Please use this identifier to cite or link to this item: http://hdl.handle.net/10773/5247
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dc.contributor.authorMorais, A.B. dept
dc.contributor.authorPereira, A.B.pt
dc.date.accessioned2012-01-19T15:30:46Z-
dc.date.issued2007-
dc.identifier.issn1359-835Xpt
dc.identifier.urihttp://hdl.handle.net/10773/5247-
dc.description.abstractThis paper describes an experimental study involving double cantilever beam (DCB), end-notched flexure (ENF) and 4-point end-notched flexure (4ENF) tests on carbon/epoxy unidirectional specimens. The main purpose was to evaluate the so-called effective crack method (ECM), which avoids operator crack position monitoring. Extensive fibre bridging in DCB tests made the ECM inappropriate, as shown in subsequent finite element analyses. On the other hand, the ECM gave very consistent results from ENF tests, despite the usually unstable initiation. The present results confirmed some dependence of perceived initiation toughness values on ENF specimen geometry predicted in recent numerical studies. Differences between results of ENF and 4ENF tests could be explained by friction effects in the latter.pt
dc.description.sponsorshipFCT/FEDER EU fund - POCI/EME/57956/2004pt
dc.language.isoengpt
dc.publisherElsevierpt
dc.relation.urihttp://www.scopus.com/inward/record.url?eid=2-s2.0-33845444335&partnerID=40&md5=fdcce8057f9ffccebaa8c358715204d7
dc.rightsrestrictedAccesspor
dc.subjectDelaminationpt
dc.subjectFracture toughnesspt
dc.subjectFinite element analysis (FEA)pt
dc.subjectMechanical testingpt
dc.subjectEffective crack methodpt
dc.titleApplication of the effective crack method to mode I and mode II interlaminar fracture of carbon/epoxy unidirectional laminatespt
dc.typearticlept
dc.peerreviewedyespt
ua.distributioninternationalpt
degois.publication.firstPage785pt
degois.publication.issue3
degois.publication.issue3pt
degois.publication.lastPage794pt
degois.publication.titleComposites Part A: Applied Science and Manufacturingpt
degois.publication.volume38pt
dc.date.embargo10000-01-01-
dc.identifier.doi10.1016/j.compositesa.2006.09.001*
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