Delamination modeling of laminate plate made of sublaminates
The paper presents the mixed-mode delamination of plates made of sublaminates. To this purpose an opening load mode of delamination is proposed as failure model. The failure model is implemented in ANSYS code to calculate the mixed-mode delamination response as energy release rate. The analysis is b...
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description | The paper presents the mixed-mode delamination of plates made of sublaminates. To this purpose an opening load mode of delamination is proposed as failure model. The failure model is implemented in ANSYS code to calculate the mixed-mode delamination response as energy release rate. The analysis is based on interface techniques. Within the interface finite element modeling there are calculated the individual components of damage parameters as spring reaction forces, relative displacements and energy release rates along the lamination front. |
doi_str_mv | 10.1063/1.4992420 |
format | Conference Proceeding |
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To this purpose an opening load mode of delamination is proposed as failure model. The failure model is implemented in ANSYS code to calculate the mixed-mode delamination response as energy release rate. The analysis is based on interface techniques. Within the interface finite element modeling there are calculated the individual components of damage parameters as spring reaction forces, relative displacements and energy release rates along the lamination front.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/1.4992420</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Delamination ; Energy release rate ; Finite element method ; Mathematical models ; Modelling</subject><ispartof>AIP conference proceedings, 2017, Vol.1863 (1)</ispartof><rights>Author(s)</rights><rights>2017 Author(s). Published by AIP Publishing.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://pubs.aip.org/acp/article-lookup/doi/10.1063/1.4992420$$EHTML$$P50$$Gscitation$$H</linktohtml><link.rule.ids>309,310,314,777,781,786,787,791,4498,23911,23912,25121,27905,27906,76133</link.rule.ids></links><search><contributor>Simos, Theodore</contributor><contributor>Tsitouras, Charalambos</contributor><creatorcontrib>Kormaníková, Eva</creatorcontrib><creatorcontrib>Kotrasová, Kamila</creatorcontrib><title>Delamination modeling of laminate plate made of sublaminates</title><title>AIP conference proceedings</title><description>The paper presents the mixed-mode delamination of plates made of sublaminates. To this purpose an opening load mode of delamination is proposed as failure model. The failure model is implemented in ANSYS code to calculate the mixed-mode delamination response as energy release rate. The analysis is based on interface techniques. Within the interface finite element modeling there are calculated the individual components of damage parameters as spring reaction forces, relative displacements and energy release rates along the lamination front.</description><subject>Delamination</subject><subject>Energy release rate</subject><subject>Finite element method</subject><subject>Mathematical models</subject><subject>Modelling</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2017</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNp9kE1LxDAQhoMoWFcP_oOCN6FrJp8teJH1Exa8KHgLaZNIl7apTSv4703dijcvM_DOMx_vIHQOeA1Y0CtYs6IgjOADlADnkEkB4hAlGBcsI4y-HaOTEHYYk0LKPEHXt7bRbd3psfZd2npjm7p7T71LF9mmfTPHVhs7y2EqfyvhFB053QR7tuQVer2_e9k8Ztvnh6fNzTbrCadjRiUXNgfDnKyI08KU8VQdFce1w9xYqR0tuZVSViWvMBORyrXjkDshiaYrdLGf2w_-Y7JhVDs_DV1cqQiAwNFxQSJ1uadCVY8_flQ_1K0evtSnHxSo5TOqN-4_GLCaX_nXQL8BS1llgA</recordid><startdate>20170721</startdate><enddate>20170721</enddate><creator>Kormaníková, Eva</creator><creator>Kotrasová, Kamila</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20170721</creationdate><title>Delamination modeling of laminate plate made of sublaminates</title><author>Kormaníková, Eva ; Kotrasová, Kamila</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p253t-3756e81d4f7c2fa6db106ae81f5af05de7af3b5e777cb5c0462fa8af518f672a3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Delamination</topic><topic>Energy release rate</topic><topic>Finite element method</topic><topic>Mathematical models</topic><topic>Modelling</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Kormaníková, Eva</creatorcontrib><creatorcontrib>Kotrasová, Kamila</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Kormaníková, Eva</au><au>Kotrasová, Kamila</au><au>Simos, Theodore</au><au>Tsitouras, Charalambos</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Delamination modeling of laminate plate made of sublaminates</atitle><btitle>AIP conference proceedings</btitle><date>2017-07-21</date><risdate>2017</risdate><volume>1863</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>The paper presents the mixed-mode delamination of plates made of sublaminates. To this purpose an opening load mode of delamination is proposed as failure model. The failure model is implemented in ANSYS code to calculate the mixed-mode delamination response as energy release rate. The analysis is based on interface techniques. Within the interface finite element modeling there are calculated the individual components of damage parameters as spring reaction forces, relative displacements and energy release rates along the lamination front.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/1.4992420</doi><tpages>4</tpages></addata></record> |
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source | AIP Journals Complete |
subjects | Delamination Energy release rate Finite element method Mathematical models Modelling |
title | Delamination modeling of laminate plate made of sublaminates |
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