<?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">WJM</journal-id><journal-title-group><journal-title>World Journal of Mechanics</journal-title></journal-title-group><issn pub-type="epub">2160-049X</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/wjm.2011.12005</article-id><article-id pub-id-type="publisher-id">WJM-4670</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><subject> Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  An Efficient Numerical Method for Calculation of Elastic and Thermo-Elastic Fields in a Homogeneous Medium with Several Heterogeneous Inclusions
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>ergey</surname><given-names>Kanaun</given-names></name><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><author-notes><corresp id="cor1">* E-mail:<email>kanaoun@itesm.mx</email></corresp></author-notes><pub-date pub-type="epub"><day>19</day><month>04</month><year>2011</year></pub-date><volume>01</volume><issue>02</issue><fpage>31</fpage><lpage>43</lpage><history><date date-type="received"><day>February</day>	<month>12,</month>	<year>2011</year></date><date date-type="rev-recd"><day>March</day>	<month>31,</month>	<year>2011</year>	</date><date date-type="accepted"><day>April</day>	<month>8,</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 work is devoted to calculation of static elastic and thermo-elastic fields in a homogeneous medium with a finite number of isolated heterogeneous inclusions. Firstly, the problem is reduced to the solution of inte-gral equations for strain and stress fields in the medium with inclusions. Then, Gaussian approximating func-tions are used for discretization of these equations. For such functions, the elements of the matrix of the dis-cretized problem are calculated in explicit analytical forms. The method is mesh free, and only the coordi-nates of the approximating nodes are the geometrical information required in the method. If such nodes compose a regular grid, the matrix of the discretized problem obtains the Toeplitz properties. By the calcula-tion of matrix-vector products with such matrices, the Fast Fourier Transform technique may be used. The latter accelerates essentially the process of the iterative solution of the disretized problem. The results of calculations of elastic fields in 3D-medium with an isolated spherical heterogeneous inclusion are compared with exact solutions. Examples of the calculation of elastic and thermo-elastic fields in the medium with several inclusions are presented.
 
</p></abstract><kwd-group><kwd>Elasticity</kwd><kwd> Heterogeneous Medium</kwd><kwd> Integral Equations</kwd><kwd> Gaussian Approximating Functions</kwd><kwd> 
Toeplitz Matrix</kwd><kwd> Fast Fourier Transform</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Calculation of elastic fields in homogeneous materials with isolated heterogeneous inclusions is an important problem of stress analysis of composites and materials with defects. Efficient numerical methods of the solution of this problem are based on the volume integral equations for the fields in heterogeneous media (see, e.g., [1-3]). By the use of these equations, the fields inside the inclusions become principal unknowns of the problem. If the fields inside the inclusions are known, the fields in the medium are reconstructed from the original integral equations. Thus, the problem should be solved only in the region occupied by the inclusions. This is the main advantage of the Integral Equation Method (IEM) over the Finite Element Method (FEM), where the fields in the medium as well as in the inclusions are equivalent unknowns, and the solution has to be found in the whole region. The IEM is preferable if inclusions being smaller than the characteristic sizes of the body are situated far from its boundary.</p><p>A conventional method of the solution of integral equations is based on the following procedure. The region of integration is divided into a finite number of sub-regions, where the unknown functions are approximated by some standard functions (e.g., polynomial splines, radial functions, wavelets, etc.). After application of the Method of Moments or the Collocation Method the problem is reduced to a finite system of linear algebraic equations with respect to the coefficients of the approximation (the discretized problem) (see, e.g., [<xref ref-type="bibr" rid="scirp.4670-ref3">3</xref>]). The elements of the matrix of this system are integrals over the sub-regions. For conventional approximating functions, a great portion of computer time is spent for numerical calculation of these integrals. The matrices of the discretized problems are usually non-sparse and have large dimensions (if high accuracy of the numerical solutions is required). Computational cost of the solution of linear algebraic systems with such matrices is rather high. In application to the 3D-integral equations of elasticity for a medium with inclusions, this traditional numerical scheme was carried out in [4,5].</p><p>In this work, an efficient numerical method for the solution of integral equations of elasticity and thermoelasticity for a 3D-homogeneous medium with a finite number of isolated inclusions is developed. For discretization of these equations, the Gaussian radial approximating functions are used. The theory of approximation by Gaussian and similar functions was developed in [<xref ref-type="bibr" rid="scirp.4670-ref6">6</xref>]. For such functions, the elements of the matrix of the discretized problems are calculated in explicit analytical forms. Thus, the time of the construction of this matrix is essentially reduced in comparison with the methods that incorporate conventional approximating functions and require numerical integration by the calculation of the matrix elements. For regular grids of approximating nodes, the matrix of the discretized problem has the Toeplitz structure, and the Fast Fourier Transform (FFT) technique may be used for the calculation of matrix-vector products in the process of iterative solution of the discretized problem. The initial “geometrical” information required in the method is only the coordinates of the approximating nodes but not detailed forms of the mesh cells. Thus, the method is mesh free in fact.</p><p>For the numerical solution of 2D-volume integral equations of elasticity, a similar method was developed in [<xref ref-type="bibr" rid="scirp.4670-ref7">7</xref>]. In the present work, the method is extended on the 3D-volume integral equations of elasticity and thermo elasticity.</p><p>The structure of this paper is as follows. In Section 2, the 3D-volume integral equations of elasticity for strain and stress fields in a homogeneous medium with a set of isolated heterogeneous inclusions are considered. In Section 3, Gaussian approximating functions are used for discretization of these equations. Comparisons of the numerical and exact solutions for a medium with a spherical inclusion which elastic properties vary along the radius are presented in Section 4. A medium with several isolated inclusions is also considered in this section. In Section 5, the problem of thermo-elasticity for the medium with inhomogeneities is considered. In the Conclusions, some details of the proposed method and the area of its application are discussed.</p></sec><sec id="s2"><title>2. Integral Equations of Static Elasticity for a Homogeneous Medium with a Finite Number of Isolated Inclusions</title><p>Let an infinite homogeneous medium with the tensor of elastic constants <img src="3-4900011\6067c6e7-2742-4d14-85af-3dd923c3d509.jpg" /> contain a finite number N of isolated inclusions that occupy regions <img src="3-4900011\7556b893-159a-4e73-a26d-5dd1f0cac24d.jpg" /> (<img src="3-4900011\a70e2207-e951-4f3e-a238-dd046f3f0b6e.jpg" />). Elastic properties inside each region <img src="3-4900011\bb725864-f36d-4882-a12a-7d31d8b8b85d.jpg" />are defined by the tensors<img src="3-4900011\0d5d4d6f-b641-4ee3-9619-fcd346be3bf5.jpg" />, where<img src="3-4900011\fa79b3ab-84a9-4ecf-a93c-4147ec1ac638.jpg" /> is a point of the 3D-space. The medium is subjected to an external strain <img src="3-4900011\b4c8952e-0aab-4009-9dc9-c1f5bc88048a.jpg" /> (or stress<img src="3-4900011\92a7f7f2-4829-4074-9606-6a62265c8e0a.jpg" />) field, and the objective is to calculate elastic strain and stress fields in the medium with the inclusions. This problem may be reduced to volume integral equations for the strain <img src="3-4900011\f465e795-3696-4863-bcee-67d1fca7a33c.jpg" /> or stress <img src="3-4900011\db8937a1-38b4-417a-9d25-cd1f1b25d592.jpg" /> tensors inside the inclusions. Let<img src="3-4900011\be3eb735-f285-4248-b90c-d3efce3ee2f1.jpg" />, and <img src="3-4900011\9f3b28d0-c908-4aff-824c-3faed953a591.jpg" />be the characteristic function of the region V occupied by the inclusions: <img src="3-4900011\0059efdf-c07e-4d8a-8725-80a3f494ed58.jpg" />if<img src="3-4900011\9b07a56d-6589-4cc4-849c-d21409b5f8c5.jpg" />, <img src="3-4900011\a29f76d1-e287-42fe-bcb0-7a3a4ae58d46.jpg" />if<img src="3-4900011\1b13bbc6-c002-497f-a175-2e76b5cd1348.jpg" />. The strain field <img src="3-4900011\483f01d4-82f8-4a29-88ae-73df3c06db94.jpg" /> in the medium with the inclusions satisfies the following integral equation (see, e.g., [1,8]):</p><disp-formula id="scirp.4670-formula81498"><label>(1)</label><graphic position="anchor" xlink:href="3-4900011\65e4d8b8-f58f-41bf-b2b1-3dcd3e7e5860.jpg"  xlink:type="simple"/></disp-formula><p>Here<img src="3-4900011\66fd7d6a-4bce-4576-9da9-cf39301bb029.jpg" />, <img src="3-4900011\3b304768-5e8c-4ce9-a13b-4290de3f3b77.jpg" />when<img src="3-4900011\8fde3536-4057-4111-ac0c-3b342bf18f26.jpg" />, and <img src="3-4900011\fb39af6c-5dfa-4120-9c3c-79bc2264793c.jpg" /> when<img src="3-4900011\1e7eb955-20f4-488a-ba29-6d4503b6c232.jpg" />. Summation with respect to repeating tensorial (low) indices is implied. The kernel <img src="3-4900011\6749619b-b352-4066-898c-638cbf33f639.jpg" /> of the integral operator in this equation is the second derivative of the Green function <img src="3-4900011\9111cf5d-a9fb-44fa-9872-ae7a55da2563.jpg" /> of the homogeneous host medium <img src="3-4900011\edd42751-832d-493c-be7a-351f0a888d50.jpg" /></p><disp-formula id="scirp.4670-formula81499"><label>(2)</label><graphic position="anchor" xlink:href="3-4900011\e1f95e3f-167e-416b-832c-7b97a063273a.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="3-4900011\92d552cc-e7ed-4c18-898c-d9ab01045e97.jpg" /> is the solution of the following equation:</p><disp-formula id="scirp.4670-formula81500"><label>(3)</label><graphic position="anchor" xlink:href="3-4900011\f425f230-c7f0-422e-85a0-b0a5f08c3fac.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="3-4900011\5079c0a5-0941-458f-a1aa-22ed98db8236.jpg" /> is Kronecker’s symbol, <img src="3-4900011\1873d4f4-3ad2-4901-8192-8f7f54d40f0e.jpg" />is Dirac’s delta-function. The parentheses in indices mean symmetrization.</p><p>A similar equation may be written for the stress field σ(x) in the medium with the inclusions ([1,8]):</p><disp-formula id="scirp.4670-formula81501"><label>(4)</label><graphic position="anchor" xlink:href="3-4900011\930b99b5-2da3-4c5d-bc43-792e7ec6f30b.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="3-4900011\ba9bf43d-eed4-408a-a369-f9eaac86c544.jpg" /> is an external stress field applied to the medium<img src="3-4900011\102ebc8e-610d-4633-be9c-4ec52ec6d247.jpg" />, <img src="3-4900011\0cb4095d-562d-4c5c-b080-a8440b72445f.jpg" />, <img src="3-4900011\c1028410-680a-463f-80cd-6402ca25346d.jpg" /><img src="3-4900011\2d19d6c0-d19b-4abf-a495-45259dfa6e0c.jpg" />and</p><disp-formula id="scirp.4670-formula81502"><label>(5)</label><graphic position="anchor" xlink:href="3-4900011\517bc471-42d6-4d39-b5d8-7fd32b44d948.jpg"  xlink:type="simple"/></disp-formula><p>Note that the functions <img src="3-4900011\10246671-3167-45bb-b191-36e1bdbab56a.jpg" /> and <img src="3-4900011\9dc6a71d-68bf-4bde-a3dd-74412343418f.jpg" /> in (2) and (5) behave as <img src="3-4900011\14e43817-9bcb-45ae-9312-0cd54b28b7aa.jpg" /> when<img src="3-4900011\738c5d9d-3d91-437b-ba8c-fecd701f4c87.jpg" />, and therefore, the integral operators K and S in (1) and (4) are singular. Regularizations of these operators on continuous tensorfunctions with a finite support are indicated in [1,9]. Let <img src="3-4900011\c453cebe-b197-43e7-a0b4-189bffa11826.jpg" /> be a smooth tensor-function which Fourier transform <img src="3-4900011\323bc9a3-45b5-4b28-b9cf-9d0ac9be0e71.jpg" /> is bounded and tends to zero at infinity as <img src="3-4900011\f5cf8aa0-4da2-4005-b0b5-2485eb3e02a8.jpg" /> or faster. In this case, the actions of the operators K and S on such a function are defined by the equations:</p><disp-formula id="scirp.4670-formula81503"><label>(6)</label><graphic position="anchor" xlink:href="3-4900011\d1f49cbb-22cd-4658-9512-948d98d8232f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81504"><label>(7)</label><graphic position="anchor" xlink:href="3-4900011\dc88de70-d1e3-41b0-a78e-44d702e5883b.jpg"  xlink:type="simple"/></disp-formula><p>The integrals in the right-hand sides of these equations exist as ordinary integrals. Here <img src="3-4900011\bfed7f6e-82bc-41a9-a8e0-95aca39f7283.jpg" /> and <img src="3-4900011\d5d5366d-1fe3-4724-bb50-6d2d51d95cca.jpg" /> are the Fourier transforms of the functions <img src="3-4900011\58dee6de-4bc2-4b21-838c-972bc1d7e9ad.jpg" /> and<img src="3-4900011\2d59fddf-3f2f-4eac-98cf-517e906b930f.jpg" />. If the medium is isotropic, the functions <img src="3-4900011\be94767f-81eb-42ce-9acd-f4a12da44716.jpg" /> and <img src="3-4900011\fc625612-2f9a-45ae-b976-8cae83336b17.jpg" /> take the forms:</p><disp-formula id="scirp.4670-formula81505"><label>(8)</label><graphic position="anchor" xlink:href="3-4900011\f00bec2d-5509-42ed-be9b-95b6c158e1db.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81506"><label>, (9)</label><graphic position="anchor" xlink:href="3-4900011\ccf2f9be-e2bb-4dc6-a757-4f1119c4b6ad.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81507"><label>, (10)</label><graphic position="anchor" xlink:href="3-4900011\52545771-662c-45b0-a858-442050d15c4d.jpg"  xlink:type="simple"/></disp-formula><p>where k is the vector parameter of the Fourier transform, <img src="3-4900011\7523fe76-3b77-4843-b553-b122cd3dad74.jpg" />is the scalar product of the vectors k and x, <img src="3-4900011\a86466cb-95ed-42a1-ba46-c4c9428db05c.jpg" />and <img src="3-4900011\f9d10d9e-ad7b-4c7c-9cbd-82484185e1ab.jpg" /> are the Lame constants of the host medium,</p><disp-formula id="scirp.4670-formula81508"><label>. (11)</label><graphic position="anchor" xlink:href="3-4900011\d24f0b6b-9961-4ce6-8aa3-05f7e64abfd8.jpg"  xlink:type="simple"/></disp-formula><p><img src="3-4900011\5dc8eaad-5ec8-4ee1-88fc-3f620f4e9b48.jpg" />are the elements of the tensor basis introduced in [<xref ref-type="bibr" rid="scirp.4670-ref1">1</xref>] for presentation of fourth-rank tensors:</p><disp-formula id="scirp.4670-formula81509"><label>(12)</label><graphic position="anchor" xlink:href="3-4900011\0602fa0f-7e74-41fc-a5dc-9c77bb0a4801.jpg"  xlink:type="simple"/></disp-formula><p>Because the strain <img src="3-4900011\355a6a6d-6b2a-499a-ba40-043d7996e2be.jpg" /> and stress <img src="3-4900011\49347e59-4cc7-41ad-bfca-a4e2922d4337.jpg" /> tensors under the integrals in (1) and (4) are multiplied by the function<img src="3-4900011\2d239f42-c8da-4b46-a060-8167f5be0463.jpg" />, the elastic fields inside the inclusions (in the region V) are in fact the principal unknowns of the problem. The fields in the medium are reconstructed from the same Equations (1) and (4) if the fields inside the inclusions are known. Another important fact that follows from the structure of (1) and (4) is that for the numerical solution of this equation, any appropriate region <img src="3-4900011\7819871e-d622-4ea0-b850-9b1b2e825d3e.jpg" /> that includes V may be considered. In particular, by the solution of the problem for an inclusion V of arbitrary shape one can consider a cuboid region <img src="3-4900011\f1b841aa-5d66-47e4-87a7-16502debcd23.jpg" /> that contains V (see <xref ref-type="fig" rid="fig1">Figure 1</xref>).</p><p>Unique solutions of (1) and (4) exist if the tensor of the elastic constants <img src="3-4900011\b7c4c6bf-0e0d-4479-ab6a-c87879b787f3.jpg" /> and the inverse tensor <img src="3-4900011\2127aba2-ca84-4d7b-b812-8519a6b19c59.jpg" /> do not degenerate inside V [<xref ref-type="bibr" rid="scirp.4670-ref9">9</xref>].</p></sec><sec id="s3"><title>3. Numerical Solution of the Integral Equations (1) and (4)</title><sec id="s3_1"><title>3.1. Discretization of Equation (1) for Strains by the Gaussian Approximating Functions</title><p>We consider Equation (1) for the elastic strains in a medium with heterogeneities and following to [<xref ref-type="bibr" rid="scirp.4670-ref6">6</xref>] find its solution in the form of the series:</p><disp-formula id="scirp.4670-formula81510"><label>(13)</label><graphic position="anchor" xlink:href="3-4900011\0d8cb753-609e-4a22-ba92-bdde7557e697.jpg"  xlink:type="simple"/></disp-formula><p>Here<img src="3-4900011\b58c01b2-f735-4657-bcff-47a47bbd7895.jpg" />, <img src="3-4900011\3c5c3a09-119f-4967-86dc-5e44edc32c8d.jpg" />are the nodes of a regular grid that covers a cuboid <img src="3-4900011\774650e1-1a1a-4a40-9b2e-817a161a5b5f.jpg" />that contains the region V occupied by the inclusions, h is the distances between the neighbor nodes, M is the total number of the nodes in V, <img src="3-4900011\e272620b-0b33-4919-8f0e-50b253abc852.jpg" />are unknown coefficients of the approximation. The parameter H has the order of 1<img src="3-4900011\3aaca766-bc7c-42ad-8315-7ce113a626ed.jpg" />. Substituting (13) into the integral in (1) leads to the following equation:</p><disp-formula id="scirp.4670-formula81511"><label>(14)</label><graphic position="anchor" xlink:href="3-4900011\e6d210ca-4485-4bb8-9412-2b490a12b889.jpg"  xlink:type="simple"/></disp-formula><p>where<img src="3-4900011\5b4a0e51-d104-4952-8071-aa0b0dc548cb.jpg" />, and the tensor <img src="3-4900011\d82daf54-e988-4172-81bf-2c465fd79ac4.jpg" /> has the form:</p><disp-formula id="scirp.4670-formula81512"><label>(15)</label><graphic position="anchor" xlink:href="3-4900011\823aca52-8e5f-405d-b66c-1d576da764c4.jpg"  xlink:type="simple"/></disp-formula><p>Here, the definition (6) of the operator K and Equation (8) for <img src="3-4900011\a353ec85-dab1-46ec-a2c6-a7ff7536d4ca.jpg" /> are used,</p><disp-formula id="scirp.4670-formula81513"><label>. (16)</label><graphic position="anchor" xlink:href="3-4900011\59d22b8c-5f50-4371-b996-ad56e82585d1.jpg"  xlink:type="simple"/></disp-formula><p>Note that in (14), <img src="3-4900011\04c353f6-d152-4720-bd6b-151f4c607125.jpg" />if<img src="3-4900011\9786749c-022f-4ef3-891f-42897ff2813e.jpg" />.</p><p>After introducing a spherical coordinate system in the k-space and integrating firstly over the unite sphere, and then, over the radius<img src="3-4900011\87f8c96d-ca5f-4483-a040-fc5cb8d0683e.jpg" />, the integral in the right hand side of (15) is calculated explicitly, and the tensor <img src="3-4900011\ff702ea7-3347-4bdc-ab6f-5e2103849713.jpg" /> takes the form:</p><p><img src="3-4900011\4fc5f119-494f-47a5-87d7-9be7693817b2.jpg" />(17)</p><disp-formula id="scirp.4670-formula81514"><label>(18)</label><graphic position="anchor" xlink:href="3-4900011\f1eebc3a-4680-49fc-8040-f923a6ab0694.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="3-4900011\60d1da3b-6c1e-41de-8f5a-c953198860f6.jpg" /> are the elements of the tensor basis (12). The three scalar functions<img src="3-4900011\4fb3c6b0-b388-450d-bdde-58272038604b.jpg" />, <img src="3-4900011\b78a62e8-006b-4ff3-8432-798529a991ff.jpg" />, <img src="3-4900011\6e5a3876-dae4-4123-a836-cd72611c9bb0.jpg" />in (17) and (18) have the forms:</p><disp-formula id="scirp.4670-formula81515"><label>(19)</label><graphic position="anchor" xlink:href="3-4900011\f73d7a7c-ceb8-4ba4-84d9-09ff0eb13e31.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81516"><label>(20)</label><graphic position="anchor" xlink:href="3-4900011\dc026ed0-72aa-497d-82e3-8197b847a832.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81517"><label>(21)</label><graphic position="anchor" xlink:href="3-4900011\3e7e067e-9029-437e-9d38-83068113285e.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81518"><label>(22)</label><graphic position="anchor" xlink:href="3-4900011\a7761a1c-1e2c-4d1f-bafe-d5c291e653b9.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="3-4900011\bddab91e-1cc3-4da4-bb6a-d83fcfd3fb8e.jpg" /> is the probability integral:</p><p><img src="3-4900011\7c1bd321-e565-407d-a743-45043a37d1b1.jpg" /></p><p>The system of linear algebraic equations for the unknowns <img src="3-4900011\7706c4a2-333d-4d2c-8149-e8a29a9bce3f.jpg" /> in (13) follows from (14) if the latter is satisfied at all the nodes (the Collocation Method). Note that if the nodes of the approximation (13) compose a cubic grid, the coefficients of the approximation <img src="3-4900011\be1e2e92-eae8-48f0-a412-877496c7b739.jpg" /> coincide with the values of the strain field <img src="3-4900011\216f591a-d1e5-453a-bb83-027381d4f081.jpg" /> in the corresponding nodes (<img src="3-4900011\d820ea8d-e87d-48a9-923b-d7a336cb7310.jpg" />(see [<xref ref-type="bibr" rid="scirp.4670-ref6">6</xref>]). As a result, we obtain the system of linear algebraic equations for the coefficients <img src="3-4900011\a5d5f844-6370-492e-bd63-4aa04aeca244.jpg" /> in the form:</p><disp-formula id="scirp.4670-formula81519"><label>(23)</label><graphic position="anchor" xlink:href="3-4900011\1cdf38ca-bbb9-4ab1-bd61-6ea9bd73019f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81520"><label>(24)</label><graphic position="anchor" xlink:href="3-4900011\fc77e2b7-7390-42c4-a392-90082c2e0502.jpg"  xlink:type="simple"/></disp-formula><p>This system may be written in the canonical form as follows:</p><disp-formula id="scirp.4670-formula81521"><label>(25)</label><graphic position="anchor" xlink:href="3-4900011\cb140cfe-bf91-4c12-8bc5-9d76eff4e73a.jpg"  xlink:type="simple"/></disp-formula><p>where I is the unit matrix of the dimensions<img src="3-4900011\6095dc6d-bd0c-44c4-84c2-210a476fdbc1.jpg" />, and the vectors of the unknowns X and the right-hand side F are</p><disp-formula id="scirp.4670-formula81522"><label>(26)</label><graphic position="anchor" xlink:href="3-4900011\771f653b-90d0-4273-9390-259a23194da1.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81523"><label>(27)</label><graphic position="anchor" xlink:href="3-4900011\7b7cc138-df4d-4567-9a3e-d46d82d09696.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="3-4900011\dc288e60-7464-45ab-83e0-a71ef103c6cc.jpg" /> is the transposition operation.</p><p>The matrix B in (25) has the dimensions <img src="3-4900011\05489234-b47a-4ff9-9a5d-3db5cce1e2ad.jpg" /> and consists of 36 sub-matrices <img src="3-4900011\20c39eb1-0d49-4799-9a8b-00f1197992e9.jpg" /> of the dimensions<img src="3-4900011\8f7bef63-f11a-401a-8707-2772cbf94579.jpg" />,</p><disp-formula id="scirp.4670-formula81524"><label>(28)</label><graphic position="anchor" xlink:href="3-4900011\f25a4ea4-aee4-49e6-a993-2625cc9c7512.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81525"><label>(29)</label><graphic position="anchor" xlink:href="3-4900011\06e39e45-bf30-4957-be46-2e854d3e8e47.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81526"><label>(30)</label><graphic position="anchor" xlink:href="3-4900011\068b5147-f40e-4521-a9c0-58399c7c4a00.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81527"><label>(31)</label><graphic position="anchor" xlink:href="3-4900011\e0d70703-23e8-4f7e-b6b8-84d753615008.jpg"  xlink:type="simple"/></disp-formula><p><img src="3-4900011\5c542d62-77e4-4be7-8332-91a59091cae0.jpg" /></p><disp-formula id="scirp.4670-formula81528"><label>(32)</label><graphic position="anchor" xlink:href="3-4900011\ad772fd0-ea7e-455d-8616-dbaf56479bf4.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81529"><label>(33)</label><graphic position="anchor" xlink:href="3-4900011\6dede626-a862-4268-becb-8164c06b17fe.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81530"><label>(34)</label><graphic position="anchor" xlink:href="3-4900011\02023188-e5d3-4889-bca8-09732ace86ec.jpg"  xlink:type="simple"/></disp-formula><p>In these equations,<img src="3-4900011\cca4e45a-fa99-4796-b8b6-87b45f4ba617.jpg" />; summation from 1 to 3 with respect to repeating indices i, j is implied. These equations follow from (23) and (27). As it is seen from (19)-(22), the elements of the matrix B in (29)-(34) have simple analytical forms and are calculated fast.</p></sec><sec id="s3_2"><title>3.2. Discretization of Equation (4) for Stresses by the Gaussian Approximating Functions</title><p>Let us consider (4) and find its solution in the form similar to (13):</p><disp-formula id="scirp.4670-formula81531"><label>(35)</label><graphic position="anchor" xlink:href="3-4900011\b81d3724-3b35-48f2-b7b0-d909f14abdae.jpg"  xlink:type="simple"/></disp-formula><p>Substituting this approximation in (4) and using the Collocation Methods we obtain the following linear algebraic system for the coefficients<img src="3-4900011\3c772edd-a66e-40fe-b5d5-6bad89d8f4a9.jpg" />:</p><disp-formula id="scirp.4670-formula81532"><label>(36)</label><graphic position="anchor" xlink:href="3-4900011\08573af2-10be-47d1-9aa8-8326b24feebd.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81533"><label>(37)</label><graphic position="anchor" xlink:href="3-4900011\a38959b8-dd14-4ef7-9f90-4660b335263c.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81534"><label>(38)</label><graphic position="anchor" xlink:href="3-4900011\7376d392-ddac-4514-9b58-d125fd116c25.jpg"  xlink:type="simple"/></disp-formula><p>The last integral is calculated similar to the integral in (15), and the tensor Γ(x) takes the following form:</p><disp-formula id="scirp.4670-formula81535"><label>(39)</label><graphic position="anchor" xlink:href="3-4900011\9bdaafac-2f76-4f3b-8dc1-37e7c869dc41.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81536"><label>(40)</label><graphic position="anchor" xlink:href="3-4900011\9fcb692d-e627-4830-a700-6726879d4b5a.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81537"><label>(41)</label><graphic position="anchor" xlink:href="3-4900011\f6818fc9-b716-4e99-bc63-e1dd6d321b7f.jpg"  xlink:type="simple"/></disp-formula><p>Here the functions Φ<sub>0</sub>, Φ<sub>1</sub>, Φ<sub>2</sub> and<img src="3-4900011\641d33fa-7ca1-42ae-8f23-6ad5eedd667c.jpg" />, <img src="3-4900011\d9cc913d-9f93-49de-a74d-63f253aaa682.jpg" />, <img src="3-4900011\73627479-00a1-4504-a3ef-e8f1bd8f475e.jpg" />are defined in (18) and (19)-(22).</p><p>Similar to (23), the discretized Equation (36) may be presented in the canonical form (25). In this case, the vector of unknowns X is composed from the values of the stress tensor <img src="3-4900011\e1a08a7c-c90c-47eb-94b9-1f500e6691b4.jpg" /> at the nodes, the vector of the right hand side F consists of the components of the external stress field <img src="3-4900011\48cf7dad-0bfe-416d-a686-f283c0a2afe4.jpg" /> at the nodes similar to (26), (27). The matrices <img src="3-4900011\ae4b9070-3944-46c8-bb33-ecb92b3f3e97.jpg" /> in (28) are defined in (29)-(34), where <img src="3-4900011\7337d189-1c16-40dd-b92a-59a826b22530.jpg" /> should be changed for<img src="3-4900011\479eec59-fd70-4371-8b09-f4fb030f2a1a.jpg" />, and <img src="3-4900011\cce105c4-3f8a-45bd-ac06-85dd7c4558bc.jpg" /> for <img src="3-4900011\4cd70faf-6cfd-4262-b1ed-a53d8a6788c7.jpg" />.</p></sec><sec id="s3_3"><title>3.3. Numerical Solution of the System (25)</title><p>It follows from (17)-(22) and (29)-(34) that B in (25) is a non-sparse matrix which dimensions may be very large if high accuracy of the solution is required. For the solution of linear algebraic systems with such matrices, only iterative methods are efficient. For instance, if the Minimal Residue Method (see, e.g., [<xref ref-type="bibr" rid="scirp.4670-ref10">10</xref>]) is used, the n-th iteration <img src="3-4900011\2722f50d-c6cd-4ee6-a31a-e755c99f7c90.jpg" /> of the solution of (25) is calculated as follows:</p><disp-formula id="scirp.4670-formula81538"><label>(42)</label><graphic position="anchor" xlink:href="3-4900011\9bbaf9c5-8401-4e7f-9755-fc13cfec73fc.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81539"><label>(43)</label><graphic position="anchor" xlink:href="3-4900011\e2d47bb1-53cd-4da5-b3ca-93e0e381f1fd.jpg"  xlink:type="simple"/></disp-formula><p>with the initial values X<sup>(0)</sup>, Y<sup>(0)</sup> of the vectors X and Y</p><disp-formula id="scirp.4670-formula81540"><label>. (44)</label><graphic position="anchor" xlink:href="3-4900011\9063e568-d13d-4f5e-93fa-9bc21f9997b3.jpg"  xlink:type="simple"/></disp-formula><p>Thus, the vector <img src="3-4900011\f15e37b1-8f30-40d3-9eb2-3f337cfbba9e.jpg" /> is to be multiplied by the matrix B at every step of the iteration process. For nonsparse matrices of large dimensions, calculation of such a product is an expensive computational operation. If, however, a regular grid of approximating nodes is used, the volume of calculations is reduced substantially. Let us consider the product BY in detail. For the matrix B that corresponds to (28)-(34), this product is a combination of the following sums:</p><disp-formula id="scirp.4670-formula81541"><label>(45)</label><graphic position="anchor" xlink:href="3-4900011\9b7f8383-11b4-49db-8a09-c3eb01b0aa56.jpg"  xlink:type="simple"/></disp-formula><p>where the tensor <img src="3-4900011\a2ace57e-f1a0-4f7b-8756-3ce7607697c5.jpg" /> is defined in (17). For a regular node grid with a step h, the coordinates of every node <img src="3-4900011\edac000a-643d-4b80-a443-5700538b4a62.jpg" /> can be presented in the form:</p><disp-formula id="scirp.4670-formula81542"><label>(46)</label><graphic position="anchor" xlink:href="3-4900011\93988054-5f0e-4fad-b2ed-e896423bdeae.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81543"><label>(47)</label><graphic position="anchor" xlink:href="3-4900011\8979ce98-9032-40de-a113-247f9dbe8059.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="3-4900011\7f586098-0518-44d9-82ee-cfaeed377430.jpg" /> are integers, <img src="3-4900011\9682dd7d-50b6-4730-a160-a75f7a1193cc.jpg" />, <img src="3-4900011\fd45c595-89d0-488c-9cf4-b52f8c53de00.jpg" />, <img src="3-4900011\d29f2d10-3049-418f-baa8-bfe4b702a390.jpg" />are minimal values of the node coordinates in the cuboid V which sides are parallel to the axes<img src="3-4900011\66f26ef5-e295-4f81-bb65-249e18c0b7e6.jpg" />, <img src="3-4900011\eecbcb32-19f4-4dd8-aba2-8afac2dc7e16.jpg" />,<img src="3-4900011\716a0a95-9331-4420-81fb-2e899f91a1ad.jpg" />. Thus, the position of every node may be defined by 3 integers (m, n, p). Connection between the one and three-index numerations of the nodes may be introduced by the equation:</p><disp-formula id="scirp.4670-formula81544"><label>(48)</label><graphic position="anchor" xlink:href="3-4900011\1622341d-a648-4afe-8eee-468a6e3be3f3.jpg"  xlink:type="simple"/></disp-formula><p>Here N<sub>1</sub>, N<sub>2</sub>, N<sub>3</sub> is the number of the nodes along the corresponding sides of V,<img src="3-4900011\7d3fc843-c63f-43ea-8b5b-be392f623551.jpg" />. In the threeindex numeration, the sum (45) is presented as follows:</p><disp-formula id="scirp.4670-formula81545"><label>, (49)</label><graphic position="anchor" xlink:href="3-4900011\b0841108-c497-45cf-b7b4-a587165b4c80.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81546"><label>(50)</label><graphic position="anchor" xlink:href="3-4900011\dc622855-607c-46b3-afb2-629ba3163516.jpg"  xlink:type="simple"/></disp-formula><p>It is seen from the last equation that the object <img src="3-4900011\1abaf06c-4a0e-4ff3-a48d-1736c20945bc.jpg" /> has the Toeplitz structure: it depends on the differences of the indices:<img src="3-4900011\88f3f8ca-36cb-40e6-bdcc-78348829f4b5.jpg" />, <img src="3-4900011\f02edece-2242-41b0-adb8-d2514b292ccf.jpg" />and<img src="3-4900011\416dec77-4170-40d1-8a3d-61adb71c2e7c.jpg" />. As a result, the Fourier Transform Technique can be used for the calculation of the triple sums in (49), and therefore, of the matrix-vector products. Application of the FFT algorithms for calculation of these sums essentially accelerates the iterative process (42)-(44). In addition, one has to keep in the computer memory not all the matrices <img src="3-4900011\58ccb8bb-b7cd-4649-bc00-6d3c2828327c.jpg" /> of the dimensions <img src="3-4900011\4573f34a-f076-43a2-bd07-9a785cff5d26.jpg" /> but only one column and one row of every such a matrix: the object that has the dimensions <img src="3-4900011\34efb491-3b88-42f8-a434-f8b7b0dee59a.jpg" /> and is calculated once for all the iteration process. The details of the FFT algorithm for the calculation of the matrix-vector products are described in [7,11].</p></sec></sec><sec id="s4"><title>4. Results of the Calculations</title><sec id="s4_1"><title>4.1. An Isolated Heterogeneous Inclusion in a Homogeneous Elastic Medium</title><p>Let us apply the method to the calculation of elastic fields inside a spherical isotropic inclusion of a radius a with radially varying elastic properties. The elastic fields will be considered in a Cartesian coordinate system (<img src="3-4900011\2e0bb0ec-4ce4-4bd8-b5f0-bce46b295f34.jpg" />) with the origin at the center of the inclusion. The medium is isotropic with the Young module E<sub>0</sub> and the Poisson ratio<img src="3-4900011\54a1398f-b210-434b-bee3-ca247d82131b.jpg" />. First, we consider an inclusion with parabolic change of the Young module <img src="3-4900011\2d1a4dff-67bb-4994-877b-bebc20a82c79.jpg" /> along the radius:</p><disp-formula id="scirp.4670-formula81547"><label>(51)</label><graphic position="anchor" xlink:href="3-4900011\336adba8-0e50-4e3b-86fb-5281b4b793c6.jpg"  xlink:type="simple"/></disp-formula><p>and constant Poisson ratio<img src="3-4900011\d73a7857-a844-485b-87d3-6105b749e5b0.jpg" />. The medium with the inclusion is subjected to a constant one-dimensional external stress field <img src="3-4900011\a30614fc-247a-41ec-8f94-6bc9d7c11ad2.jpg" /> in the direction of the x<sub>1</sub>-axis, <img src="3-4900011\3bcd88dc-c1b3-409f-ba59-9f0870a381e8.jpg" />is a scalar. In this case, the Young module <img src="3-4900011\40b97f55-3e67-4ecc-8163-e77150a86f15.jpg" /> is a continuous function together with the components <img src="3-4900011\457d7e88-0318-4eb2-8988-9307aedc9e05.jpg" /> of the stress tensor. The distributions of the components<img src="3-4900011\e4e3cb02-622a-4c16-91fe-abd6f86ab7d5.jpg" />, <img src="3-4900011\b3dc5e8f-458f-407b-aada-bb17c4ea11b6.jpg" />along the x<sub>1</sub> and x<sub>2</sub>-axes are presented in Figures 2-3. While the functions <img src="3-4900011\d622a7d1-978f-4041-a40c-1c65e4d57f76.jpg" /> and <img src="3-4900011\94ef4aeb-4378-451d-92f8-479cee1ee359.jpg" /> are on the right-hand sides in these figures, the functions <img src="3-4900011\1e0b1d0b-4b8a-4310-b6ea-3ae4ed71a392.jpg" /> and <img src="3-4900011\5fb1be05-f981-4683-a6a3-b0d5e2b8fd72.jpg" /> on their left-hand sides. The graphs in Figures 2-3 correspond to the numerical solution of Equation (4) for stresses inside the cube V:<img src="3-4900011\a72fda93-0ce6-4eb1-8acc-ef4f17089f83.jpg" />,<img src="3-4900011\7081e184-a01d-4ca4-b046-77dd36d35cc6.jpg" />. The regular grids of approximating nodes with the steps <img src="3-4900011\c3892e5f-6e14-4a5c-a526-b31939808c9f.jpg" /> (the total number of the nodes is<img src="3-4900011\623aa887-e2e2-4c5b-8877-d9ffabddca15.jpg" />), and <img src="3-4900011\19cd8cfe-4dc2-438b-accb-884efdb3befe.jpg" /> (M = 262 144) were considered. The graphs in <xref ref-type="fig" rid="fig4">Figure 4</xref> describe the distribution of the shear stress <img src="3-4900011\ddfdf8c9-fa5b-4434-aef8-e9ed343e3a63.jpg" /> along the x<sub>1</sub> and x<sub>3</sub> axes if the medium is subjected to the external shear stress tensor<img src="3-4900011\88920cd4-ee7d-41a0-9e69-7541c49a9596.jpg" />.</p><p>The bold lines in Figures 2-4 are exact distributions of the components of the elastic stress field obtained by the method presented in [<xref ref-type="bibr" rid="scirp.4670-ref8">8</xref>]. It is seen that for the grid step<img src="3-4900011\4087f6e2-de53-44f4-8cf1-60709f79daa5.jpg" />, the numerical solutions are practically coincide with the exact ones. The influence of the parameter H in (35) on the numerical results is not essential if<img src="3-4900011\98e6b3fa-614e-4546-9717-19d88e10f666.jpg" />, and <img src="3-4900011\65a07069-f993-4c28-a0e7-52687c482fe9.jpg" /> is taken in the calculations.</p><p>The same problem was solved with the help of Equation (1) for strains. The medium was subjected to the</p><p>external strain field<img src="3-4900011\51d0a65c-847e-4e63-b8a4-ac54313369ae.jpg" />, where <img src="3-4900011\c15bacba-0f84-45e5-9fbe-3bcd03ba0504.jpg" /> is a constant. The corresponding distributions of the components <img src="3-4900011\6de4668a-dd1d-4e8b-807c-d16124601ac0.jpg" /> and <img src="3-4900011\a2cde6eb-9169-4941-be8f-1b0881d31b52.jpg" /> of the strain tensor inside the inclusion are in Figures 5-6. <xref ref-type="fig" rid="fig7">Figure 7</xref> shows the distribution of the shear strain <img src="3-4900011\85028baa-43dc-468f-a161-26a7e70aef0e.jpg" /> by application of the external shear strain tensor<img src="3-4900011\6f296497-62fc-4d8c-88d8-9e27a9ac2dac.jpg" />. The solid lines in these figures are exact distributions of the corresponding components of the strain tensor. It is seen that similar to the equation for stresses, the numerical solution coincides practically with the exact one for the step of the node grid<img src="3-4900011\dc8b29b4-0fdf-4c25-ae22-f8fa596e9d6e.jpg" />. But the number of iterations in the process (42)-(44) turns out to be almost two times more than by the use of Equation (4) for stresses. This fact reflects general situation: the iteration process based on Equation (4) for stresses converges faster than the same process based on Equation (1) for strains if the inclusion is more rigid than the medium. In the opposite case, when the inclusion is softer than the medium, the iteration process based on the equation for strains converges faster than the same process based on the equation for stresses.</p><p>Note that if elastic moduli are not continuous on surfaces inside the inclusion or on the inclusion boundary, some components of the stress and strain tensors have jumps on these surfaces.</p><p>In this case, for accurate description of the elastic fields, the grid of the approximating nodes should be sufficiently fine. In the next example, we consider elastic fields in a spherical inclusion of the radius a that consists of a central kernel in the region <img src="3-4900011\b45c9ac5-4c68-4446-8218-60bb054444a9.jpg" /> with the Young module<img src="3-4900011\8c820dba-ecc8-4a94-9bc3-f7e10c1dfb2b.jpg" />, and a layer in the region <img src="3-4900011\5acb8612-c9e6-4186-827b-f3f89ce5d8e2.jpg" /> with the Young module<img src="3-4900011\7303104d-d447-4ce7-99a8-1385d06f5f46.jpg" />. The inclusion is embedded in a homogeneous medium with the Young module<img src="3-4900011\04777ef1-3877-47c6-99ec-d9bf7b04f8d4.jpg" />, Poisson ratios of the medium and the inclusion are the same<img src="3-4900011\054e0890-d440-4bbe-b213-c919052ef01e.jpg" />. For the</p><p>uniaxial external strain field<img src="3-4900011\16253e26-6dca-4041-99cd-6e65fa9fb27a.jpg" />, the corresponding distributions of the components <img src="3-4900011\b7974956-e92f-494c-a936-ab2639a12b72.jpg" /> and <img src="3-4900011\8a84967a-cda5-4796-bae6-c0cb07340ed5.jpg" /> of the strain tensor inside the inclusion are presented in Figures 8-9. For the external shear strain field<img src="3-4900011\df4aa854-4860-48f9-bac8-55ae932b5658.jpg" />, the distribution of the component <img src="3-4900011\fc750689-2cbc-4635-9e65-88590153f197.jpg" /> is in <xref ref-type="fig" rid="fig1">Figure 1</xref>0. Equation (1) for strains and cubic node grids with the steps<img src="3-4900011\8b56d048-fcef-4e94-9a52-0b9001912ebb.jpg" />, <img src="3-4900011\20b72864-400f-4567-9d49-e290841e762d.jpg" />(M = 68921) and <img src="3-4900011\a422624f-cae2-44d6-8f93-e09487abb5ea.jpg" /> (M = 8 120 601) were used for the construction of the graphs in Figures 8-10. The bold lines in these figures are exact solutions obtained by the method presented in [<xref ref-type="bibr" rid="scirp.4670-ref8">8</xref>]. It is seen from these figures that the numerical solutions tend to the exact one when the step h decreases.</p><p>The stress distributions in a layered spherical inclusion which Young moduli are more than the Young module of the medium are presented in Figures 11-13. In this case, <img src="3-4900011\0b699f18-7fbe-4a86-b72c-fdf1502e192f.jpg" />when <img src="3-4900011\9ab77150-0519-4786-b4cd-00569bbb4b66.jpg" /> and <img src="3-4900011\17c32753-114d-415a-919f-e2f72f0f3004.jpg" /> when 0.5&lt;|x|/a≤1,<img src="3-4900011\7cbb131b-7c16-4377-86d5-40a72a52ac42.jpg" />. The graphs in Figures 11-12 correspond to the uniaxial external stress field <img src="3-4900011\616b6e16-bcc0-44a9-bb79-7d237d452409.jpg" /> and in <xref ref-type="fig" rid="fig1">Figure 1</xref>3 to the external shear stress field<img src="3-4900011\200abb39-067f-4a0e-974d-5a698572f0c2.jpg" />. For the numerical solutions, Equation (4) for stresses was used with the node grid steps<img src="3-4900011\64f64d2f-1197-42dd-992d-1dd420c9332d.jpg" />, <img src="3-4900011\bc4c73d0-11c5-43a8-a6e5-c3d6e7437a5f.jpg" />, and<img src="3-4900011\7ed52982-8294-4ed8-ab2e-f3776f21e7f9.jpg" />.</p><p>Figures 2-13 demonstrate convergence of the numerical solution to the exact distribution of the elastic fields inside the inclusions when step h decreases. The iterative scheme (42)-(44) converges for any finite values of the elastic constants of the inclusion and the matrix. The number of the iterations grows together with the contrast in the elastic properties of the matrix and the inclusion as well as with the number M of the approximating nodes. Note that for not very large contrast in the elastic properties of the medium and the inclusion, the well-known Conjugate Gradient Method (see, e.g., [<xref ref-type="bibr" rid="scirp.4670-ref10">10</xref>]) applied to the solution of (23) or (36) converges faster than the Minimal Residue Method (42)-(44). But for large contrasts in the properties, the Conjugate Gradient Method may diverge, meanwhile the Minimal Residue Method keeps converging.</p></sec><sec id="s4_2"><title>4.2. Several Isolated Inclusions</title><p>Let a homogeneous medium contain three isolated spherical inclusions of equal radii <img src="3-4900011\85a5309f-1a66-46b0-a274-5d90f50cf2d0.jpg" /> We assume that the centers of the inclusions are at the vertices <img src="3-4900011\40068c1b-11ce-47b1-b992-542fa208e97f.jpg" /> of an equilateral triangle with the coordinates:</p><disp-formula id="scirp.4670-formula81548"><label>(53)</label><graphic position="anchor" xlink:href="3-4900011\7d7b98cf-3129-4155-84ff-7d2e3a0440fa.jpg"  xlink:type="simple"/></disp-formula><p>The numerical solution is constructed in the cuboid V that contains all these inclusions (<img src="3-4900011\6d27c7af-87a3-4a27-91ee-c5f52208b6df.jpg" />,<img src="3-4900011\bc791e14-3b54-473c-b836-1c17900138b7.jpg" /> ,<img src="3-4900011\86c913fc-847d-4fae-8d81-4a2c9538b429.jpg" />) (<xref ref-type="fig" rid="fig1">Figure 1</xref>4). The Young moduli of the medium and the inclusions are E<sub>0</sub> and E, and<img src="3-4900011\117b97e3-2b2d-4305-953d-2e27e0bae691.jpg" />.</p><p>A cubic node grid with the step <img src="3-4900011\048044c7-bb84-4552-b141-0b2b6b504177.jpg" />(M = 1 030 301) and <img src="3-4900011\95040b22-ac39-4eea-b84f-16710e715e15.jpg" /> (M = 8 120 601) that covers the cuboid V was used in the calculations,<img src="3-4900011\6eca6de9-cd68-4587-b63f-d9404a095241.jpg" />. For the external uniaxial stress field <img src="3-4900011\5cbf8e83-0aa8-4f9f-ac73-0688481f6c3d.jpg" /> acting along the x<sub>3</sub>-axis, the distribution of the component <img src="3-4900011\8f437d9a-e4f7-4afd-a4e3-ab9175a1fdec.jpg" /> of the stress tensor in the plane <img src="3-4900011\b6a35ded-4fc9-4876-addf-be0d335ea738.jpg" /> is presented in <xref ref-type="fig" rid="fig1">Figure 1</xref>5. The distributions of the components<img src="3-4900011\5aa88a35-bc14-40bb-81a1-057105f118ef.jpg" />, <img src="3-4900011\98e008e1-6370-4719-8f5e-a4e59e5bf6b8.jpg" />and <img src="3-4900011\fd56aeab-6c97-44dc-a3b6-db88f1352dce.jpg" /> along the lines<img src="3-4900011\f8ce000e-3ba7-4899-bbe1-512760a372a5.jpg" />, <img src="3-4900011\0eb77d64-681a-4e72-a781-185e12515d2c.jpg" />and<img src="3-4900011\f00bf432-ee62-4128-88ed-073f64477dfc.jpg" />, <img src="3-4900011\0ca2502a-72a0-4a6d-9ac1-ddbfedba47a7.jpg" />that go through the centers of the inclusions are in Figures 16-18, correspondingly. For the solution, Equation (4) for stresses was used.</p></sec></sec><sec id="s5"><title>5. The Problem of Thermo-Elasticity</title><p>We consider a homogeneous elastic medium with several</p><p>heterogeneous inclusions that occupy regions V<sup>k</sup> (k = 1,2,<img src="3-4900011\f9bb3e1b-5c6d-423e-bddd-d56dd9a50a9d.jpg" />). In addition to the elastic stiffness tensors <img src="3-4900011\dcb168b9-4d3d-40fb-950d-4e1d64976f7f.jpg" /> and <img src="3-4900011\744740cb-f6ba-4019-8e23-f58fa5e60ea9.jpg" /> of the inclusions and the host medium we introduce the second-rank tensors <img src="3-4900011\3d1d898f-eb18-4029-92ae-0f2cc8abdbc2.jpg" /> and <img src="3-4900011\968edeb2-1c89-466e-a3b8-09dfd8c26fc7.jpg" /> of thermal expansions of the corresponding materials. The tensors of the elastic stiffness and thermo-expansion of the medium with inclusions are represented in the forms:</p><disp-formula id="scirp.4670-formula81549"><label>(53)</label><graphic position="anchor" xlink:href="3-4900011\2981f0bc-e74b-424b-8db6-4690848fba98.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="3-4900011\25ede190-668a-4fe6-ac3a-d757db893a3e.jpg" /> is the characteristic function of the region occupied by the inclusions, the tensors <img src="3-4900011\eab5008f-920c-4882-a26a-66ee7921d5b1.jpg" /> and <img src="3-4900011\32cf0df9-99a5-4812-8a16-c19ae6556913.jpg" /> are constant, <img src="3-4900011\e7262bc2-5ed7-412c-8b80-f3526e297def.jpg" />, and<img src="3-4900011\36ed3d5d-51ef-443c-a9bf-7917f6766e7d.jpg" />,<img src="3-4900011\5a85a344-df3d-47c8-b336-fc350f49f1d3.jpg" /> if <img src="3-4900011\1c3fffd2-96f4-432a-9e1b-2ae22f4efe8c.jpg" /> If the medium is subjected to an external stress field and a temperature field<img src="3-4900011\51d714d0-7715-4db1-9f01-b9e9ad40c2a3.jpg" />, the stress tensor in the medium satisfies the following system of differential equations:</p><disp-formula id="scirp.4670-formula81550"><label>(54)</label><graphic position="anchor" xlink:href="3-4900011\c9ce9fe6-7e95-4b9d-ba91-8c1c1324d741.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="3-4900011\0df8e412-c093-4101-be31-b821d50ab6cd.jpg" /> is the tensor of elastic deformation that defines the stress tensor σ according to Hooke’s law, <img src="3-4900011\75bdea96-8d0d-4af0-954e-01481f5e678d.jpg" />is the temperature deformation of the medium, and <img src="3-4900011\b5279c1d-a64a-4736-8d2a-1a9daa1840fd.jpg" /> is the operator of incompatibility (<img src="3-4900011\14a8b609-40c5-45c2-ab67-4e04128701cd.jpg" />is the Levi-Civita tensor). If we introduce an auxiliary tensor <img src="3-4900011\c5b3099e-036a-46b4-9bb1-606bc449d655.jpg" /> by the equation</p><disp-formula id="scirp.4670-formula81551"><label>(55)</label><graphic position="anchor" xlink:href="3-4900011\7c00234b-0fc1-455f-8276-4fdc80508e94.jpg"  xlink:type="simple"/></disp-formula><p>system (54) may be rewritten in the following form:</p><disp-formula id="scirp.4670-formula81552"><label>(56)</label><graphic position="anchor" xlink:href="3-4900011\343d23c4-9bee-4f62-b43a-39c3b1474a9f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81553"><label>(57)</label><graphic position="anchor" xlink:href="3-4900011\0aaee99a-7d73-4605-a68a-e82c94f91113.jpg"  xlink:type="simple"/></disp-formula><p>The system (56) may be interpreted as a system of differential equations for internal stresses in a homogeneous medium with the constant stiffness tensor <img src="3-4900011\40f5534c-63c6-48d9-a72f-28d9f656f332.jpg" /> in the presence of dislocation moments of the density<img src="3-4900011\4353e308-524f-4df5-8827-52567e08ba1c.jpg" />. The solution of (56) may be presented in the integral form (see [8,12]):</p><disp-formula id="scirp.4670-formula81554"><label>(58)</label><graphic position="anchor" xlink:href="3-4900011\58bb5278-24cc-4446-9571-4716b0370cd1.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="3-4900011\e2772eb7-cd25-4f15-86e5-b588db316bed.jpg" /> is an external stress field applied to the medium. The kernel <img src="3-4900011\730fb6bc-71be-4137-86a6-1a70fc8e6030.jpg" /> of the integral operator in this equation coincides with the generalized function <img src="3-4900011\c03d7389-b760-4dae-a1af-49ddec689120.jpg" /> in (5), integration in (58) is spread over the entire medium. Substitution of the tensors <img src="3-4900011\8558114e-7b3a-49c9-a077-a786c984e8ab.jpg" /> and <img src="3-4900011\2503eeff-7cbd-418c-80fa-742f491419b2.jpg" /> from (57) and (53) into (58) yields</p><disp-formula id="scirp.4670-formula81555"><label>(59)</label><graphic position="anchor" xlink:href="3-4900011\c5c5a36a-c3d1-4168-b807-f5e4611c7e45.jpg"  xlink:type="simple"/></disp-formula><p>If<img src="3-4900011\52cc34d1-7e7c-46c0-a257-ac72a1e83f51.jpg" />, this equation coincides with Equation (4) for stresses in a medium with heterogeneities.</p><p>Let <img src="3-4900011\b4df2b15-fd90-4998-bfef-6733b12d4e86.jpg" /> be a constant temperature field, and for<img src="3-4900011\cb5ff62c-9d64-4761-8f52-642d8f57afe3.jpg" />, the medium be free of the temperature stresses. In this case, the value of the last integral in (59) depends on the conditions at infinity. If deformation is not restricted at infinity, this integral is equal to zero (see [<xref ref-type="bibr" rid="scirp.4670-ref8">8</xref>]):</p><disp-formula id="scirp.4670-formula81556"><label>(60)</label><graphic position="anchor" xlink:href="3-4900011\d7e02f18-74c6-4e8f-a22f-e698e50c900c.jpg"  xlink:type="simple"/></disp-formula><p>Meanwhile, for the condition that the total deformation of the medium is equal to zero, we have</p><disp-formula id="scirp.4670-formula81557"><label>(61)</label><graphic position="anchor" xlink:href="3-4900011\47b9c45e-2079-475d-854b-88d9de2e93cd.jpg"  xlink:type="simple"/></disp-formula><p>The right-hand side in this equation is the stress field in an infinite homogeneous medium with the properties<img src="3-4900011\bdd273df-4847-4b4c-b7ec-17a1dba87cd8.jpg" />, <img src="3-4900011\33c970ea-a789-4e7b-848c-c68a23c6ac10.jpg" />subjected to a constant temperature field T by the condition that the total deformation of the medium is zero.</p><p>In the absence of external stresses <img src="3-4900011\9c44495c-8a13-4325-be15-357e1ef8e798.jpg" /> and restrictions at infinity, (59) takes the form</p><disp-formula id="scirp.4670-formula81558"><label>(62)</label><graphic position="anchor" xlink:href="3-4900011\b2df0eae-b0d0-4d62-8f2c-e7aa28c3b79b.jpg"  xlink:type="simple"/></disp-formula><p>Approximation of the tensors <img src="3-4900011\501d56af-618d-4366-a3d3-3440554a8d7d.jpg" /> and <img src="3-4900011\afb4f00f-9c9b-4c5b-8359-df719c592237.jpg" /> by the Gaussian functions similar to (35) and application of the Collocation Method lead to the following discretized form of this equation:</p><disp-formula id="scirp.4670-formula81559"><label>(63)</label><graphic position="anchor" xlink:href="3-4900011\ac52a4d5-cb52-42bf-978d-8c30d7de115b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4670-formula81560"><label>(64)</label><graphic position="anchor" xlink:href="3-4900011\03c844e0-25e1-471f-9622-c8b814a1daa6.jpg"  xlink:type="simple"/></disp-formula><p>This system may be presented in the canonical form (25) which left-hand side coincides with the discretised form of Equation (4) for stresses, and the components of the vector F in its right-hand side are defined as follows:</p><disp-formula id="scirp.4670-formula81561"><label>(65)</label><graphic position="anchor" xlink:href="3-4900011\54c63cf4-3f6d-45fb-8b7d-777f14e1e414.jpg"  xlink:type="simple"/></disp-formula><p>Because the objects <img src="3-4900011\15d4b2bb-3f97-445e-a931-63612b1cb530.jpg" /> in (64) for <img src="3-4900011\8332a9d2-b79c-413f-875e-2fcbfcebd484.jpg" /> have the Teoplitz properties, the FFT technique may be used for the calculation of the vector F.</p><p>Distributions of temperature stresses in the medium with three spherical inclusions considered in Subsection 4.2 are presented in Figures 19-24. The Young’s module E<sub>0</sub>, Poisson ratio ν<sub>0</sub>, and the coefficient of thermo expansion</p><p><img src="3-4900011\7e65332b-1e90-45aa-ae59-2b1a51d2f4c2.jpg" />of the host medium are taken as follows<img src="3-4900011\14b13357-d0ed-42e0-8025-b071390e339f.jpg" />, <img src="3-4900011\b9ad7224-a81a-42d4-af42-0a556f3b8359.jpg" />, α<sub>0</sub> = 23 &#215; 10<sup>–6</sup>/˚C that corresponds to aluminum. The same parameters of the inclusions are<img src="3-4900011\87214a4f-69d1-468c-bdee-201e1f3d19d1.jpg" />, <img src="3-4900011\e3c1edf3-5fcd-4bc5-bc98-ef7c1d7cc34c.jpg" />, α<sub>0</sub> = 9 &#215; 10<sup>–6</sup>/˚C that corresponds to titanium. The solution of (64) was constructed in the cuboid<img src="3-4900011\2b424da3-353b-4888-a2ec-2a645e2a77ac.jpg" />, <img src="3-4900011\8fb690aa-7e8f-4726-859a-75b9802dc80a.jpg" />,<img src="3-4900011\5f45e87d-a02b-4126-9b3b-cd1309330b40.jpg" />. The radii of the inclusions are taken<img src="3-4900011\03af6024-05a8-42c0-be44-15d0177bbf25.jpg" />. Note that the stress distribution does not depend on the absolute sizes of the inclusions. The distributions of the components<img src="3-4900011\5c06bee7-f504-48de-8862-276ccdf660b0.jpg" />, <img src="3-4900011\baad4e9b-bb35-4424-99bb-528fa3877eb0.jpg" />, <img src="3-4900011\b60e6ea5-1144-4052-bae3-6f6c5885bbc9.jpg" />of the stress tensor along the axis <img src="3-4900011\bd112652-53a8-4cab-ace0-ada6c6fb5f98.jpg" /> for <img src="3-4900011\d08f1c63-4c46-4295-ab93-00e8d0025bde.jpg" /> and <img src="3-4900011\7543a85d-9fe2-4f8b-8974-e80fe8785203.jpg" /> are shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>9, 21 and 23. The distributions of the same stresses in the plane <img src="3-4900011\b06a908b-d30b-41e3-8769-c728dc076117.jpg" /> are shown in Figures 20, 22 and 24. The calculations are performed for the step of the node grid<img src="3-4900011\df08429d-377a-4ae9-86c4-596cf968d58c.jpg" />,<img src="3-4900011\c7779c9e-6c96-44f9-bead-0dcd226813cd.jpg" />.</p><p>Note that the integral equation for the stress field in an elasto-plastic heterogeneous medium follows from (57) and (58) if the temperature deformation T is changed for the plastic deformation<img src="3-4900011\f96d92ad-588b-48b1-9779-83266645d091.jpg" />. Because the plastic deformation is a non-linear function of stresses, the final equation will be non-linear with respect to the stress tensor. The conventional procedure of linearization of elasto-plastic problems is well known. The process of loading of the medium is divided into small intervals, and the problem is considered as linear in every such an interval. The same algorithm may be applied to the solution of the integral equation for the stresses in elasto-platic heterogeneous media.</p></sec><sec id="s6"><title>6. Conclusions</title><p>An efficient numerical method for the solution of 3Dproblems of elasticity and thermo-elasticity for a medium with isolated heterogeneous inclusions is proposed. The method may be applied to the solution of other problems of mathematical physics that can be reduced to volume integral equations. In particular, in [13,14], the method was used for the solution of the problems of electromagnetic wave scattering on perfectly conducting screens and 3D-dielectric bodies.</p><p>The main difficulty in the numerical solution of 3Dintegral equations of mathematical physics is a large number of approximation functions (approximating nodes) that should be taken in order to achieve acceptable accuracy. In the present method, this difficulty is overcome by the following means. First, the Gaussian approximating functions allow us to obtain the elements of the matrix of the discretized problems in closed analytical forms and thus, to calculate them fast. Second, the use of regular node grids provides Toeplitz properties to the matrix of the discretized problem. As a result, the number of independent elements of this matrix is essentially reduced, and in addition, the FFT algorithms may be applied to calculating matrix-vector products with such matrices.</p><p>For some integral equations of mathematical physics or other types of approximating functions, the elements of the matrix of the discretized problem are not calculated explicitly but expressed via a finite number of standard one-dimensional integrals that can be tabulated (see [6,13]). So, in these cases, the matrices of the discretized problems are also calculated fast.</p><p>For regular node grids and any type of identical approximating functions centered at the nodes, the matrices of the discretized problems obtain the Toeplitz properties. Thus, in these cases, the possibility of exploiting FFT algorithms for the calculation of the matrix-vector products always exists.</p><p>There are various ways of improvement of the method. As it is shown in [<xref ref-type="bibr" rid="scirp.4670-ref6">6</xref>], the Gaussian functions multiplied with special polynomials increase the precision of the approximation. If such functions are used in the framework of the method, all the algorithms presented in this work will be the same, and only the form of the functions<img src="3-4900011\5aa64a95-b030-4ef9-b07d-40f02c888c2d.jpg" />, <img src="3-4900011\dd3def6f-5201-4269-b895-e8ba97feb24c.jpg" />, and <img src="3-4900011\aaeaa9c5-e5f3-499d-95a6-1eee58cf9909.jpg" /> in (19)-(22) will change.</p><p>Note that in the framework of the method, many parts of the problem may be calculated in parallel. 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