Buckling response of rectangular laminated composite plates with cutouts

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dc.contributor.authorBaba, Buket Okutan
dc.date.accessioned2025-01-27T21:21:35Z
dc.date.available2025-01-27T21:21:35Z
dc.date.issued2007
dc.departmentÇanakkale Onsekiz Mart Üniversitesi
dc.description.abstractResults from numerical and experimental study of the buckling response of compression-loaded E/glass-epoxy composite plates with centrally located circular and semicircular cutouts are presented. The effects of ply orientation angle and cutout shape on the buckling response of laminates subjected to uniaxial static loads are investigated. The laminated composites are analyzed using the finite element analysis software ANSYS. The change in critical buckling response of thin rectangular symmetric and antisymmetric laminates with respect to the ply orientation angle and cutout shape has been studied. In addition, results are presented from buckling analysis and these results are compared to experimentally measured results.
dc.identifier.endpage24
dc.identifier.issn0792-1233
dc.identifier.issn2191-0359
dc.identifier.issue1
dc.identifier.scopus2-s2.0-34249895595
dc.identifier.scopusqualityQ3
dc.identifier.startpage17
dc.identifier.urihttps://hdl.handle.net/20.500.12428/29002
dc.identifier.volume14
dc.identifier.wosWOS:000245619400002
dc.identifier.wosqualityQ4
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherWalter De Gruyter Gmbh
dc.relation.ispartofScience and Engineering of Composite Materials
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WoS_20250125
dc.subjectlayered structures
dc.subjectfinite element analysis
dc.subjectbuckling
dc.subjectcutout
dc.titleBuckling response of rectangular laminated composite plates with cutouts
dc.typeArticle

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