Free vibration of axially loaded composite beams using a four-unknown shear and normal deformation theory

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dc.authoridThai, Huu-Tai/0000-0002-4461-9548
dc.authoridVo, Thuc/0000-0002-7137-4507
dc.authorwosidThai, Huu-Tai/C-1796-2012
dc.authorwosidAydogdu, Metin/A-2596-2009
dc.authorwosidVo, Thuc P/B-9385-2011
dc.contributor.authorVo, Thuc P.
dc.contributor.authorHuu-Tai Thai
dc.contributor.authorAydogdu, Metin
dc.date.accessioned2024-06-12T10:58:18Z
dc.date.available2024-06-12T10:58:18Z
dc.date.issued2017
dc.departmentTrakya Üniversitesien_US
dc.description.abstractThis paper presents free vibration of composite beams under axial load using a four-unknown shear and normal deformation theory. The constitutive equation is reduced from the 3D stress-strain relations of orthotropic lamina. The governing differential equations of motion are derived using the Hamilton's principle. A two-node C-1 beam element is developed by using a mixed interpolation with linear and Hermite-cubic polynomials for unknown variables. Numerical results are computed and compared with those available in the literature and commercial finite element software (ANSYS and ABAQUS). The comparison study illustrates the effects of normal strain, Jay-ups and Poisson's ratio on the natural frequencies and load-frequency curves of composite beams. (C) 2017 Elsevier Ltd. All rights reserved.en_US
dc.description.sponsorshipNorthumbria Universityen_US
dc.description.sponsorshipThe first author gratefully acknowledges research support fund from Northumbria University. The first author also would like to thank Professor Ranjan Banerjee at City, University of London for discussions the results.en_US
dc.identifier.doi10.1016/j.compstruct.2017.07.022
dc.identifier.endpage414en_US
dc.identifier.issn0263-8223
dc.identifier.issn1879-1085
dc.identifier.scopus2-s2.0-85025474885en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.startpage406en_US
dc.identifier.urihttps://doi.org/10.1016/j.compstruct.2017.07.022
dc.identifier.urihttps://hdl.handle.net/20.500.14551/19991
dc.identifier.volume178en_US
dc.identifier.wosWOS:000409150100036en_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/openAccessen_US
dc.subjectComposite Beamsen_US
dc.subjectNormal Strainen_US
dc.subjectPoisson Effecten_US
dc.subjectShear And Normal Deformation Theoryen_US
dc.subjectPly Laminated Beamsen_US
dc.subjectArbitrary Boundary-Conditionsen_US
dc.subjectSinus Finite-Elementsen_US
dc.subjectSandwich Beamsen_US
dc.subjectBuckling Analysisen_US
dc.subjectStress Continuityen_US
dc.subjectRitz Methoden_US
dc.subjectModelen_US
dc.subjectFormulationen_US
dc.subjectBehavioren_US
dc.titleFree vibration of axially loaded composite beams using a four-unknown shear and normal deformation theoryen_US
dc.typeArticleen_US

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