Response of GLARE fiber–metal laminates under radial in-plane preloading and lateral indentation
This article deals with the static response of thin circular clamped GLAss REinforced (GLARE) fiber–metal laminates subjected to radial in-plane tensile preloading and lateral indentation by a hemispherical indentor simultaneously. The response is initially predicted using ANSYS software and nonline...
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Veröffentlicht in: | Journal of reinforced plastics and composites 2015-09, Vol.34 (17), p.1392-1402 |
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description | This article deals with the static response of thin circular clamped GLAss REinforced (GLARE) fiber–metal laminates subjected to radial in-plane tensile preloading and lateral indentation by a hemispherical indentor simultaneously. The response is initially predicted using ANSYS software and nonlinear analysis. From this analysis, the load-indentation and strain energy-indentation curves are calculated. Regression of the obtained Finite Element Method (FEM) results, using specific load-indentation relation, reveals that the response of the GLARE plates can be predicted with this relation. It also reveals how preloading alters the load-indentation relation of the GLARE plates. Then, analytical formulas are derived to predict the GLARE plate indentation load and strain energy as a function of central plate deflection and the magnitude of preloading. The derived analytical formulas are applied successfully for preloaded GLARE 2-2/1-0.3, GLARE 3-3/2-0.4 and GLARE 3-3/2-0.3 circular plates with various diameters. The analytically predicted load-indentation and strain energy-indentation curves are compared with corresponding FEM results and a very good agreement is found. |
doi_str_mv | 10.1177/0731684415592058 |
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The response is initially predicted using ANSYS software and nonlinear analysis. From this analysis, the load-indentation and strain energy-indentation curves are calculated. Regression of the obtained Finite Element Method (FEM) results, using specific load-indentation relation, reveals that the response of the GLARE plates can be predicted with this relation. It also reveals how preloading alters the load-indentation relation of the GLARE plates. Then, analytical formulas are derived to predict the GLARE plate indentation load and strain energy as a function of central plate deflection and the magnitude of preloading. The derived analytical formulas are applied successfully for preloaded GLARE 2-2/1-0.3, GLARE 3-3/2-0.4 and GLARE 3-3/2-0.3 circular plates with various diameters. The analytically predicted load-indentation and strain energy-indentation curves are compared with corresponding FEM results and a very good agreement is found.</description><identifier>ISSN: 0731-6844</identifier><identifier>EISSN: 1530-7964</identifier><identifier>DOI: 10.1177/0731684415592058</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><subject>Fiber-metal laminates ; Finite element method ; Glare ; Indentation ; Mathematical analysis ; Plates ; Regression analysis ; Strain</subject><ispartof>Journal of reinforced plastics and composites, 2015-09, Vol.34 (17), p.1392-1402</ispartof><rights>The Author(s) 2015</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c314t-ee128425511a261bf80661833565b2e68201685522e57d99064c922356618123</citedby><cites>FETCH-LOGICAL-c314t-ee128425511a261bf80661833565b2e68201685522e57d99064c922356618123</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/0731684415592058$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/0731684415592058$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,780,784,21819,27924,27925,43621,43622</link.rule.ids></links><search><creatorcontrib>Bikakis, George SE</creatorcontrib><title>Response of GLARE fiber–metal laminates under radial in-plane preloading and lateral indentation</title><title>Journal of reinforced plastics and composites</title><description>This article deals with the static response of thin circular clamped GLAss REinforced (GLARE) fiber–metal laminates subjected to radial in-plane tensile preloading and lateral indentation by a hemispherical indentor simultaneously. The response is initially predicted using ANSYS software and nonlinear analysis. From this analysis, the load-indentation and strain energy-indentation curves are calculated. Regression of the obtained Finite Element Method (FEM) results, using specific load-indentation relation, reveals that the response of the GLARE plates can be predicted with this relation. It also reveals how preloading alters the load-indentation relation of the GLARE plates. Then, analytical formulas are derived to predict the GLARE plate indentation load and strain energy as a function of central plate deflection and the magnitude of preloading. The derived analytical formulas are applied successfully for preloaded GLARE 2-2/1-0.3, GLARE 3-3/2-0.4 and GLARE 3-3/2-0.3 circular plates with various diameters. The analytically predicted load-indentation and strain energy-indentation curves are compared with corresponding FEM results and a very good agreement is found.</description><subject>Fiber-metal laminates</subject><subject>Finite element method</subject><subject>Glare</subject><subject>Indentation</subject><subject>Mathematical analysis</subject><subject>Plates</subject><subject>Regression analysis</subject><subject>Strain</subject><issn>0731-6844</issn><issn>1530-7964</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2015</creationdate><recordtype>article</recordtype><recordid>eNp1kD9PwzAQxS0EEqWwM3pkCfgc24nHqip_pEpIVffISS5VqsQOdjKw8R34hnwSHMqExHTSvd873XuE3AK7B8iyB5aloHIhQErNmczPyAJkypJMK3FOFrOczPoluQrhyBgHIcSClDsMg7MBqWvo03a129CmLdF_fXz2OJqOdqZvrRkx0MnW6Kk3dRvXrU2Gzlikg8fOxZ09UGPriI_of_Qa7WjG1tlrctGYLuDN71yS_eNmv35Otq9PL-vVNqlSEGOCCDwXXEoAwxWUTc6UgjxNpZIlR5VzFgNKyTnKrNaaKVFpzqMcKeDpktydzg7evU0YxqJvQ4Xd_KWbQhFLyrTONVcRZSe08i4Ej00x-LY3_r0AVsxtFn_bjJbkZAnmgMXRTd7GLP_z3y_vcxE</recordid><startdate>20150901</startdate><enddate>20150901</enddate><creator>Bikakis, George SE</creator><general>SAGE Publications</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>20150901</creationdate><title>Response of GLARE fiber–metal laminates under radial in-plane preloading and lateral indentation</title><author>Bikakis, George SE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c314t-ee128425511a261bf80661833565b2e68201685522e57d99064c922356618123</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2015</creationdate><topic>Fiber-metal laminates</topic><topic>Finite element method</topic><topic>Glare</topic><topic>Indentation</topic><topic>Mathematical analysis</topic><topic>Plates</topic><topic>Regression analysis</topic><topic>Strain</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Bikakis, George SE</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Journal of reinforced plastics and composites</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Bikakis, George SE</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Response of GLARE fiber–metal laminates under radial in-plane preloading and lateral indentation</atitle><jtitle>Journal of reinforced plastics and composites</jtitle><date>2015-09-01</date><risdate>2015</risdate><volume>34</volume><issue>17</issue><spage>1392</spage><epage>1402</epage><pages>1392-1402</pages><issn>0731-6844</issn><eissn>1530-7964</eissn><abstract>This article deals with the static response of thin circular clamped GLAss REinforced (GLARE) fiber–metal laminates subjected to radial in-plane tensile preloading and lateral indentation by a hemispherical indentor simultaneously. The response is initially predicted using ANSYS software and nonlinear analysis. From this analysis, the load-indentation and strain energy-indentation curves are calculated. Regression of the obtained Finite Element Method (FEM) results, using specific load-indentation relation, reveals that the response of the GLARE plates can be predicted with this relation. It also reveals how preloading alters the load-indentation relation of the GLARE plates. Then, analytical formulas are derived to predict the GLARE plate indentation load and strain energy as a function of central plate deflection and the magnitude of preloading. The derived analytical formulas are applied successfully for preloaded GLARE 2-2/1-0.3, GLARE 3-3/2-0.4 and GLARE 3-3/2-0.3 circular plates with various diameters. The analytically predicted load-indentation and strain energy-indentation curves are compared with corresponding FEM results and a very good agreement is found.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/0731684415592058</doi><tpages>11</tpages></addata></record> |
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subjects | Fiber-metal laminates Finite element method Glare Indentation Mathematical analysis Plates Regression analysis Strain |
title | Response of GLARE fiber–metal laminates under radial in-plane preloading and lateral indentation |
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