Free vibration and buckling analysis of laminated composites and sandwich microbeams using a transverse shear-normal deformable beam theory

dc.authoridKaramanlı, Armağan/0000-0003-3990-6515
dc.authoridAYDOGDU, METIN/0000-0003-4567-2532
dc.authorwosidKaramanlı, Armağan/AGG-2487-2022
dc.authorwosidAydogdu, Metin/A-2596-2009
dc.contributor.authorKaramanli, Armagan
dc.contributor.authorAydogdu, Metin
dc.date.accessioned2024-06-12T11:09:21Z
dc.date.available2024-06-12T11:09:21Z
dc.date.issued2020
dc.departmentTrakya Üniversitesien_US
dc.description.abstractIn this paper, the free vibration and buckling responses of laminated composite and sandwich microbeams with arbitrary boundary conditions are investigated. The governing equations based on the modified couple stress theory are derived by using the total potential energy of a microbeam and employing a transverse shear-normal deformable beam theory. Extensive analysis results in terms of dimensionless fundamental frequencies and dimensionless critical buckling loads are introduced for various boundary conditions, aspect ratios, orthotropy ratios, fiber orientation angles, thickness to material length scale parameter ratios, and core thickness to face layer thickness ratios.en_US
dc.identifier.doi10.1177/1077546319878538
dc.identifier.endpage228en_US
dc.identifier.issn1077-5463
dc.identifier.issn1741-2986
dc.identifier.issue3-4en_US
dc.identifier.scopus2-s2.0-85075007102en_US
dc.identifier.scopusqualityQ2en_US
dc.identifier.startpage214en_US
dc.identifier.urihttps://doi.org/10.1177/1077546319878538
dc.identifier.urihttps://hdl.handle.net/20.500.14551/22783
dc.identifier.volume26en_US
dc.identifier.wosWOS:000498343200001en_US
dc.identifier.wosqualityQ2en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherSage Publications Ltden_US
dc.relation.ispartofJournal Of Vibration And Controlen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectNormal Deformationen_US
dc.subjectModified Couple Stress Theoryen_US
dc.subjectLaminated Compositeen_US
dc.subjectFree Vibrationen_US
dc.subjectBucklingen_US
dc.subjectCouple Stress Theoryen_US
dc.titleFree vibration and buckling analysis of laminated composites and sandwich microbeams using a transverse shear-normal deformable beam theoryen_US
dc.typeArticleen_US

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