).</p><p>3) Isotropic generalized thermoelastic medium with hydrostatic initial stress (IGTEHIS) by dashed line.</p><p>4) Isotropic generalized thermoelastic medium without hydrostatic initial stress (IGTEWHIS) by dashed line with centered symbol (*).</p><p>These graphical results represent the solutions obtained by using the generalized theory with two relaxation times (G-L theory) by taking<img src="9-8101378\29132c09-c174-441f-a8cd-11fba3b989cd.jpg" />,<img src="9-8101378\8aa80b3f-f0ea-43f1-824f-c9c6c4b7f1f5.jpg" />.</p></sec><sec id="s8"><title>8. Discussions</title><p>The values of normal displacement for the case of FRGTEHIS increase sharply in the range and then</p><p>oscillate with distance. In case of IGTEHIS, the variations of normal displacement are very less in magnitude and for FRGTEWHIS, IGTEWHIS, these variations are quite uniform and at a particular point these variations are opposite in nature i.e. when one is on the zenith and the other one is on the lowest point. These variations are shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>.</p><p>It is observed from <xref ref-type="fig" rid="fig2">Figure 2</xref> that the variations of normal force stress for FRGTEHIS, FRGTEWHIS, IGTEHIS are similar in oscillating manner. The variation of normal force stress for IGTEWHIS is highly oscillating in nature in comparison to the variations obtained for FRGTEHIS, FRGTEWHIS, IGTEHIS.</p><p>The deformation of the body effects the change in temperature to a large extent as compared to normal displacement and normal force stress which is evident from <xref ref-type="fig" rid="fig3">Figure 3</xref>. Among all the mediums, the variation of temperature distribution is least oscillating for IGTEHIS.</p></sec><sec id="s9"><title>9. Conclusions</title><p>1) The affects of anisotropy and hydrostatic initial stress are observed on all the quantities.</p><p>2) The variations of the temperature distribution are more oscillatory in nature than those of of normal force stress and normal displacement .</p><p>3) The variations for L-S and G-L theory of thermoelasticity are close, although the authors have de-</p><p>picted the graphical results only for G-L theory.</p></sec><sec id="s10"><title>10. 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