Stress intensity factor for repaired crack with bonded composite patch under thermo-mechanical loading
In this study, the finite element method is used to analyze the effect of the thermal residual stresses resulting from adhesive curing on the performances of the bonded composite repair in aircraft structures. The stress intensity factor at the crack tip is chosen as the fracture criterion in order...
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| Veröffentlicht in: | Journal of reinforced plastics and composites 2011-03, Vol.30 (5), p.416-424 |
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| container_end_page | 424 |
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| container_issue | 5 |
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| container_title | Journal of reinforced plastics and composites |
| container_volume | 30 |
| creator | Mhamdia, R. Bouadjra, B. Bachir Serier, B. Ouddad, W. Feaugas, X. Touzain, S. |
| description | In this study, the finite element method is used to analyze the effect of the thermal residual stresses resulting from adhesive curing on the performances of the bonded composite repair in aircraft structures. The stress intensity factor at the crack tip is chosen as the fracture criterion in order to estimate the repair performances. The effects of the curing temperature, the geometrical properties of the patch, and the adhesive properties on the variation of the stress intensity factor are analyzed. The obtained results show a significant negative effect of the thermal residual stresses on the repair efficiency and this effect can be reduced if the different repair parameters are optimized. |
| doi_str_mv | 10.1177/0731684410397899 |
| format | Article |
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The obtained results show a significant negative effect of the thermal residual stresses on the repair efficiency and this effect can be reduced if the different repair parameters are optimized.</description><subject>Adhesive bonding</subject><subject>Aircraft structures</subject><subject>Application fields</subject><subject>Applied sciences</subject><subject>Bonding</subject><subject>Chemical Sciences</subject><subject>Curing</subject><subject>Exact sciences and technology</subject><subject>Fracture mechanics</subject><subject>Polymer industry, paints, wood</subject><subject>Repair</subject><subject>Residual stress</subject><subject>Stress intensity factor</subject><subject>Technology of polymers</subject><issn>0731-6844</issn><issn>1530-7964</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2011</creationdate><recordtype>article</recordtype><recordid>eNp1kD1rHDEQhkVwIGcnfUo1AbvYWF8nnUpj4jhw4CJJLWa1s145u6u1pEvwv7eWMy4MKYaBZ555i5eQz5x95dyYS2Yk1zulOJPW7Kx9RzZ8K1ljrFYnZLOem_X-gZzm_MCY4EqpDel_loQ50zAXnHMoT7QHX2KifZ2EC4SEHfUJ_B_6L5SBtnHuVhKnJVYf6QLFD_RQaaJlwDTFZkI_wBw8jHSM0IX5_iN538OY8dPLPiO_b779ur5t9nfff1xf7Ruv-LY0Co0UwFDoTnspBO48YwZa2W59BwhGGK20raTtGFTU9r0WoFprLNfCyDNyccwdYHRLChOkJxchuNurvVsZE8rYreR_eXXPj-6S4uMBc3FTyB7HEWaMh-y4NlxKpXa2quyo-hRzTti_ZnPm1vrd2_rry5eXdMi1iD7B7EN-_ROKK6MZq15z9DLco3uIhzTXgv6f-wzOIpKA</recordid><startdate>20110301</startdate><enddate>20110301</enddate><creator>Mhamdia, R.</creator><creator>Bouadjra, B. 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Bachir</creatorcontrib><creatorcontrib>Serier, B.</creatorcontrib><creatorcontrib>Ouddad, W.</creatorcontrib><creatorcontrib>Feaugas, X.</creatorcontrib><creatorcontrib>Touzain, S.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><collection>Hyper Article en Ligne (HAL)</collection><jtitle>Journal of reinforced plastics and composites</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Mhamdia, R.</au><au>Bouadjra, B. Bachir</au><au>Serier, B.</au><au>Ouddad, W.</au><au>Feaugas, X.</au><au>Touzain, S.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Stress intensity factor for repaired crack with bonded composite patch under thermo-mechanical loading</atitle><jtitle>Journal of reinforced plastics and composites</jtitle><date>2011-03-01</date><risdate>2011</risdate><volume>30</volume><issue>5</issue><spage>416</spage><epage>424</epage><pages>416-424</pages><issn>0731-6844</issn><eissn>1530-7964</eissn><coden>JRPCDW</coden><abstract>In this study, the finite element method is used to analyze the effect of the thermal residual stresses resulting from adhesive curing on the performances of the bonded composite repair in aircraft structures. The stress intensity factor at the crack tip is chosen as the fracture criterion in order to estimate the repair performances. The effects of the curing temperature, the geometrical properties of the patch, and the adhesive properties on the variation of the stress intensity factor are analyzed. The obtained results show a significant negative effect of the thermal residual stresses on the repair efficiency and this effect can be reduced if the different repair parameters are optimized.</abstract><cop>London, England</cop><pub>SAGE Publications</pub><doi>10.1177/0731684410397899</doi><tpages>9</tpages><orcidid>https://orcid.org/0000-0002-1368-2843</orcidid></addata></record> |
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| ispartof | Journal of reinforced plastics and composites, 2011-03, Vol.30 (5), p.416-424 |
| issn | 0731-6844 1530-7964 |
| language | eng |
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| source | SAGE Complete A-Z List |
| subjects | Adhesive bonding Aircraft structures Application fields Applied sciences Bonding Chemical Sciences Curing Exact sciences and technology Fracture mechanics Polymer industry, paints, wood Repair Residual stress Stress intensity factor Technology of polymers |
| title | Stress intensity factor for repaired crack with bonded composite patch under thermo-mechanical loading |
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