Analysis of interlaminar stresses in the torsion of symmetric laminates
A modified shear deformation theory based on Reissner-type assumptions was considered in obtaining an approximate solution for the torsion of a symmetrically laminated, anisotropic plate. In-plane stresses were modified.
Gespeichert in:
Veröffentlicht in: | AIAA journal 1994-03, Vol.32 (3), p.662-665 |
---|---|
1. Verfasser: | |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 665 |
---|---|
container_issue | 3 |
container_start_page | 662 |
container_title | AIAA journal |
container_volume | 32 |
creator | Whitney, James M |
description | A modified shear deformation theory based on Reissner-type assumptions was considered in obtaining an approximate solution for the torsion of a symmetrically laminated, anisotropic plate. In-plane stresses were modified. |
doi_str_mv | 10.2514/3.12038 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_26464024</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2703035</sourcerecordid><originalsourceid>FETCH-LOGICAL-a354t-1a81982ebe6385366270894bf02026c3c01363f31948358686e93ee485a9373c3</originalsourceid><addsrcrecordid>eNpd0E1LAzEQBuAgCtYq_oVFRPGwmmSy2eyxFK2C4EXBW4jrLKbsR82kYP-9qS0WPYWEh3cmL2Ongl_LQqgbuBaSg9ljI1EA5GCK13024pyLXKhCHrIjonm6ydKIEZtNeteuyFM2NJnvI4bWdb53IaMYkAgpvWbxA7M4BPJDv3a06jqMwdfZBkekY3bQuJbwZHuO2cvd7fP0Pn98mj1MJ4-5g0LFXDgjKiPxDXVaDLSWJTeVemu45FLXUHMBGhoQlTJQGG00VoCoTOEqKKGGMbvY5C7C8LlEirbzVGPbuh6HJVmplVZcqgTP_sH5sAzps8msi6nKUid0uUF1GIgCNnYRfOfCygpu121asD9tJnm-jXNUu7YJrq89_XJI-ypYT73aMOed203cptjFe2ObZdtG_Iq7yL_2_-Rv0V6K4A</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>215339776</pqid></control><display><type>article</type><title>Analysis of interlaminar stresses in the torsion of symmetric laminates</title><source>Alma/SFX Local Collection</source><creator>Whitney, James M</creator><creatorcontrib>Whitney, James M</creatorcontrib><description>A modified shear deformation theory based on Reissner-type assumptions was considered in obtaining an approximate solution for the torsion of a symmetrically laminated, anisotropic plate. In-plane stresses were modified.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/3.12038</identifier><identifier>CODEN: AIAJAH</identifier><language>eng</language><publisher>Reston, VA: American Institute of Aeronautics and Astronautics</publisher><subject>Aerodynamics ; Design engineering ; Exact sciences and technology ; Fundamental areas of phenomenology (including applications) ; Physics ; Solid mechanics ; Static elasticity ; Static elasticity (thermoelasticity...) ; Structural and continuum mechanics</subject><ispartof>AIAA journal, 1994-03, Vol.32 (3), p.662-665</ispartof><rights>1994 INIST-CNRS</rights><rights>Copyright American Institute of Aeronautics and Astronautics Mar 1994</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a354t-1a81982ebe6385366270894bf02026c3c01363f31948358686e93ee485a9373c3</citedby><cites>FETCH-LOGICAL-a354t-1a81982ebe6385366270894bf02026c3c01363f31948358686e93ee485a9373c3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=3948434$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Whitney, James M</creatorcontrib><title>Analysis of interlaminar stresses in the torsion of symmetric laminates</title><title>AIAA journal</title><description>A modified shear deformation theory based on Reissner-type assumptions was considered in obtaining an approximate solution for the torsion of a symmetrically laminated, anisotropic plate. In-plane stresses were modified.</description><subject>Aerodynamics</subject><subject>Design engineering</subject><subject>Exact sciences and technology</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Physics</subject><subject>Solid mechanics</subject><subject>Static elasticity</subject><subject>Static elasticity (thermoelasticity...)</subject><subject>Structural and continuum mechanics</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1994</creationdate><recordtype>article</recordtype><recordid>eNpd0E1LAzEQBuAgCtYq_oVFRPGwmmSy2eyxFK2C4EXBW4jrLKbsR82kYP-9qS0WPYWEh3cmL2Ongl_LQqgbuBaSg9ljI1EA5GCK13024pyLXKhCHrIjonm6ydKIEZtNeteuyFM2NJnvI4bWdb53IaMYkAgpvWbxA7M4BPJDv3a06jqMwdfZBkekY3bQuJbwZHuO2cvd7fP0Pn98mj1MJ4-5g0LFXDgjKiPxDXVaDLSWJTeVemu45FLXUHMBGhoQlTJQGG00VoCoTOEqKKGGMbvY5C7C8LlEirbzVGPbuh6HJVmplVZcqgTP_sH5sAzps8msi6nKUid0uUF1GIgCNnYRfOfCygpu121asD9tJnm-jXNUu7YJrq89_XJI-ypYT73aMOed203cptjFe2ObZdtG_Iq7yL_2_-Rv0V6K4A</recordid><startdate>19940301</startdate><enddate>19940301</enddate><creator>Whitney, James M</creator><general>American Institute of Aeronautics and Astronautics</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>19940301</creationdate><title>Analysis of interlaminar stresses in the torsion of symmetric laminates</title><author>Whitney, James M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a354t-1a81982ebe6385366270894bf02026c3c01363f31948358686e93ee485a9373c3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1994</creationdate><topic>Aerodynamics</topic><topic>Design engineering</topic><topic>Exact sciences and technology</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Physics</topic><topic>Solid mechanics</topic><topic>Static elasticity</topic><topic>Static elasticity (thermoelasticity...)</topic><topic>Structural and continuum mechanics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Whitney, James M</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Whitney, James M</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Analysis of interlaminar stresses in the torsion of symmetric laminates</atitle><jtitle>AIAA journal</jtitle><date>1994-03-01</date><risdate>1994</risdate><volume>32</volume><issue>3</issue><spage>662</spage><epage>665</epage><pages>662-665</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><coden>AIAJAH</coden><abstract>A modified shear deformation theory based on Reissner-type assumptions was considered in obtaining an approximate solution for the torsion of a symmetrically laminated, anisotropic plate. In-plane stresses were modified.</abstract><cop>Reston, VA</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/3.12038</doi><tpages>4</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0001-1452 |
ispartof | AIAA journal, 1994-03, Vol.32 (3), p.662-665 |
issn | 0001-1452 1533-385X |
language | eng |
recordid | cdi_proquest_miscellaneous_26464024 |
source | Alma/SFX Local Collection |
subjects | Aerodynamics Design engineering Exact sciences and technology Fundamental areas of phenomenology (including applications) Physics Solid mechanics Static elasticity Static elasticity (thermoelasticity...) Structural and continuum mechanics |
title | Analysis of interlaminar stresses in the torsion of symmetric laminates |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-01T21%3A12%3A23IST&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=Analysis%20of%20interlaminar%20stresses%20in%20the%20torsion%20of%20symmetric%20laminates&rft.jtitle=AIAA%20journal&rft.au=Whitney,%20James%20M&rft.date=1994-03-01&rft.volume=32&rft.issue=3&rft.spage=662&rft.epage=665&rft.pages=662-665&rft.issn=0001-1452&rft.eissn=1533-385X&rft.coden=AIAJAH&rft_id=info:doi/10.2514/3.12038&rft_dat=%3Cproquest_cross%3E2703035%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=215339776&rft_id=info:pmid/&rfr_iscdi=true |