Buckling of laminated composite and sandwich beams due to axially varying in-plane loads

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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.accessioned2024-06-12T10:58:18Z
dc.date.available2024-06-12T10:58:18Z
dc.date.issued2019
dc.departmentTrakya Üniversitesien_US
dc.description.abstractThis paper is dedicated to study the elastic buckling behavior of isotropic, laminated composite and sandwich beams subjected to various axially varying in-plane loads and boundary conditions (BCs). The formulation of the problem is derived by using the Ritz method with the displacement field based on a shear and normal deformable beam theory (SNDBT). Polynomial functions are employed to present the displacement field. The convergence studies are performed and then obtained results are compared with those of reported works. Results from extensive analysis are presented for different BCs, aspect ratios, orthotropy ratios, fiber angles and loading conditions. It is observed that the type of the axially variable in-plane load significantly affects the critical buckling loads and mode shapes of the beams depending on the BCs. The normal deformation effect depends on not only the aspect ratio but also BCs and the fiber orientation angles.en_US
dc.identifier.doi10.1016/j.compstruct.2018.11.067
dc.identifier.endpage408en_US
dc.identifier.issn0263-8223
dc.identifier.issn1879-1085
dc.identifier.scopus2-s2.0-85057290809en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.startpage391en_US
dc.identifier.urihttps://doi.org/10.1016/j.compstruct.2018.11.067
dc.identifier.urihttps://hdl.handle.net/20.500.14551/19989
dc.identifier.volume210en_US
dc.identifier.wosWOS:000455087700035en_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.subjectComposite Beamen_US
dc.subjectBucklingen_US
dc.subjectRitz Methoden_US
dc.subjectShear And Normal Deformable Beam Theoryen_US
dc.subjectIn Plane Variable Axial Loaden_US
dc.subjectFunctionally Graded Microbeamsen_US
dc.subjectFree-Vibrationen_US
dc.subjectBoundary-Conditionsen_US
dc.subjectRectangular-Platesen_US
dc.subjectPostbuckling Analysisen_US
dc.subject4-Unknown Shearen_US
dc.subjectRitz-Solutionen_US
dc.subjectStabilityen_US
dc.subjectColumnsen_US
dc.subjectBehavioren_US
dc.titleBuckling of laminated composite and sandwich beams due to axially varying in-plane loadsen_US
dc.typeArticleen_US

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