Please use this identifier to cite or link to this item: http://hdl.handle.net/10773/21144
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dc.contributor.authorMorais, Alfredopt
dc.contributor.authorPereira, António Bastospt
dc.contributor.authorMoura, M. F. S. F. dept
dc.contributor.authorSilva, F. G. A.pt
dc.contributor.authorDourado, N.pt
dc.date.accessioned2017-12-13T12:27:59Z-
dc.date.issued2015-04-01-
dc.identifier.issn0263-8223pt
dc.identifier.urihttp://hdl.handle.net/10773/21144-
dc.description.abstractThis paper presents an experimental and numerical study of the mixed-mode I-II delamination of unidirectional carbon/epoxy laminates. Double cantilever beam, end-notched flexure and mixed-mode bending tests were conducted in order to cover the full range of mode-mix combinations. Finite element cohesive zone models with a bilinear softening cohesive law were subsequently employed to fit experimental load-displacement curves. This required a genetic algorithm to find optimal bilinear softening parameters. Good agreement was achieved between predicted and experimental curves. Furthermore, the bilinear softening parameters showed consistent variations with the global mode-mix that could be interpreted in terms of local damage mechanisms. Nevertheless, further research is needed to define mixed-mode tractions and separations leading to a unique cohesive law.pt
dc.language.isoengpt
dc.publisherElsevierpt
dc.rightsrestrictedAccesspor
dc.subjectDelaminationpt
dc.subjectMixed-mode I-IIpt
dc.subjectMixed-mode bendingpt
dc.subjectCohesive lawpt
dc.subjectInverse methodpt
dc.titleBilinear approximations to the mixed-mode I-II delamination cohesive law using an inverse methodpt
dc.typearticlept
dc.peerreviewedyespt
ua.distributioninternationalpt
degois.publication.firstPage361pt
degois.publication.lastPage366pt
degois.publication.titleComposite Structurespt
degois.publication.volume122pt
dc.date.embargo10000-01-01-
dc.identifier.doi10.1016/j.compstruct.2014.11.058pt
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