Thermal buckling of hybrid angle-ply laminated composite plates with a hole

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dc.contributor.authorSahin, OS
dc.date.accessioned2020-03-26T16:58:20Z
dc.date.available2020-03-26T16:58:20Z
dc.date.issued2005
dc.departmentSelçuk Üniversitesien_US
dc.description.abstractIn this paper, thermal buckling analysis of symmetric and antisymmetric laminated hybrid composite plates with a hole subjected to a uniform temperature rise for different boundary conditions is presented. The first-order shear deformation theory in conjunction with variational energy method is employed in mathematical formulation. The eight-node Lagrangian finite element technique is used for obtaining the thermal buckling temperatures of glass-epoxy/boron-epoxy hybrid laminates. The effects of hole size, layup sequences and boundary conditions on thermal buckling temperatures are investigated. The results are shown in graphical form for various boundary conditions. (c) 2005 Elsevier Ltd. All rights reserved.en_US
dc.identifier.doi10.1016/j.compscitech.2005.03.007en_US
dc.identifier.endpage1790en_US
dc.identifier.issn0266-3538en_US
dc.identifier.issue11.12.2020en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.startpage1780en_US
dc.identifier.urihttps://dx.doi.org/10.1016/j.compscitech.2005.03.007
dc.identifier.urihttps://hdl.handle.net/20.500.12395/19941
dc.identifier.volume65en_US
dc.identifier.wosWOS:000231046700018en_US
dc.identifier.wosqualityQ1en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherELSEVIER SCI LTDen_US
dc.relation.ispartofCOMPOSITES SCIENCE AND TECHNOLOGYen_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 angle-ply laminated composite plates with a holeen_US
dc.typeArticleen_US

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