Buckling of cross-ply composite plates with linearly varying In-plane loads

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dc.authoridAksencer, Tolga/0000-0001-9926-9605
dc.authorwosidAydogdu, Metin/A-2596-2009
dc.contributor.authorAydogdu, Metin
dc.contributor.authorAksencer, Tolga
dc.date.accessioned2024-06-12T10:55:25Z
dc.date.available2024-06-12T10:55:25Z
dc.date.issued2018
dc.departmentTrakya Üniversitesien_US
dc.description.abstractBuckling of composite plates with linearly varying in-plane loads has been studied. Loaded edges are assumed as simply supported and the remaining ones are arbitrary. First order and third order shear deformation plate theories are used in the formulation of the problem. Ritz method has been utilized with simple polynomials in displacement field. By modifying displacement field components, the continuity of transverse stresses is satisfied among the layers of cross-ply symmetric lay-up composite plates. Results are obtained for different material, geometrical properties and loading conditions. (C) 2017 Elsevier Ltd. All rights reserved.en_US
dc.identifier.doi10.1016/j.compstruct.2017.02.085
dc.identifier.endpage231en_US
dc.identifier.issn0263-8223
dc.identifier.issn1879-1085
dc.identifier.scopus2-s2.0-85014187542en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.startpage221en_US
dc.identifier.urihttps://doi.org/10.1016/j.compstruct.2017.02.085
dc.identifier.urihttps://hdl.handle.net/20.500.14551/19392
dc.identifier.volume183en_US
dc.identifier.wosWOS:000414592800023en_US
dc.identifier.wosqualityQ1en_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/closedAccessen_US
dc.subjectBucklingen_US
dc.subjectCompositeen_US
dc.subjectLinearly Varying Loaden_US
dc.subjectRitz Methoden_US
dc.subjectLaminated Compositeen_US
dc.subjectRectangular-Platesen_US
dc.subjectBoundary-Conditionsen_US
dc.subjectFree-Vibrationen_US
dc.subjectRemain Flaten_US
dc.titleBuckling of cross-ply composite plates with linearly varying In-plane loadsen_US
dc.typeArticleen_US

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