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Numerical prediction of delamination onset in carbon/epoxy composites drilling

dc.contributor.authorDurão, Luís M.
dc.contributor.authorMoura, M. F. S. F. de
dc.contributor.authorMarques, A. T.
dc.date.accessioned2014-03-12T16:00:10Z
dc.date.available2014-03-12T16:00:10Z
dc.date.issued2008
dc.description.abstractDespite the fact that their physical properties make them an attractive family of materials, composites machining can cause several damage modes such as delamination, fibre pull-out, thermal degradation, and others. Minimization of axial thrust force during drilling reduces the probability of delamination onset, as it has been demonstrated by analytical models based on linear elastic fracture mechanics (LEFM). A finite element model considering solid elements of the ABAQUS® software library and interface elements including a cohesive damage model was developed in order to simulate thrust forces and delamination onset during drilling. Thrust force results for delamination onset are compared with existing analytical models.por
dc.identifier.doi10.1016/j.engfracmech.2007.03.009pt_PT
dc.identifier.issn0013-7944
dc.identifier.urihttp://hdl.handle.net/10400.22/4187
dc.language.isoengpor
dc.peerreviewedyespor
dc.publisherElsevierpor
dc.relation.ispartofseriesEngineering Fracture Mechanics; Vol. 75, Issue 9
dc.relation.publisherversionhttp://www.sciencedirect.com/science/article/pii/S0013794407001191por
dc.subjectDelaminationpor
dc.subjectFinite elementpor
dc.subjectCarbon fibre laminatespor
dc.titleNumerical prediction of delamination onset in carbon/epoxy composites drillingpor
dc.typejournal article
dspace.entity.typePublication
oaire.citation.endPage2778por
oaire.citation.startPage2767por
oaire.citation.titleEngineering Fracture Mechanicspor
oaire.citation.volume75por
person.familyNameDurão
person.givenNameLuís Miguel
person.identifier.orcid0000-0002-0002-5836
person.identifier.scopus-author-id14055887400
rcaap.rightsrestrictedAccesspor
rcaap.typearticlepor
relation.isAuthorOfPublication7b302bea-0227-4548-9635-ec55d5ea50f4
relation.isAuthorOfPublication.latestForDiscovery7b302bea-0227-4548-9635-ec55d5ea50f4

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