Thermal buckling of hybrid laminated composite plates with a hole

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dc.contributor.authorAvci, A
dc.contributor.authorSahin, OS
dc.contributor.authorUyaner, M
dc.date.accessioned2020-03-26T16:58:20Z
dc.date.available2020-03-26T16:58:20Z
dc.date.issued2005
dc.departmentSelçuk Üniversitesien_US
dc.description.abstractThermal buckling analysis of symmetric and antisymmetric cross-ply laminated hybrid composite plates with a hole subjected to a uniform temperature rise for different boundary conditions are presented in this paper. The first-order shear deformation theory in conjunction with variational energy method is employed in the mathematical formulation. The eight-node Lagrangian finite element technique is used for finding the thermal buckling temperatures of hybrid laminates. The effects of hole size, lay-up sequences and boundary conditions on the thermal buckling temperatures are investigated. The results are shown in graphical form for various conditions. (c) 2004 Published by Elsevier Ltd.en_US
dc.identifier.doi10.1016/j.compstruct.2004.03.017en_US
dc.identifier.endpage254en_US
dc.identifier.issn0263-8223en_US
dc.identifier.issn1879-1085en_US
dc.identifier.issue2en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.startpage247en_US
dc.identifier.urihttps://dx.doi.org/10.1016/j.compstruct.2004.03.017
dc.identifier.urihttps://hdl.handle.net/20.500.12395/19942
dc.identifier.volume68en_US
dc.identifier.wosWOS:000227692900012en_US
dc.identifier.wosqualityQ2en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherELSEVIER SCI LTDen_US
dc.relation.ispartofCOMPOSITE STRUCTURESen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.selcuk20240510_oaigen_US
dc.subjecthybrid composite platesen_US
dc.subjectthermal bucklingen_US
dc.subjectfinite element methoden_US
dc.titleThermal buckling of hybrid laminated composite plates with a holeen_US
dc.typeArticleen_US

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