Piezothermoelastic Solution for Angle-Ply Laminated Cylindrical Panel
A three dimensional solution is presented for simply supported, angle-ply laminated hybrid cylindrical panel under cylindrical bending. The differential equations with variable coefficients are solved by the modified Frobenius method. Numerical results are presented for sinusoidal loads to illustrat...
Gespeichert in:
Veröffentlicht in: | Journal of intelligent material systems and structures 1997-05, Vol.8 (5), p.452-464 |
---|---|
Hauptverfasser: | , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 464 |
---|---|
container_issue | 5 |
container_start_page | 452 |
container_title | Journal of intelligent material systems and structures |
container_volume | 8 |
creator | Dumir, P. C. Dube, G. P. Kumar, Satish |
description | A three dimensional solution is presented for simply supported, angle-ply laminated hybrid cylindrical panel under cylindrical bending. The differential equations with variable coefficients are solved by the modified Frobenius method. Numerical results are presented for sinusoidal loads to illustrate the effect of the thickness parameter and the lamination angle. The two dimensional classical lamination theory and first order shear deformation theory are assessed by comparison with the three dimensional solution. |
doi_str_mv | 10.1177/1045389X9700800508 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_36351257</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_1045389X9700800508</sage_id><sourcerecordid>36351257</sourcerecordid><originalsourceid>FETCH-LOGICAL-c376t-3e473497741fdfed417729402ab1800e0d806723e44928d05e99fd00de42ab6b3</originalsourceid><addsrcrecordid>eNqF0M1LwzAYBvAgCs7pP-CpB_FW9-arSY9jzA8YOFDBW8madGakzUzaw_zrzdjwIugpOfzeh4cHoWsMdxgLMcHAOJXleykAJAAHeYJGmFPIJabyNP0TyPfiHF3EuAHAkgMdofnSmi_ff5jQeuNU7G2dvXg39NZ3WeNDNu3WzuRLt8sWqrWd6o3OZjtnOx1srVy2VJ1xl-isUS6aq-M7Rm_389fZY754fniaTRd5TUXR59QwQVkpBMONboxmqTopGRC1wqm1AS2hECQxVhKpgZuybDSANiyRYkXH6PaQuw3-czCxr1oba-NcKuGHWNGCcky4-BcSQTFgyhIkB1gHH2MwTbUNtlVhV2Go9tNWv6dNRzfHdBXTBk1QXW3jzyWBkktCEpscWFRrU238ELo0zl_B36OmhO4</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>27310134</pqid></control><display><type>article</type><title>Piezothermoelastic Solution for Angle-Ply Laminated Cylindrical Panel</title><source>SAGE Complete A-Z List</source><creator>Dumir, P. C. ; Dube, G. P. ; Kumar, Satish</creator><creatorcontrib>Dumir, P. C. ; Dube, G. P. ; Kumar, Satish</creatorcontrib><description>A three dimensional solution is presented for simply supported, angle-ply laminated hybrid cylindrical panel under cylindrical bending. The differential equations with variable coefficients are solved by the modified Frobenius method. Numerical results are presented for sinusoidal loads to illustrate the effect of the thickness parameter and the lamination angle. The two dimensional classical lamination theory and first order shear deformation theory are assessed by comparison with the three dimensional solution.</description><identifier>ISSN: 1045-389X</identifier><identifier>EISSN: 1530-8138</identifier><identifier>DOI: 10.1177/1045389X9700800508</identifier><language>eng</language><publisher>851 New Holland Ave., Box 3535, Lancaster, PA 17604, USA: SAGE Publications</publisher><subject>Exact sciences and technology ; Fundamental areas of phenomenology (including applications) ; Physics ; Solid mechanics ; Structural and continuum mechanics ; Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...) ; Vibrations and mechanical waves</subject><ispartof>Journal of intelligent material systems and structures, 1997-05, Vol.8 (5), p.452-464</ispartof><rights>1998 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c376t-3e473497741fdfed417729402ab1800e0d806723e44928d05e99fd00de42ab6b3</citedby><cites>FETCH-LOGICAL-c376t-3e473497741fdfed417729402ab1800e0d806723e44928d05e99fd00de42ab6b3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/1045389X9700800508$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/1045389X9700800508$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,778,782,21806,27911,27912,43608,43609</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=2095822$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Dumir, P. C.</creatorcontrib><creatorcontrib>Dube, G. P.</creatorcontrib><creatorcontrib>Kumar, Satish</creatorcontrib><title>Piezothermoelastic Solution for Angle-Ply Laminated Cylindrical Panel</title><title>Journal of intelligent material systems and structures</title><description>A three dimensional solution is presented for simply supported, angle-ply laminated hybrid cylindrical panel under cylindrical bending. The differential equations with variable coefficients are solved by the modified Frobenius method. Numerical results are presented for sinusoidal loads to illustrate the effect of the thickness parameter and the lamination angle. The two dimensional classical lamination theory and first order shear deformation theory are assessed by comparison with the three dimensional solution.</description><subject>Exact sciences and technology</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Physics</subject><subject>Solid mechanics</subject><subject>Structural and continuum mechanics</subject><subject>Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</subject><subject>Vibrations and mechanical waves</subject><issn>1045-389X</issn><issn>1530-8138</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1997</creationdate><recordtype>article</recordtype><recordid>eNqF0M1LwzAYBvAgCs7pP-CpB_FW9-arSY9jzA8YOFDBW8madGakzUzaw_zrzdjwIugpOfzeh4cHoWsMdxgLMcHAOJXleykAJAAHeYJGmFPIJabyNP0TyPfiHF3EuAHAkgMdofnSmi_ff5jQeuNU7G2dvXg39NZ3WeNDNu3WzuRLt8sWqrWd6o3OZjtnOx1srVy2VJ1xl-isUS6aq-M7Rm_389fZY754fniaTRd5TUXR59QwQVkpBMONboxmqTopGRC1wqm1AS2hECQxVhKpgZuybDSANiyRYkXH6PaQuw3-czCxr1oba-NcKuGHWNGCcky4-BcSQTFgyhIkB1gHH2MwTbUNtlVhV2Go9tNWv6dNRzfHdBXTBk1QXW3jzyWBkktCEpscWFRrU238ELo0zl_B36OmhO4</recordid><startdate>19970501</startdate><enddate>19970501</enddate><creator>Dumir, P. C.</creator><creator>Dube, G. P.</creator><creator>Kumar, Satish</creator><general>SAGE Publications</general><general>Technomic</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7U5</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope></search><sort><creationdate>19970501</creationdate><title>Piezothermoelastic Solution for Angle-Ply Laminated Cylindrical Panel</title><author>Dumir, P. C. ; Dube, G. P. ; Kumar, Satish</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c376t-3e473497741fdfed417729402ab1800e0d806723e44928d05e99fd00de42ab6b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1997</creationdate><topic>Exact sciences and technology</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Physics</topic><topic>Solid mechanics</topic><topic>Structural and continuum mechanics</topic><topic>Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)</topic><topic>Vibrations and mechanical waves</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Dumir, P. C.</creatorcontrib><creatorcontrib>Dube, G. P.</creatorcontrib><creatorcontrib>Kumar, Satish</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Journal of intelligent material systems and structures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Dumir, P. C.</au><au>Dube, G. P.</au><au>Kumar, Satish</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Piezothermoelastic Solution for Angle-Ply Laminated Cylindrical Panel</atitle><jtitle>Journal of intelligent material systems and structures</jtitle><date>1997-05-01</date><risdate>1997</risdate><volume>8</volume><issue>5</issue><spage>452</spage><epage>464</epage><pages>452-464</pages><issn>1045-389X</issn><eissn>1530-8138</eissn><abstract>A three dimensional solution is presented for simply supported, angle-ply laminated hybrid cylindrical panel under cylindrical bending. The differential equations with variable coefficients are solved by the modified Frobenius method. Numerical results are presented for sinusoidal loads to illustrate the effect of the thickness parameter and the lamination angle. The two dimensional classical lamination theory and first order shear deformation theory are assessed by comparison with the three dimensional solution.</abstract><cop>851 New Holland Ave., Box 3535, Lancaster, PA 17604, USA</cop><pub>SAGE Publications</pub><doi>10.1177/1045389X9700800508</doi><tpages>13</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 1045-389X |
ispartof | Journal of intelligent material systems and structures, 1997-05, Vol.8 (5), p.452-464 |
issn | 1045-389X 1530-8138 |
language | eng |
recordid | cdi_proquest_miscellaneous_36351257 |
source | SAGE Complete A-Z List |
subjects | Exact sciences and technology Fundamental areas of phenomenology (including applications) Physics Solid mechanics Structural and continuum mechanics Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...) Vibrations and mechanical waves |
title | Piezothermoelastic Solution for Angle-Ply Laminated Cylindrical Panel |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-16T03%3A31%3A05IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Piezothermoelastic%20Solution%20for%20Angle-Ply%20Laminated%20Cylindrical%20Panel&rft.jtitle=Journal%20of%20intelligent%20material%20systems%20and%20structures&rft.au=Dumir,%20P.%20C.&rft.date=1997-05-01&rft.volume=8&rft.issue=5&rft.spage=452&rft.epage=464&rft.pages=452-464&rft.issn=1045-389X&rft.eissn=1530-8138&rft_id=info:doi/10.1177/1045389X9700800508&rft_dat=%3Cproquest_cross%3E36351257%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=27310134&rft_id=info:pmid/&rft_sage_id=10.1177_1045389X9700800508&rfr_iscdi=true |