<?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.2011.12006</article-id><article-id pub-id-type="publisher-id">WJM-4671</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>
 
 
  Thermal Bending of Circular Plates for Non-Axisymmetrical Problems
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>hengzhu</surname><given-names>Dong</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>Weihong</surname><given-names>Peng</given-names></name></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Jun</surname><given-names>Li</given-names></name></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Fashan</surname><given-names>Li</given-names></name></contrib></contrib-group><author-notes><corresp id="cor1">* E-mail:<email>dongzhengzhu@hotmail.com(HD)</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>44</fpage><lpage>49</lpage><history><date date-type="received"><day>February</day>	<month>17,</month>	<year>2011</year></date><date date-type="rev-recd"><day>March</day>	<month>30,</month>	<year>2011</year>	</date><date date-type="accepted"><day>April</day>	<month>12,</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>
 
 
  Using the Green function, the boundary integral formula and natural boundary integral equation for thermal elastic problems are obtained. Then based on bending solutions to circular plates subjected to the non-axi- symmetrical load, by utilizing the Fourier series and convolution formulae, the bending solutions under non-axisymmetrical thermal conditions have been obtained. The calculating process is simple. Examples show the discussed methods are effective.
 
</p></abstract><kwd-group><kwd>Thermal Bending Problems</kwd><kwd> Circular Plate</kwd><kwd> Boundary Integral Formula</kwd><kwd> Natural Boundary 
Integral Equation</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Due to the complexity of the thermoelasticity problems, analytic solutions can be obtained only for axisymmetrical problems and simply problems [1-6]. For general non-axisymmetrical loads and general non-axisymmetrical boundary conditions, the numerical computation is the main method [7,8,9]. For bending problems of solid circular plates, Fu Bao-lian adopted the reciprocal theorem and took the solution of the clamped circular plate as the basic solution to discuss some bending solutions under axis-symmetrical loads [<xref ref-type="bibr" rid="scirp.4671-ref10">10</xref>]. Wang An-wen introduced the point source function to discuss the nonsymmetrical bending problems under the concentrated force [11,12].<sup> </sup>Yu De-hao discussed bending problems of plates with the natural boundary element method [13,14].<sup> </sup>Using the above methods, Li Shun-cai discussed the bending problems of solid circular plates under the boundary loads [15-17]. On the basis of the same method, using Fourier series and several convolution formulae, the boundary integral formula and natural boundary integral equation for the thermal bending of circular plates are obtained. The calculating process is simple. Examples show that the discussed methods are effective.</p></sec><sec id="s2"><title>2. Boundary Integral Formula and Natural Boundary Integral Equation</title><p>The differential equation of elastic plate bending problems is</p><disp-formula id="scirp.4671-formula96339"><label>(1)</label><graphic position="anchor" xlink:href="4-4900013\998b72ef-540c-4a5d-b4f8-52825c26ca87.jpg"  xlink:type="simple"/></disp-formula><p>where, <img src="4-4900013\dc3ac319-0f8a-457c-aeee-20d506d648a5.jpg" />is the Laplacian operator, u is the deflection of the plate, q is the surface density of external loads, D is the bending rigidity of the plate, <img src="4-4900013\db4785c5-e658-49fd-b6c9-47aaf8e37e16.jpg" />is the plate in a circle domain. For convenient, suppose the circle is a unit circle.</p><p>Using the Green formula of the bending problems for thin plates, we get</p><disp-formula id="scirp.4671-formula96340"><label>(2)</label><graphic position="anchor" xlink:href="4-4900013\4a216a6c-1ecc-4365-b824-307f7d19746e.jpg"  xlink:type="simple"/></disp-formula><p>Let<img src="4-4900013\e0de3f68-07da-4072-928e-c71ba94fa718.jpg" />, which is the Green function of the biharmonic equation in<img src="4-4900013\5ef9db56-5864-4fc6-b8e5-be625230e656.jpg" />, and then the Poisson integral equation of the bending problem of the plate can be found</p><disp-formula id="scirp.4671-formula96341"><label>(3)</label><graphic position="anchor" xlink:href="4-4900013\5c34d754-7048-4fe6-8b84-3b7c68ac3c97.jpg"  xlink:type="simple"/></disp-formula><p>where<img src="4-4900013\621bb38c-98c8-4b3f-8e57-9891a94cbf18.jpg" />, <img src="4-4900013\f4432203-b402-4673-a070-c82f5afda4e1.jpg" />, <img src="4-4900013\5c57d7f4-7ef6-4ccf-bbf0-3b69b7c6522a.jpg" />, <img src="4-4900013\d25bb196-f8cc-49be-bf9b-34826c563e79.jpg" />,</p><p><img src="4-4900013\2b0ac354-cb23-4371-b881-224cb6cfcc75.jpg" />is the Laplacian operator related to<img src="4-4900013\af9fa9e7-8f2e-49e8-8d4e-8f7346ca03b5.jpg" />. The Green function in the unit circular domain can be obtained from the basic solution of the biharmonic equation</p><disp-formula id="scirp.4671-formula96342"><label>(4)</label><graphic position="anchor" xlink:href="4-4900013\210355e6-772b-4be5-aaf8-f788f684ff19.jpg"  xlink:type="simple"/></disp-formula><p>where, <img src="4-4900013\df014547-0931-4727-a084-a799170ca343.jpg" />and <img src="4-4900013\f470e571-aa49-4fea-a273-08ac8c67a0c5.jpg" /> represent the polar coordinate <img src="4-4900013\55681ee7-3da6-4e76-85ef-49bcb53ad0f3.jpg" /> and <img src="4-4900013\5b84b763-cccc-440e-9082-9c58c10e4486.jpg" /> respectively. Thus</p><p><img src="4-4900013\0a7bfde8-17cf-4a16-9e85-ed0367bef735.jpg" /></p><p><img src="4-4900013\c0710513-faed-4d76-85d5-59474a01b0f9.jpg" /></p><p>Hence, the Poisson integral formula of the bending circular plates can be obtained as</p><p><img src="4-4900013\60970413-22f7-48bd-8425-3a9795c37935.jpg" /></p><p>where, * is the convolution with regard to<img src="4-4900013\82fe3679-0e97-4b2e-a6c4-52bc1f3526f3.jpg" />, <img src="4-4900013\4855f18c-1c94-4abe-81b7-9dd9f27446e7.jpg" />, <img src="4-4900013\4586f34a-fffc-409b-b5d2-27f30f0f55e6.jpg" />denote the deflection and slope at the edge respectively. For the supported edge, <img src="4-4900013\a3a514ff-5fce-4f2e-b2e8-96739a91d7fe.jpg" />, the above equation will be educed to</p><disp-formula id="scirp.4671-formula96343"><label>(5)</label><graphic position="anchor" xlink:href="4-4900013\80a4990c-e848-4215-a111-2f87011c8e3d.jpg"  xlink:type="simple"/></disp-formula><p>Suppose M is the differential boundary operator in the polar coordinate system, the bending moment Mu</p><disp-formula id="scirp.4671-formula96344"><label>(6)</label><graphic position="anchor" xlink:href="4-4900013\88b6f2b7-b9f2-4810-b6bd-b6e9ae49aaf0.jpg"  xlink:type="simple"/></disp-formula><p>where, <img src="4-4900013\abc67730-ec3e-4669-b16f-5c06247dd02b.jpg" />is Poisson ratio. Let the boundary operator acts on Equation (5), and use the limit formula of generalized function</p><p><img src="4-4900013\1f362277-7801-4d57-b7cc-7bf5bafccd6b.jpg" /></p><p>The natural boundary integral equation of the bending problems<sup> </sup>can be obtained as</p><disp-formula id="scirp.4671-formula96345"><label>(7)</label><graphic position="anchor" xlink:href="4-4900013\b52d942a-5ebf-412b-866f-6f84d69576de.jpg"  xlink:type="simple"/></disp-formula><p>here</p><p><img src="4-4900013\5c9f7ad6-1aba-462f-a3d1-d2f16596b2c6.jpg" /></p></sec><sec id="s3"><title>3. Thermoelasticity Equation and Boundary Conditions</title><p>The steady-state thermoelasticity equation is</p><p><img src="4-4900013\62f4fa5f-f2cf-4c0d-a08c-b98aafa75e2b.jpg" /></p><p>where q<sup>*</sup> is the surface distribution density of the thermoelasticity equivalent load over the plate. Suppose h is the thickness of the plate, E is elastic modulus, α is the thermal expansion coefficient and D is the bending rigidity of the plate. In general, suppose the thermal distribution is linear along the plate thickness, the equivalent load</p><p><img src="4-4900013\d943e347-0266-45b4-b4a2-f0af16869420.jpg" /></p><p><img src="4-4900013\55a2e183-d76b-4dba-bb30-bccb1fc44324.jpg" /></p><p>where</p><p><img src="4-4900013\17f536e7-ff6b-447c-bf37-f33329eb7996.jpg" /></p><p>T(r, θ) is the thermal distribution function on the surface of the plate.</p><p>The equivalent boundary conditions of the clamped bending plate are<img src="4-4900013\c9680ed9-6aa5-4ef1-81d9-480dfc81508e.jpg" />,<img src="4-4900013\b34a99f9-9e09-49c5-bb1d-d684b61ef5ed.jpg" />. The equivalent boundary conditions of the simply bending plate are</p><p><img src="4-4900013\daaf978b-abe8-42f5-af58-3058ddaf3309.jpg" /></p><p>If in the plate there are no internal heat sources, then<img src="4-4900013\bce8d9b0-f6cd-4ae4-8649-9bfd0367efda.jpg" />, q<sup>*</sup> = 0, for the simply plate, <img src="4-4900013\5ebb4f42-7a62-4ab7-8da3-e22d75ef92e1.jpg" />, Equations (5) and (6) will be reduced to</p><disp-formula id="scirp.4671-formula96346"><label>(8)</label><graphic position="anchor" xlink:href="4-4900013\2c0330d5-addd-4bfb-8808-d6c747ac445c.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.4671-formula96347"><label>(9)</label><graphic position="anchor" xlink:href="4-4900013\8da30844-a3dd-4aa4-8a3d-48ca7d00e7d9.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. Heat Sources on the Plate</title><p>Firstly consider internal heat sources in the plate. The solution process is discussed through some examples.</p><p>Example 1 For comparison, suppose the thermal distribution function on the surface of the plate is axisymmetrical, <img src="4-4900013\71cff11e-eb05-4e29-94aa-5c86363f7c27.jpg" /></p><p><img src="4-4900013\16933eea-df79-4e2b-a83a-ebcf340e9964.jpg" /></p><p>For the clamped plate, from (5)</p><p><img src="4-4900013\4643e085-6a33-44a4-9ffa-cf011cadbedd.jpg" /></p><p>This solution is according to the axisymmetrical solution</p><p><img src="4-4900013\9c2c24c7-222b-4a2e-a67b-0753f8294a71.jpg" />&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;</p><p>For the simply plate, firstly from the Equation (7) to get u<sub>n</sub> which is a constant in axisymmetrical problems. Using the convolution formula [18,19]</p><p><img src="4-4900013\18b236af-1674-4d95-88af-eb01c67c639d.jpg" /></p><p>if k = 0, we have</p><p><img src="4-4900013\8a1ff415-7f28-4871-b831-91e0aed2f2b5.jpg" /></p><p>From (7), we get</p><p><img src="4-4900013\a6a59459-349a-4790-aee8-f429e2324205.jpg" /></p><p>So that</p><p><img src="4-4900013\1a22a355-3a2b-41b0-8390-7a35464a6b58.jpg" /></p><p>Substituting it into (8) and using the convolution formula</p><p><img src="4-4900013\e3ff3660-d8f2-459f-9a7d-04df178c4d4a.jpg" /></p><p>We get</p><p><img src="4-4900013\e0d325dd-ddb1-49de-81c5-359ead1fbeed.jpg" /></p><p>The solution is according to the axisymmetrical solution.</p><p>Example 2 Suppose the center of the thermal distribution function <img src="4-4900013\30079d6e-f439-4e7d-b558-edc1bcf823e5.jpg" /> is in the point<img src="4-4900013\f6c16300-f369-4b37-be30-63fe5f365aea.jpg" />. This is a non-axisymmetrical problem.</p><p><img src="4-4900013\461ea6d7-1cbf-4f85-8ebc-1a803e4e35a8.jpg" /></p><p>and</p><p><img src="4-4900013\27a80789-a51a-4c20-8d24-cda99cc8bf26.jpg" /></p><p>For the clamped plate, from (5)</p><p><img src="4-4900013\cadaeb4d-d562-47c2-89ee-03ef96ff06bb.jpg" /></p><p>Suppose μ = 0.3, D = 1, α/h = 1, by the numerical calculation, the deflections of the plate are shown as <xref ref-type="fig" rid="fig1">Figure 1</xref>.</p><p>The center deflection of the plate is 0.046 and the maximum deflection is 0.048.</p><p>For the simply plate, firstly using Equation (7) to get u<sub>n </sub>, suppose</p><p><img src="4-4900013\4a5cebfa-7511-45c0-854e-f5abeb8f9dab.jpg" /></p><p>Then suppose μ = 0.3, D = 1, α/h = 1, the left expression of (7) is expanded to Fourier series</p><p><img src="4-4900013\a9e5a3a5-4b48-4e32-b109-116e8fa0d848.jpg" /></p><p>Substituting it into (8) which is an integral with a strongly singular Poisson kernel, and using the convolution formula, we get</p><p><img src="4-4900013\9a407592-ca07-448b-aa29-4ed6ea0576f4.jpg" /></p><p>Then</p><p><img src="4-4900013\140e8648-cda8-4e8f-95b2-8fca2ba93e7e.jpg" /></p><p>The deflections of the plate are shown as <xref ref-type="fig" rid="fig2">Figure 2</xref>.</p><p>The center deflection of the plate is 0.669 and the maximum deflection is 0.67.</p></sec><sec id="s5"><title>5. No Heat Sources on the Plate</title><p>When there are no heat sources on the plate, T(r,θ) satisfies harmonic equation, <img src="4-4900013\f761ec5d-15dc-468f-b7ed-6d79cad193e9.jpg" />, thus, q<sup>*</sup> = 0. For the clamped plate, there is no bending deflections on the plate. For the simply plate, (5) and (7) will be reduced to</p><p><img src="4-4900013\27dbd2cd-89d8-4466-b95f-6479890838e7.jpg" /></p><p><img src="4-4900013\eac3c4f8-21ae-41e7-b483-4db02e5b2e88.jpg" /></p><p>Example 3 On the boundary of a simply plate, T(1,θ) = sin2θ, in the plate T(r, θ) = r<sup>2</sup> sin2θ.</p><p>Suppose</p><p><img src="4-4900013\3991b6e4-4925-476b-8e0a-e5153d02eaf1.jpg" /></p><p>Then using the convolution formula</p><p><img src="4-4900013\df2cc293-9cb6-46ea-80ba-441c02a53290.jpg" />s We get</p><p><img src="4-4900013\c35bb1c9-f749-418e-b2bf-192dddf46403.jpg" /></p><p>Substituting it into (8) and using the convolution formula</p><p><img src="4-4900013\f59072d3-c320-4afd-a41c-33f8949bc273.jpg" /></p><p>We have</p><p><img src="4-4900013\8fe0ef71-3317-48dd-9e0a-72545760e93b.jpg" /></p><p>From above equation, we get</p><p><img src="4-4900013\20ac1531-3b5a-47e3-992b-b1cd630ff722.jpg" /></p><p>Suppose μ = 0.3, D = 1, α/h = 1, the bending deflections and the bending resultants are as <xref ref-type="fig" rid="fig3">Figure 3</xref> and <xref ref-type="fig" rid="fig4">Figure 4</xref>:</p></sec><sec id="s6"><title>6. Conclusions</title><p>Based on the Green function method, the boundary integral formula and natural boundary integral equation with</p><p>the strongly singular kernel are educed for the thermal bending problem of the plate supported at the boundary. he convolution formulae are utilized to get the solutions of deflection and slope directly for simple problems. As to complex problems, the Fourier series will be used to get the solutions with nice convergence velocity and computational accuracy. The calculating process is simple. accuracy. The calculating process is simple. The problems of other complicated loads can be solved with the similar method or by the superposition with the solutions of the above examples.</p></sec><sec id="s7"><title>7. Acknowledgements</title><p>This work is supported by grants of National Basic Research Program of China, No. 2007CB209400 and Project Funded by the Priority Academic Program Development of Jiangsu Higher Education Institutions (PAPD), also supported by State Key Laboratory of Coal Resources and Safe Mining (CUMT) (SKLCRS08X04), supported by Foundation for National Doctoral Dissertation author of China (200760) and Program for New Century Excellent Talents in University (NCET-07-804).</p></sec><sec id="s8"><title>REFERENCES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.4671-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">S. P. Timoshengko and S. Woinowsky-Krieger, “Theory of Plates and Shells,” 2nd Edition, McGraw-Hill, New York, 1959.</mixed-citation></ref><ref id="scirp.4671-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">R. Szilard, “Theory and Analysis of Plates-Classical and Numerical Methods,” Prentice Hall, New Jersey, 1974.</mixed-citation></ref><ref id="scirp.4671-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">J. L. Zhu, “The Boundary Element Method for Elliptic Boundary Value Problems,” Science Press, Beijing, 1988.</mixed-citation></ref><ref id="scirp.4671-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">J. L. Zhu, “The Boundary Integral Equation Method for Solving Dirichelt Problem of Plane Biharmonic Equation,” Journal of Computational Mathematics, Vol. 6, No. 3, 1984, pp. 278-288.</mixed-citation></ref><ref id="scirp.4671-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">K. Chandrashekhara, “Theory of Plates,” University Press, Hyderabad, 2001, pp. 147-182.</mixed-citation></ref><ref id="scirp.4671-ref6"><label>6</label><mixed-citation publication-type="other" xlink:type="simple">P. F. Hou, L. J. Guo and W. Lu, “Simply Supported Circular Plate under Uniform Thermo-Mechanical Coupling Loading,” Journal of Zhejiang University (Engineering Science), Vol. 41, No. 1, January 2007, pp. 104-108.</mixed-citation></ref><ref id="scirp.4671-ref7"><label>7</label><mixed-citation publication-type="other" xlink:type="simple">Z. G. Zhao and P. R. Wang, “The Laplace Transform Finite Element Method for Dynamic Coupled Thermoelastic Bending Problems of Thin Plates,” Acta Mechanica Solida Sinica, Vol. 18, No. 2, 1997, pp. 183-187.</mixed-citation></ref><ref id="scirp.4671-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">Y. Sun and W. X. Zhong, “Finite Element Surface Stress Calculation,” Chinese Journal of Computational Mechanics, Vol. 27, No. 2, April 2010, pp. 177-181.</mixed-citation></ref><ref id="scirp.4671-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">I. Babuska and T. Stroubolis, “The Finite Element and Its Reliability,” Oxford University Press, London, 2001.</mixed-citation></ref><ref id="scirp.4671-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">B. L. Fu, “The New Bending Theorem of the Thin Plates on Reciprocal Method,” Science Press, Beijing, 2003.</mixed-citation></ref><ref id="scirp.4671-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">A. W. Wang, “Solution to Asymmetric Bending of Circular Plates under Single Load by Using Point-Source Function,” Acta Mechanica Sinica, Vol. 24, No. 3, 1992, pp. 381-387.</mixed-citation></ref><ref id="scirp.4671-ref12"><label>12</label><mixed-citation publication-type="other" xlink:type="simple">X. S. Wang, “δ Function and Its Application in Mechanics,” Science Press, Beijing, 1993.</mixed-citation></ref><ref id="scirp.4671-ref13"><label>13</label><mixed-citation publication-type="other" xlink:type="simple">D. H. Yu, “Mathematics Theory of National Boundary Element Method,” Science Press, Beijing, 1993.</mixed-citation></ref><ref id="scirp.4671-ref14"><label>14</label><mixed-citation publication-type="other" xlink:type="simple">D. H. Yu, “Natural Boundary Integral Equations and Related Computational Methods ,” Journal of Yanshan University, Vol. 28, No. 2, March 2004, pp. 111-113.</mixed-citation></ref><ref id="scirp.4671-ref15"><label>15</label><mixed-citation publication-type="other" xlink:type="simple">S. C. Li and Z. Z. Dong, “Natural Boundary Element Method to the Bending Problem of the Circular Plate under the Non-Continuous Loads,” Journal of Guangdong Industrial University, Vol. 16, No. 2, 2004, pp.83-88.</mixed-citation></ref><ref id="scirp.4671-ref16"><label>16</label><mixed-citation publication-type="other" xlink:type="simple">S. C. Li, Z. Z. Dong and W. H. Xie, “Application of Natural Boundary Element Method to the Bending Problem of the Elastic Thin Plate,” Journal of Xuzhou Normal University, Vol. 20, No. 4, 2002, pp. 12-15.</mixed-citation></ref><ref id="scirp.4671-ref17"><label>17</label><mixed-citation publication-type="other" xlink:type="simple">S. C. Li, Z. Z. Dong and W. H. Xie, “The Analytical Formulas of Bending Deflection for Infinite Plates with a Unit Circle under the Boundary Loads,” Journal of Gansu Sciences, Vol. 16, No. 2, 2004, pp. 83-88.</mixed-citation></ref><ref id="scirp.4671-ref18"><label>18</label><mixed-citation publication-type="other" xlink:type="simple">I. M. Gel’fand and G. E. Shilov, “Generalized Functions,” Academic Press, New York, 1964.</mixed-citation></ref><ref id="scirp.4671-ref19"><label>19</label><mixed-citation publication-type="other" xlink:type="simple">D. H. Yu, “Natural Boundary Integral Method and Its Applications,” Science Press &amp; Kluwer Academic Publishers, Beijing, 2002.</mixed-citation></ref></ref-list></back></article>