Numerical analysis of the influences of thermal stresses on the efficiency of bonded composite repair of cracked metallic panels
In this study, the three-dimensional finite element method is used to analyze the effects of the thermal residual stresses due to the adhesive curing on the efficiency of bonded composite repair of cracked aluminum panels. The variation of the stress intensity factor at the crack tip is used for eva...
Gespeichert in:
Veröffentlicht in: | Journal of composite materials 2017-11, Vol.51 (26), p.3701-3709 |
---|---|
Hauptverfasser: | , , , , |
Format: | Artikel |
Sprache: | eng |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 3709 |
---|---|
container_issue | 26 |
container_start_page | 3701 |
container_title | Journal of composite materials |
container_volume | 51 |
creator | Mhamdia, Rachid Serier, B Albedah, A Bachir Bouiadjra, B Kaddouri, K |
description | In this study, the three-dimensional finite element method is used to analyze the effects of the thermal residual stresses due to the adhesive curing on the efficiency of bonded composite repair of cracked aluminum panels. The variation of the stress intensity factor at the crack tip is used for evaluating the repair performances. The effects of the geometrical and the mechanical properties of the composite patch and the adhesive on the repair efficiency were highlighted. The obtained results show that the thermal residual stresses significantly increase the stress intensity factor at the crack tip which reduces the repair efficiency. |
doi_str_mv | 10.1177/0021998317692033 |
format | Article |
fullrecord | <record><control><sourceid>sage_cross</sourceid><recordid>TN_cdi_crossref_primary_10_1177_0021998317692033</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sage_id>10.1177_0021998317692033</sage_id><sourcerecordid>10.1177_0021998317692033</sourcerecordid><originalsourceid>FETCH-LOGICAL-c281t-2e196fb14f9c9e43fa5a052c651cb779acd335328d1ade3345a1a5b5e9cda2353</originalsourceid><addsrcrecordid>eNp1kLtOxDAQRS0EEstCT-kfCPgRx-sSrXhJK2hAoosmkzF4yUt2ttiOTyfh0SBRjXTPuVNcxs6luJDS2kshlHRupaUtnBJaH7CFNFpk1umXQ7aYcTbzY3aS0lYIYWVeLNjHw66lGBAaDh00-xQS7z0f34iHzjc76pB-k9hOVhojpTRn3ZdF3gcMk7afrarvaqo59u3QpzASjzRAiDPCCPg-sZZGaJqAfICOmnTKjjw0ic5-7pI931w_re-yzePt_fpqk6FayTFTJF3hK5l7h45y7cGAMAoLI7Gy1gHWWhutVrWEmrTODUgwlSGHNaiJLJn4_ouxTymSL4cYWoj7UopyXrD8u-BUyb4rCV6p3Pa7OC2U_vc_AUXlc2A</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>Numerical analysis of the influences of thermal stresses on the efficiency of bonded composite repair of cracked metallic panels</title><source>SAGE Complete A-Z List</source><creator>Mhamdia, Rachid ; Serier, B ; Albedah, A ; Bachir Bouiadjra, B ; Kaddouri, K</creator><creatorcontrib>Mhamdia, Rachid ; Serier, B ; Albedah, A ; Bachir Bouiadjra, B ; Kaddouri, K</creatorcontrib><description>In this study, the three-dimensional finite element method is used to analyze the effects of the thermal residual stresses due to the adhesive curing on the efficiency of bonded composite repair of cracked aluminum panels. The variation of the stress intensity factor at the crack tip is used for evaluating the repair performances. The effects of the geometrical and the mechanical properties of the composite patch and the adhesive on the repair efficiency were highlighted. The obtained results show that the thermal residual stresses significantly increase the stress intensity factor at the crack tip which reduces the repair efficiency.</description><identifier>ISSN: 0021-9983</identifier><identifier>EISSN: 1530-793X</identifier><identifier>DOI: 10.1177/0021998317692033</identifier><language>eng</language><publisher>London, England: SAGE Publications</publisher><ispartof>Journal of composite materials, 2017-11, Vol.51 (26), p.3701-3709</ispartof><rights>The Author(s) 2017</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c281t-2e196fb14f9c9e43fa5a052c651cb779acd335328d1ade3345a1a5b5e9cda2353</citedby><cites>FETCH-LOGICAL-c281t-2e196fb14f9c9e43fa5a052c651cb779acd335328d1ade3345a1a5b5e9cda2353</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/0021998317692033$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/0021998317692033$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,776,780,21800,27903,27904,43599,43600</link.rule.ids></links><search><creatorcontrib>Mhamdia, Rachid</creatorcontrib><creatorcontrib>Serier, B</creatorcontrib><creatorcontrib>Albedah, A</creatorcontrib><creatorcontrib>Bachir Bouiadjra, B</creatorcontrib><creatorcontrib>Kaddouri, K</creatorcontrib><title>Numerical analysis of the influences of thermal stresses on the efficiency of bonded composite repair of cracked metallic panels</title><title>Journal of composite materials</title><description>In this study, the three-dimensional finite element method is used to analyze the effects of the thermal residual stresses due to the adhesive curing on the efficiency of bonded composite repair of cracked aluminum panels. The variation of the stress intensity factor at the crack tip is used for evaluating the repair performances. The effects of the geometrical and the mechanical properties of the composite patch and the adhesive on the repair efficiency were highlighted. The obtained results show that the thermal residual stresses significantly increase the stress intensity factor at the crack tip which reduces the repair efficiency.</description><issn>0021-9983</issn><issn>1530-793X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp1kLtOxDAQRS0EEstCT-kfCPgRx-sSrXhJK2hAoosmkzF4yUt2ttiOTyfh0SBRjXTPuVNcxs6luJDS2kshlHRupaUtnBJaH7CFNFpk1umXQ7aYcTbzY3aS0lYIYWVeLNjHw66lGBAaDh00-xQS7z0f34iHzjc76pB-k9hOVhojpTRn3ZdF3gcMk7afrarvaqo59u3QpzASjzRAiDPCCPg-sZZGaJqAfICOmnTKjjw0ic5-7pI931w_re-yzePt_fpqk6FayTFTJF3hK5l7h45y7cGAMAoLI7Gy1gHWWhutVrWEmrTODUgwlSGHNaiJLJn4_ouxTymSL4cYWoj7UopyXrD8u-BUyb4rCV6p3Pa7OC2U_vc_AUXlc2A</recordid><startdate>201711</startdate><enddate>201711</enddate><creator>Mhamdia, Rachid</creator><creator>Serier, B</creator><creator>Albedah, A</creator><creator>Bachir Bouiadjra, B</creator><creator>Kaddouri, K</creator><general>SAGE Publications</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>201711</creationdate><title>Numerical analysis of the influences of thermal stresses on the efficiency of bonded composite repair of cracked metallic panels</title><author>Mhamdia, Rachid ; Serier, B ; Albedah, A ; Bachir Bouiadjra, B ; Kaddouri, K</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c281t-2e196fb14f9c9e43fa5a052c651cb779acd335328d1ade3345a1a5b5e9cda2353</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Mhamdia, Rachid</creatorcontrib><creatorcontrib>Serier, B</creatorcontrib><creatorcontrib>Albedah, A</creatorcontrib><creatorcontrib>Bachir Bouiadjra, B</creatorcontrib><creatorcontrib>Kaddouri, K</creatorcontrib><collection>CrossRef</collection><jtitle>Journal of composite materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Mhamdia, Rachid</au><au>Serier, B</au><au>Albedah, A</au><au>Bachir Bouiadjra, B</au><au>Kaddouri, K</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Numerical analysis of the influences of thermal stresses on the efficiency of bonded composite repair of cracked metallic panels</atitle><jtitle>Journal of composite materials</jtitle><date>2017-11</date><risdate>2017</risdate><volume>51</volume><issue>26</issue><spage>3701</spage><epage>3709</epage><pages>3701-3709</pages><issn>0021-9983</issn><eissn>1530-793X</eissn><abstract>In this study, the three-dimensional finite element method is used to analyze the effects of the thermal residual stresses due to the adhesive curing on the efficiency of bonded composite repair of cracked aluminum panels. The variation of the stress intensity factor at the crack tip is used for evaluating the repair performances. The effects of the geometrical and the mechanical properties of the composite patch and the adhesive on the repair efficiency were highlighted. The obtained results show that the thermal residual stresses significantly increase the stress intensity factor at the crack tip which reduces the repair efficiency.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/0021998317692033</doi><tpages>9</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0021-9983 |
ispartof | Journal of composite materials, 2017-11, Vol.51 (26), p.3701-3709 |
issn | 0021-9983 1530-793X |
language | eng |
recordid | cdi_crossref_primary_10_1177_0021998317692033 |
source | SAGE Complete A-Z List |
title | Numerical analysis of the influences of thermal stresses on the efficiency of bonded composite repair of cracked metallic panels |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-28T08%3A19%3A52IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-sage_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Numerical%20analysis%20of%20the%20influences%20of%20thermal%20stresses%20on%20the%20efficiency%20of%20bonded%20composite%20repair%20of%20cracked%20metallic%20panels&rft.jtitle=Journal%20of%20composite%20materials&rft.au=Mhamdia,%20Rachid&rft.date=2017-11&rft.volume=51&rft.issue=26&rft.spage=3701&rft.epage=3709&rft.pages=3701-3709&rft.issn=0021-9983&rft.eissn=1530-793X&rft_id=info:doi/10.1177/0021998317692033&rft_dat=%3Csage_cross%3E10.1177_0021998317692033%3C/sage_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rft_sage_id=10.1177_0021998317692033&rfr_iscdi=true |