Strength of quasi-isotropic laminates under off-axis loading
An experimental investigation was carried out to determine the failure properties of quasi-isotropic AS4/3501-6 carbon/epoxy laminates under conditions where the loading axis did not coincide with the fiber axis. A tubular specimen subjected to combinations of pressure and axial tension was used to...
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Veröffentlicht in: | Composites science and technology 1989, Vol.34 (1), p.19-34 |
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description | An experimental investigation was carried out to determine the failure properties of quasi-isotropic AS4/3501-6 carbon/epoxy laminates under conditions where the loading axis did not coincide with the fiber axis. A tubular specimen subjected to combinations of pressure and axial tension was used to determine the response under various tension-tension biaxial stress states. The results showed no loss of strength with rotation of the laminate orientation with respect to the loading axes at angles including 22·5°,the maximum possible for the laminate used. Maximum fiber direction strains at failure were essentially independent of the rotation of the laminate as well as the biaxial stress state. |
doi_str_mv | 10.1016/0266-3538(89)90075-4 |
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A tubular specimen subjected to combinations of pressure and axial tension was used to determine the response under various tension-tension biaxial stress states. The results showed no loss of strength with rotation of the laminate orientation with respect to the loading axes at angles including 22·5°,the maximum possible for the laminate used. Maximum fiber direction strains at failure were essentially independent of the rotation of the laminate as well as the biaxial stress state.</description><identifier>ISSN: 0266-3538</identifier><identifier>EISSN: 1879-1050</identifier><identifier>DOI: 10.1016/0266-3538(89)90075-4</identifier><identifier>CODEN: CSTCEH</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Applied sciences ; Exact sciences and technology ; Forms of application and semi-finished materials ; Laminates ; Polymer industry, paints, wood ; Technology of polymers</subject><ispartof>Composites science and technology, 1989, Vol.34 (1), p.19-34</ispartof><rights>1989</rights><rights>1989 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c364t-702d6740080012add19fd2215d70a1ff15694f0b8f415c07c83126c6161130d23</citedby><cites>FETCH-LOGICAL-c364t-702d6740080012add19fd2215d70a1ff15694f0b8f415c07c83126c6161130d23</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/0266-3538(89)90075-4$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>315,781,785,3551,4025,27925,27926,27927,45997</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=7134879$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Swanson, S.R.</creatorcontrib><creatorcontrib>Trask, B.C.</creatorcontrib><title>Strength of quasi-isotropic laminates under off-axis loading</title><title>Composites science and technology</title><description>An experimental investigation was carried out to determine the failure properties of quasi-isotropic AS4/3501-6 carbon/epoxy laminates under conditions where the loading axis did not coincide with the fiber axis. A tubular specimen subjected to combinations of pressure and axial tension was used to determine the response under various tension-tension biaxial stress states. The results showed no loss of strength with rotation of the laminate orientation with respect to the loading axes at angles including 22·5°,the maximum possible for the laminate used. Maximum fiber direction strains at failure were essentially independent of the rotation of the laminate as well as the biaxial stress state.</description><subject>Applied sciences</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Laminates</subject><subject>Polymer industry, paints, wood</subject><subject>Technology of polymers</subject><issn>0266-3538</issn><issn>1879-1050</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1989</creationdate><recordtype>article</recordtype><recordid>eNp9kEtLw0AUhQdRsFb_gYssRHQRvXcyjwREkOILCi7U9TDOo46kSTuTiP57Eytdurqb75zD_Qg5RrhAQHEJVIi84EV5VlbnFYDkOdshEyxllSNw2CWTLbJPDlL6gBGq6IRcPXfRNYvuPWt9tu51CnlIbRfbVTBZrZeh0Z1LWd9YFwfE5_orpKxutQ3N4pDseV0nd_R3p-T17vZl9pDPn-4fZzfz3BSCdbkEaoVkACUAUm0tVt5SitxK0Og9clExD2-lZ8gNSFMWSIURKBALsLSYktNN7yq2696lTi1DMq6udePaPinKmeQlwwFkG9DENqXovFrFsNTxWyGoUZUaPajRgyor9atKsSF28tevk9G1j7oxIW2zEgs2qByw6w3mhl8_g4sqmeAa42yIznTKtuH_nR-SB3sI</recordid><startdate>1989</startdate><enddate>1989</enddate><creator>Swanson, S.R.</creator><creator>Trask, B.C.</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>H8D</scope><scope>JG9</scope><scope>L7M</scope></search><sort><creationdate>1989</creationdate><title>Strength of quasi-isotropic laminates under off-axis loading</title><author>Swanson, S.R. ; Trask, B.C.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c364t-702d6740080012add19fd2215d70a1ff15694f0b8f415c07c83126c6161130d23</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1989</creationdate><topic>Applied sciences</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Laminates</topic><topic>Polymer industry, paints, wood</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Swanson, S.R.</creatorcontrib><creatorcontrib>Trask, B.C.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Materials Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Composites science and technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Swanson, S.R.</au><au>Trask, B.C.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Strength of quasi-isotropic laminates under off-axis loading</atitle><jtitle>Composites science and technology</jtitle><date>1989</date><risdate>1989</risdate><volume>34</volume><issue>1</issue><spage>19</spage><epage>34</epage><pages>19-34</pages><issn>0266-3538</issn><eissn>1879-1050</eissn><coden>CSTCEH</coden><abstract>An experimental investigation was carried out to determine the failure properties of quasi-isotropic AS4/3501-6 carbon/epoxy laminates under conditions where the loading axis did not coincide with the fiber axis. A tubular specimen subjected to combinations of pressure and axial tension was used to determine the response under various tension-tension biaxial stress states. The results showed no loss of strength with rotation of the laminate orientation with respect to the loading axes at angles including 22·5°,the maximum possible for the laminate used. Maximum fiber direction strains at failure were essentially independent of the rotation of the laminate as well as the biaxial stress state.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/0266-3538(89)90075-4</doi><tpages>16</tpages></addata></record> |
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subjects | Applied sciences Exact sciences and technology Forms of application and semi-finished materials Laminates Polymer industry, paints, wood Technology of polymers |
title | Strength of quasi-isotropic laminates under off-axis loading |
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