Loading…
Mixed mode I + II interlaminar fracture of carbon/epoxy laminates
This paper reports a study of the mixed mode I + II fracture of carbon/epoxy unidirectional and multidirectional specimens with symmetric, quasi-symmetric and markedly asymmetric legs. A beam model was developed for predicting the compliance and total strain energy release rate, G. Its predictions a...
Saved in:
| Published in: | Composites. Part A, Applied science and manufacturing Applied science and manufacturing, 2008-02, Vol.39 (2), p.322-333 |
|---|---|
| Main Authors: | , |
| Format: | Article |
| Language: | English |
| Subjects: | |
| Citations: | Items that this one cites Items that cite this one |
| Online Access: | Get full text |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| cited_by | cdi_FETCH-LOGICAL-c3733-f7867ca43f5b3a8a83fd5dcf90d34871c1de48d047a96d6ccbd1b78b026ef2013 |
|---|---|
| cites | cdi_FETCH-LOGICAL-c3733-f7867ca43f5b3a8a83fd5dcf90d34871c1de48d047a96d6ccbd1b78b026ef2013 |
| container_end_page | 333 |
| container_issue | 2 |
| container_start_page | 322 |
| container_title | Composites. Part A, Applied science and manufacturing |
| container_volume | 39 |
| creator | Pereira, A.B. de Morais, A.B. |
| description | This paper reports a study of the mixed mode I
+
II fracture of carbon/epoxy unidirectional and multidirectional specimens with symmetric, quasi-symmetric and markedly asymmetric legs. A beam model was developed for predicting the compliance and total strain energy release rate,
G. Its predictions agreed well with three-dimensional finite element models and with experimental data of double cantilever beam, end-notched flexure and mixed-mode bending tests. The mode mix was determined from a virtual crack closure technique limit value analysis, in order to overcome ambiguity for delaminations between differently oriented plies. Initiation
G
c values versus mode II ratio
G
II/
G plots had practically identical shapes, showing a linear
G
c increase with
G
II/
G
⩾
25%. Multidirectional specimens with quasi-symmetric and markedly asymmetric legs had similar
G
c values. |
| doi_str_mv | 10.1016/j.compositesa.2007.10.013 |
| format | article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_32103289</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S1359835X07002151</els_id><sourcerecordid>32103289</sourcerecordid><originalsourceid>FETCH-LOGICAL-c3733-f7867ca43f5b3a8a83fd5dcf90d34871c1de48d047a96d6ccbd1b78b026ef2013</originalsourceid><addsrcrecordid>eNqNkF1LwzAUhoMoOKf_IV7ojbRLmn6kl2P4MZh4o-BdSJMTyGibmnQy_72ZHeKlVwk5T87D-yJ0TUlKCS0X21S5bnDBjhBkmhFSxfeUUHaCZpRXPCl4Tk7jnRV1wlnxfo4uQtgSQhir6Qwtn-0eNO6cBrzGd3i9xrYfwbeys7302Hipxp0H7AxW0jeuX8Dg9l94AqL1Ep0Z2Qa4Op5z9PZw_7p6SjYvj-vVcpMoVjGWmIqXlZI5M0XDJJecGV1oZWqiWc4rqqiGnGuSV7IudalUo2lT8YZkJZgsBpqj22nv4N3HDsIoOhsUtK3swe2CYBklLON1BOsJVN6F4MGIwdtO-i9BiTiUJrbiT2niUNphFB3x781RIoOSbUzfKxt-F0S0LMmPYzVxEBN_WvAiKAu9Am09qFFoZ_9h-waFNYh2</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>32103289</pqid></control><display><type>article</type><title>Mixed mode I + II interlaminar fracture of carbon/epoxy laminates</title><source>ScienceDirect Freedom Collection 2022-2024</source><creator>Pereira, A.B. ; de Morais, A.B.</creator><creatorcontrib>Pereira, A.B. ; de Morais, A.B.</creatorcontrib><description>This paper reports a study of the mixed mode I
+
II fracture of carbon/epoxy unidirectional and multidirectional specimens with symmetric, quasi-symmetric and markedly asymmetric legs. A beam model was developed for predicting the compliance and total strain energy release rate,
G. Its predictions agreed well with three-dimensional finite element models and with experimental data of double cantilever beam, end-notched flexure and mixed-mode bending tests. The mode mix was determined from a virtual crack closure technique limit value analysis, in order to overcome ambiguity for delaminations between differently oriented plies. Initiation
G
c values versus mode II ratio
G
II/
G plots had practically identical shapes, showing a linear
G
c increase with
G
II/
G
⩾
25%. Multidirectional specimens with quasi-symmetric and markedly asymmetric legs had similar
G
c values.</description><identifier>ISSN: 1359-835X</identifier><identifier>EISSN: 1878-5840</identifier><identifier>DOI: 10.1016/j.compositesa.2007.10.013</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>A. Polymer–matrix composites (PMCs) ; Applied sciences ; B. Delamination ; B. Fracture toughness ; C. Finite element analysis (FEA) ; Exact sciences and technology ; Forms of application and semi-finished materials ; Fracture mechanics (crack, fatigue, damage...) ; Fundamental areas of phenomenology (including applications) ; Laminates ; Physics ; Polymer industry, paints, wood ; Solid mechanics ; Structural and continuum mechanics ; Technology of polymers</subject><ispartof>Composites. Part A, Applied science and manufacturing, 2008-02, Vol.39 (2), p.322-333</ispartof><rights>2007 Elsevier Ltd</rights><rights>2008 INIST-CNRS</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c3733-f7867ca43f5b3a8a83fd5dcf90d34871c1de48d047a96d6ccbd1b78b026ef2013</citedby><cites>FETCH-LOGICAL-c3733-f7867ca43f5b3a8a83fd5dcf90d34871c1de48d047a96d6ccbd1b78b026ef2013</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,778,782,27911,27912</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=20066089$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Pereira, A.B.</creatorcontrib><creatorcontrib>de Morais, A.B.</creatorcontrib><title>Mixed mode I + II interlaminar fracture of carbon/epoxy laminates</title><title>Composites. Part A, Applied science and manufacturing</title><description>This paper reports a study of the mixed mode I
+
II fracture of carbon/epoxy unidirectional and multidirectional specimens with symmetric, quasi-symmetric and markedly asymmetric legs. A beam model was developed for predicting the compliance and total strain energy release rate,
G. Its predictions agreed well with three-dimensional finite element models and with experimental data of double cantilever beam, end-notched flexure and mixed-mode bending tests. The mode mix was determined from a virtual crack closure technique limit value analysis, in order to overcome ambiguity for delaminations between differently oriented plies. Initiation
G
c values versus mode II ratio
G
II/
G plots had practically identical shapes, showing a linear
G
c increase with
G
II/
G
⩾
25%. Multidirectional specimens with quasi-symmetric and markedly asymmetric legs had similar
G
c values.</description><subject>A. Polymer–matrix composites (PMCs)</subject><subject>Applied sciences</subject><subject>B. Delamination</subject><subject>B. Fracture toughness</subject><subject>C. Finite element analysis (FEA)</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Fracture mechanics (crack, fatigue, damage...)</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Laminates</subject><subject>Physics</subject><subject>Polymer industry, paints, wood</subject><subject>Solid mechanics</subject><subject>Structural and continuum mechanics</subject><subject>Technology of polymers</subject><issn>1359-835X</issn><issn>1878-5840</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2008</creationdate><recordtype>article</recordtype><recordid>eNqNkF1LwzAUhoMoOKf_IV7ojbRLmn6kl2P4MZh4o-BdSJMTyGibmnQy_72ZHeKlVwk5T87D-yJ0TUlKCS0X21S5bnDBjhBkmhFSxfeUUHaCZpRXPCl4Tk7jnRV1wlnxfo4uQtgSQhir6Qwtn-0eNO6cBrzGd3i9xrYfwbeys7302Hipxp0H7AxW0jeuX8Dg9l94AqL1Ep0Z2Qa4Op5z9PZw_7p6SjYvj-vVcpMoVjGWmIqXlZI5M0XDJJecGV1oZWqiWc4rqqiGnGuSV7IudalUo2lT8YZkJZgsBpqj22nv4N3HDsIoOhsUtK3swe2CYBklLON1BOsJVN6F4MGIwdtO-i9BiTiUJrbiT2niUNphFB3x781RIoOSbUzfKxt-F0S0LMmPYzVxEBN_WvAiKAu9Am09qFFoZ_9h-waFNYh2</recordid><startdate>200802</startdate><enddate>200802</enddate><creator>Pereira, A.B.</creator><creator>de Morais, A.B.</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>JG9</scope></search><sort><creationdate>200802</creationdate><title>Mixed mode I + II interlaminar fracture of carbon/epoxy laminates</title><author>Pereira, A.B. ; de Morais, A.B.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c3733-f7867ca43f5b3a8a83fd5dcf90d34871c1de48d047a96d6ccbd1b78b026ef2013</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2008</creationdate><topic>A. Polymer–matrix composites (PMCs)</topic><topic>Applied sciences</topic><topic>B. Delamination</topic><topic>B. Fracture toughness</topic><topic>C. Finite element analysis (FEA)</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Fracture mechanics (crack, fatigue, damage...)</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Laminates</topic><topic>Physics</topic><topic>Polymer industry, paints, wood</topic><topic>Solid mechanics</topic><topic>Structural and continuum mechanics</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Pereira, A.B.</creatorcontrib><creatorcontrib>de Morais, A.B.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><jtitle>Composites. Part A, Applied science and manufacturing</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Pereira, A.B.</au><au>de Morais, A.B.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Mixed mode I + II interlaminar fracture of carbon/epoxy laminates</atitle><jtitle>Composites. Part A, Applied science and manufacturing</jtitle><date>2008-02</date><risdate>2008</risdate><volume>39</volume><issue>2</issue><spage>322</spage><epage>333</epage><pages>322-333</pages><issn>1359-835X</issn><eissn>1878-5840</eissn><abstract>This paper reports a study of the mixed mode I
+
II fracture of carbon/epoxy unidirectional and multidirectional specimens with symmetric, quasi-symmetric and markedly asymmetric legs. A beam model was developed for predicting the compliance and total strain energy release rate,
G. Its predictions agreed well with three-dimensional finite element models and with experimental data of double cantilever beam, end-notched flexure and mixed-mode bending tests. The mode mix was determined from a virtual crack closure technique limit value analysis, in order to overcome ambiguity for delaminations between differently oriented plies. Initiation
G
c values versus mode II ratio
G
II/
G plots had practically identical shapes, showing a linear
G
c increase with
G
II/
G
⩾
25%. Multidirectional specimens with quasi-symmetric and markedly asymmetric legs had similar
G
c values.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.compositesa.2007.10.013</doi><tpages>12</tpages><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 1359-835X |
| ispartof | Composites. Part A, Applied science and manufacturing, 2008-02, Vol.39 (2), p.322-333 |
| issn | 1359-835X 1878-5840 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_32103289 |
| source | ScienceDirect Freedom Collection 2022-2024 |
| subjects | A. Polymer–matrix composites (PMCs) Applied sciences B. Delamination B. Fracture toughness C. Finite element analysis (FEA) Exact sciences and technology Forms of application and semi-finished materials Fracture mechanics (crack, fatigue, damage...) Fundamental areas of phenomenology (including applications) Laminates Physics Polymer industry, paints, wood Solid mechanics Structural and continuum mechanics Technology of polymers |
| title | Mixed mode I + II interlaminar fracture of carbon/epoxy laminates |
| url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-15T17%3A01%3A25IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Mixed%20mode%20I%20+%20II%20interlaminar%20fracture%20of%20carbon/epoxy%20laminates&rft.jtitle=Composites.%20Part%20A,%20Applied%20science%20and%20manufacturing&rft.au=Pereira,%20A.B.&rft.date=2008-02&rft.volume=39&rft.issue=2&rft.spage=322&rft.epage=333&rft.pages=322-333&rft.issn=1359-835X&rft.eissn=1878-5840&rft_id=info:doi/10.1016/j.compositesa.2007.10.013&rft_dat=%3Cproquest_cross%3E32103289%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c3733-f7867ca43f5b3a8a83fd5dcf90d34871c1de48d047a96d6ccbd1b78b026ef2013%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=32103289&rft_id=info:pmid/&rfr_iscdi=true |