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dc.creatorĆetković, Marina
dc.date.accessioned2019-04-19T14:24:41Z
dc.date.available2019-04-19T14:24:41Z
dc.date.issued2015
dc.identifier.issn0263-8223
dc.identifier.urihttps://grafar.grf.bg.ac.rs/handle/123456789/729
dc.description.abstractThe objective of this paper is thermo-mechanical bending of laminated composite and sandwich plates subjected to mechanical load and linearly varying through the thickness temperature field. Mathematical model, based on layer-wise displacement field of Reddy, is formulated using small deflection linear-elasticity theory. The principle of virtual displacements (PVD) is used to obtain the strong and the weak form of the mathematical model. The weak form is discretized using the isoparametric finite element approximation, while the analytical solution is derived from the strong form. The originally coded MATLAB program is used to investigate the influence of plate geometry and degree of material orthotropy on thermo-mechanical response of laminate composite and sandwich plates. The accuracy of the numerical model is verified by comparison with the available results from the literature and some new results are presented.en
dc.publisherElsevier Ltd
dc.relationinfo:eu-repo/grantAgreement/MESTD/Technological Development (TD or TR)/36048/RS//
dc.rightsrestrictedAccess
dc.sourceComposite Structures
dc.subjectLaminatesen
dc.subjectThermomechanicalen
dc.subjectAnalytical modelingen
dc.subjectFinite element analysis (FEM)en
dc.titleThermo-mechanical bending of laminated composite and sandwich plates using layerwise displacement modelen
dc.typearticle
dc.rights.licenseARR
dc.citation.epage399
dc.citation.other125: 388-399
dc.citation.rankaM21
dc.citation.spage388
dc.citation.volume125
dc.identifier.doi10.1016/j.compstruct.2015.01.051
dc.identifier.scopus2-s2.0-84923352103
dc.identifier.wos000353177600040
dc.type.versionpublishedVersion


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Приказ основних података о документу