Thermal buckling of rectangular laminated plates with a hole

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dc.contributor.authorAvci, A
dc.contributor.authorKaya, S
dc.contributor.authorDaghan, B
dc.date.accessioned2020-03-26T16:58:21Z
dc.date.available2020-03-26T16:58:21Z
dc.date.issued2005
dc.departmentSelçuk Üniversitesien_US
dc.description.abstractThermal buckling analysis of symmetric and antisymmetric laminated composite plates with clamped and simply supported edges, and containing a hole is presented in this paper. The first-order shear deformation theory in conjunction with the variational energy method is employed in mathematical formulation. The eight-node Lagrangian finite element technique is used to find thermal buckling temperatures of isotropic, glass-epoxy and boron-epoxy laminates. The effects of hole size, angle of ply orientation, lay-up sequences, and boundary conditions on thermal buckling temperatures are investigated. The result is shown in graphical forms for various boundary conditions.en_US
dc.identifier.doi10.1177/1731684405043554en_US
dc.identifier.endpage272en_US
dc.identifier.issn0731-6844en_US
dc.identifier.issue3en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.startpage259en_US
dc.identifier.urihttps://dx.doi.org/10.1177/1731684405043554
dc.identifier.urihttps://hdl.handle.net/20.500.12395/19943
dc.identifier.volume24en_US
dc.identifier.wosWOS:000227136400003en_US
dc.identifier.wosqualityQ4en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherSAGE PUBLICATIONS LTDen_US
dc.relation.ispartofJOURNAL OF REINFORCED PLASTICS AND COMPOSITESen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.selcuk20240510_oaigen_US
dc.subjectcomposite platesen_US
dc.subjectthermal bucklingen_US
dc.subjectfinite element methoden_US
dc.titleThermal buckling of rectangular laminated plates with a holeen_US
dc.typeArticleen_US

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