Damage analysis of laminated composites using a new coupled micro-meso approach
ABSTRACT In this study, the simplicity and strong physical meaning of micromechanics approach and capability of mesomechanics approach for damage analysis of structures with complex loadings are employed to develop a new micro‐meso approach. For this purpose, a new micromechanics model is developed...
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| Veröffentlicht in: | Fatigue & fracture of engineering materials & structures 2010-07, Vol.33 (7), p.420-435 |
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| container_issue | 7 |
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| container_title | Fatigue & fracture of engineering materials & structures |
| container_volume | 33 |
| creator | FARROKHABADI, A. HOSSEINI-TOUDESHKY, H. MOHAMMADI, B. |
| description | ABSTRACT
In this study, the simplicity and strong physical meaning of micromechanics approach and capability of mesomechanics approach for damage analysis of structures with complex loadings are employed to develop a new micro‐meso approach. For this purpose, a new micromechanics model is developed to predict the matrix cracking initiation and evolution in laminated composites. These damage initiation and evolution are replaced with the damage criteria and flow rule in the continuum damage approach, respectively. The results of this procedure are used in the FEM damage analyses of laminated composites to predict constitutive response of layered composites. It is shown that, the predicted stress distribution and strain energy in a lamina unit cell are in good agreement with the finite element results. Furthermore, it is shown that the predicted stress–strain behaviours are in good agreement with the available experimental results for various laminates with different lay‐ups. |
| doi_str_mv | 10.1111/j.1460-2695.2010.01456.x |
| format | Article |
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In this study, the simplicity and strong physical meaning of micromechanics approach and capability of mesomechanics approach for damage analysis of structures with complex loadings are employed to develop a new micro‐meso approach. For this purpose, a new micromechanics model is developed to predict the matrix cracking initiation and evolution in laminated composites. These damage initiation and evolution are replaced with the damage criteria and flow rule in the continuum damage approach, respectively. The results of this procedure are used in the FEM damage analyses of laminated composites to predict constitutive response of layered composites. It is shown that, the predicted stress distribution and strain energy in a lamina unit cell are in good agreement with the finite element results. Furthermore, it is shown that the predicted stress–strain behaviours are in good agreement with the available experimental results for various laminates with different lay‐ups.</description><identifier>ISSN: 8756-758X</identifier><identifier>EISSN: 1460-2695</identifier><identifier>DOI: 10.1111/j.1460-2695.2010.01456.x</identifier><identifier>CODEN: FFESEY</identifier><language>eng</language><publisher>Oxford, UK: Blackwell Publishing Ltd</publisher><subject>Accuracy ; Applied sciences ; Composite materials ; Crack initiation ; Damage ; damage analysis ; Evolution ; Exact sciences and technology ; FEM ; Finite element method ; Laminates ; Mathematical models ; Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology ; mesomechanics ; Metals. Metallurgy ; Micromechanics ; transverse cracking</subject><ispartof>Fatigue & fracture of engineering materials & structures, 2010-07, Vol.33 (7), p.420-435</ispartof><rights>2010 Blackwell Publishing Ltd.</rights><rights>2015 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c4406-b8eb2f8ab3f591508f998124c340b9fdbc1202ee385334bf599d7a5127e526ab3</citedby><cites>FETCH-LOGICAL-c4406-b8eb2f8ab3f591508f998124c340b9fdbc1202ee385334bf599d7a5127e526ab3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://onlinelibrary.wiley.com/doi/pdf/10.1111%2Fj.1460-2695.2010.01456.x$$EPDF$$P50$$Gwiley$$H</linktopdf><linktohtml>$$Uhttps://onlinelibrary.wiley.com/doi/full/10.1111%2Fj.1460-2695.2010.01456.x$$EHTML$$P50$$Gwiley$$H</linktohtml><link.rule.ids>314,780,784,1416,27923,27924,45573,45574</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=22838369$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>FARROKHABADI, A.</creatorcontrib><creatorcontrib>HOSSEINI-TOUDESHKY, H.</creatorcontrib><creatorcontrib>MOHAMMADI, B.</creatorcontrib><title>Damage analysis of laminated composites using a new coupled micro-meso approach</title><title>Fatigue & fracture of engineering materials & structures</title><description>ABSTRACT
In this study, the simplicity and strong physical meaning of micromechanics approach and capability of mesomechanics approach for damage analysis of structures with complex loadings are employed to develop a new micro‐meso approach. For this purpose, a new micromechanics model is developed to predict the matrix cracking initiation and evolution in laminated composites. These damage initiation and evolution are replaced with the damage criteria and flow rule in the continuum damage approach, respectively. The results of this procedure are used in the FEM damage analyses of laminated composites to predict constitutive response of layered composites. It is shown that, the predicted stress distribution and strain energy in a lamina unit cell are in good agreement with the finite element results. Furthermore, it is shown that the predicted stress–strain behaviours are in good agreement with the available experimental results for various laminates with different lay‐ups.</description><subject>Accuracy</subject><subject>Applied sciences</subject><subject>Composite materials</subject><subject>Crack initiation</subject><subject>Damage</subject><subject>damage analysis</subject><subject>Evolution</subject><subject>Exact sciences and technology</subject><subject>FEM</subject><subject>Finite element method</subject><subject>Laminates</subject><subject>Mathematical models</subject><subject>Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology</subject><subject>mesomechanics</subject><subject>Metals. Metallurgy</subject><subject>Micromechanics</subject><subject>transverse cracking</subject><issn>8756-758X</issn><issn>1460-2695</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2010</creationdate><recordtype>article</recordtype><recordid>eNqNkE1PGzEQhq2qSE2B_2BVqnra4O_1HjggIBQJgdSCyM2adbzU6X51JyuSf18vQTn0VF9szbzPO56XEMrZnKdztp5zZVgmTKHngqUq40qb-fYDmR0aH8nM5tpkubbLT-Qz4poxbpSUM_JwBQ28BAot1DuMSLuK1tDEFjZhRX3X9B3GTUA6YmxfKNA2vKby2Nep3UQ_dFkTsKPQ90MH_tcJOaqgxnD6fh-Tp8X14-X37O7h5vby4i7zSjGTlTaUorJQykoXXDNbFYXlQnmpWFlUq9JzwUQI0mopVZlExSoHzUUetDAJOybf9r5p7J8x4MY1EX2oa2hDN6LLtcyNNKJIyi__KNfdOKR10WkmOeOyYElk96K0EOIQKtcPsYFh5zhzU85u7aY43RSnm3J2bzm7bUK_vvsDeqirAVof8cALYaWVZvrH-V73Guuw-29_t1hcT6_EZ3s-4iZsDzwMv53JZa7d8_2N-7l8_vGollfOyr8Bpp8V</recordid><startdate>201007</startdate><enddate>201007</enddate><creator>FARROKHABADI, A.</creator><creator>HOSSEINI-TOUDESHKY, H.</creator><creator>MOHAMMADI, B.</creator><general>Blackwell Publishing Ltd</general><general>Blackwell</general><general>Wiley Subscription Services, Inc</general><scope>BSCLL</scope><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>201007</creationdate><title>Damage analysis of laminated composites using a new coupled micro-meso approach</title><author>FARROKHABADI, A. ; HOSSEINI-TOUDESHKY, H. ; MOHAMMADI, B.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c4406-b8eb2f8ab3f591508f998124c340b9fdbc1202ee385334bf599d7a5127e526ab3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2010</creationdate><topic>Accuracy</topic><topic>Applied sciences</topic><topic>Composite materials</topic><topic>Crack initiation</topic><topic>Damage</topic><topic>damage analysis</topic><topic>Evolution</topic><topic>Exact sciences and technology</topic><topic>FEM</topic><topic>Finite element method</topic><topic>Laminates</topic><topic>Mathematical models</topic><topic>Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology</topic><topic>mesomechanics</topic><topic>Metals. Metallurgy</topic><topic>Micromechanics</topic><topic>transverse cracking</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>FARROKHABADI, A.</creatorcontrib><creatorcontrib>HOSSEINI-TOUDESHKY, H.</creatorcontrib><creatorcontrib>MOHAMMADI, B.</creatorcontrib><collection>Istex</collection><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Civil Engineering Abstracts</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Fatigue & fracture of engineering materials & structures</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>FARROKHABADI, A.</au><au>HOSSEINI-TOUDESHKY, H.</au><au>MOHAMMADI, B.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Damage analysis of laminated composites using a new coupled micro-meso approach</atitle><jtitle>Fatigue & fracture of engineering materials & structures</jtitle><date>2010-07</date><risdate>2010</risdate><volume>33</volume><issue>7</issue><spage>420</spage><epage>435</epage><pages>420-435</pages><issn>8756-758X</issn><eissn>1460-2695</eissn><coden>FFESEY</coden><abstract>ABSTRACT
In this study, the simplicity and strong physical meaning of micromechanics approach and capability of mesomechanics approach for damage analysis of structures with complex loadings are employed to develop a new micro‐meso approach. For this purpose, a new micromechanics model is developed to predict the matrix cracking initiation and evolution in laminated composites. These damage initiation and evolution are replaced with the damage criteria and flow rule in the continuum damage approach, respectively. The results of this procedure are used in the FEM damage analyses of laminated composites to predict constitutive response of layered composites. It is shown that, the predicted stress distribution and strain energy in a lamina unit cell are in good agreement with the finite element results. Furthermore, it is shown that the predicted stress–strain behaviours are in good agreement with the available experimental results for various laminates with different lay‐ups.</abstract><cop>Oxford, UK</cop><pub>Blackwell Publishing Ltd</pub><doi>10.1111/j.1460-2695.2010.01456.x</doi><tpages>16</tpages></addata></record> |
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| ispartof | Fatigue & fracture of engineering materials & structures, 2010-07, Vol.33 (7), p.420-435 |
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| language | eng |
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| source | Wiley Online Library All Journals |
| subjects | Accuracy Applied sciences Composite materials Crack initiation Damage damage analysis Evolution Exact sciences and technology FEM Finite element method Laminates Mathematical models Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology mesomechanics Metals. Metallurgy Micromechanics transverse cracking |
| title | Damage analysis of laminated composites using a new coupled micro-meso approach |
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