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Mode III interlaminar fracture of carbon/epoxy laminates using the edge crack torsion (ECT) test

dc.contributor.authorMorais, A. B. de
dc.contributor.authorPereira, A. B.
dc.contributor.authorMoura, M. F. S. F. de
dc.contributor.authorMagalhães, A. G.
dc.date.accessioned2014-06-12T11:59:26Z
dc.date.available2014-06-12T11:59:26Z
dc.date.issued2009
dc.description.abstractThe mode III interlaminar fracture of carbon/epoxy laminates was evaluated with the edge crack torsion (ECT) test. Three-dimensional finite element analyses were performed in order to select two specimen geometries and an experimental data reduction scheme. Test results showed considerable non-linearity before the maximum load point and a significant R-curve effect. These features prevented an accurate definition of the initiation point. Nevertheless, analyses of non-linearity zones showed two likely initiation points corresponding to GIIIc values between 850 and 1100 J/m2 for both specimen geometries. Although any of these values is realistic, the range is too broad, thus showing the limitations of the ECT test and the need for further research.por
dc.identifier.doi10.1016/j.compscitech.2008.12.019pt_PT
dc.identifier.issn0266-3538
dc.identifier.urihttp://hdl.handle.net/10400.22/4542
dc.language.isoengpor
dc.peerreviewedyespor
dc.publisherElsevierpor
dc.relation.ispartofseriesComposites Science and Technology; Vol. 69, Issue 5
dc.relation.publisherversionhttp://www.sciencedirect.com/science/article/pii/S0266353809000049por
dc.subjectPolymer–matrix composites (PMCs)por
dc.subjectFracture toughnesspor
dc.subjectDelaminationpor
dc.subjectFinite element analysis (FEA)por
dc.subjectMode IIIpor
dc.titleMode III interlaminar fracture of carbon/epoxy laminates using the edge crack torsion (ECT) testpor
dc.typejournal article
dspace.entity.typePublication
oaire.citation.endPage676por
oaire.citation.startPage670por
oaire.citation.titleComposites Science and Technologypor
oaire.citation.volume69por
rcaap.rightsopenAccesspor
rcaap.typearticlepor

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