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Non-linear finite element analysis of thin composite structures

dc.contributor.authorMoita, José Mateus Simõespt_PT
dc.contributor.authorSoares, Cristovão M. Motapt_PT
dc.contributor.authorSoares, Carlos A. Motapt_PT
dc.date.accessioned2009-02-13T17:09:35Z
dc.date.available2009-02-13T17:09:35Z
dc.date.issued1997
dc.description.abstractA non-conforming three-node triangular finite element with 18 degree of freedom, is used in conjugation with the Kirchhoff theory for the non-linear analysis of thin composite plate-shell structure. The formulation of the geometrically non-linear analysis is based on an updated Lagrangian formulation associated with the Newton-Raphson iterative technique, which incorporates an automatic arc-length control procedure.pt_PT
dc.formatapplication/pdfpt_PT
dc.identifier.citationICCM-11 PROCEEDINGS ICCM-11 Proceedings. - Australia, 1997. - VoI. 6, p. 808-818pt_PT
dc.identifier.urihttp://hdl.handle.net/10400.1/103
dc.language.isoengpt_PT
dc.relation.urihttp://www.bib.ualg.pt/artigos/DocentesEST/MOINonLiFin.pdfpt_PT
dc.rights.uriopenAccessen
dc.subjectElementos finitospt_PT
dc.subject620pt_PT
dc.subjectNon-linear analysispt_PT
dc.subjectFinite elementspt_PT
dc.subjectMultilaminate shellspt_PT
dc.titleNon-linear finite element analysis of thin composite structurespt_PT
dc.typeconference object
dspace.entity.typePublication
rcaap.typeconferenceObjectpt_PT

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