Thermal buckling behavior of cross-ply hybrid composite laminates with inclined crack

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dc.contributor.authorAvci, Ahmet
dc.contributor.authorSahin, Omer Sinan
dc.contributor.authorAtaberk, Necati
dc.date.accessioned2020-03-26T17:04:40Z
dc.date.available2020-03-26T17:04:40Z
dc.date.issued2006
dc.departmentSelçuk Üniversitesien_US
dc.description.abstractThermal buckling analysis of symmetric and antisymmetric cross-ply laminated hybrid composite plates with an inclined crack subjected to a uniform temperature rise 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 obtaining the thermal buckling temperatures of hybrid composite laminates. The effects of crack size and lay-up sequences on the thermal buckling temperatures for symmetric and antisymmetric plates are investigated. The results are shown in graphical form for various boundary conditions. (c) 2006 Elsevier Ltd. All rights reserved.en_US
dc.identifier.doi10.1016/j.compscitech.2006.02.009en_US
dc.identifier.endpage2970en_US
dc.identifier.issn0266-3538en_US
dc.identifier.issue15en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.startpage2965en_US
dc.identifier.urihttps://dx.doi.org/10.1016/j.compscitech.2006.02.009
dc.identifier.urihttps://hdl.handle.net/20.500.12395/20750
dc.identifier.volume66en_US
dc.identifier.wosWOS:000241654500036en_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/closedAccessen_US
dc.selcuk20240510_oaigen_US
dc.subjecthybrid composite platesen_US
dc.subjectthermal bucklingen_US
dc.subjectfinite element methoden_US
dc.titleThermal buckling behavior of cross-ply hybrid composite laminates with inclined cracken_US
dc.typeArticleen_US

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