Flexural analysis of laminated composite and sandwich beams using a four-unknown shear and normal deformation theory

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dc.authoridKaramanlı, Armağan/0000-0003-3990-6515
dc.authoridThai, Huu-Tai/0000-0002-4461-9548
dc.authoridNguyen, Trung Kien/0000-0002-1215-9348
dc.authoridVo, Thuc/0000-0002-7137-4507
dc.authoridLanc, Domagoj/0000-0003-1488-6589
dc.contributor.authorVo, Thuc P.
dc.contributor.authorHuu-Tai Thai
dc.contributor.authorTrung-Kien Nguyen
dc.contributor.authorLanc, Domagoj
dc.contributor.authorKaramanli, Armagan
dc.date.accessioned2024-09-11T19:50:51Z
dc.date.available2024-09-11T19:50:51Z
dc.date.issued2017
dc.departmentİstanbul Gelişim Üniversitesien_US
dc.description.abstractThis paper presents flexural analysis of composite and sandwich beams using a quasi-3D theory, which considers simultaneously three effects such as normal and shear deformation as well as anisotropy coupling. The axial and transverse displacements are assumed to be cubic and parabolic variation through the beam depth. In order to solve problem, two-node C-1 beam elements with six degrees of freedom per node are developed. Numerical examples are carried out and the results are compared with those available in literature to validate the accuracy of the present theory. The effects of fibre angle, lay-up and span-to-height ratio on displacements and stresses are studied. Some new results, which can be useful for future references, are also given. (C) 2017 Elsevier Ltd. All rights reserved.en_US
dc.description.sponsorshipDepartment of Mechanical and Construction Engineering, Northumbria Universityen_US
dc.description.sponsorshipThe first author gratefully acknowledges the financial support from the Department of Mechanical and Construction Engineering, Northumbria University for conducting this research.en_US
dc.identifier.doi10.1016/j.compstruct.2017.05.041
dc.identifier.endpage397en_US
dc.identifier.issn0263-8223
dc.identifier.issn1879-1085
dc.identifier.scopus2-s2.0-85019970931en_US
dc.identifier.startpage388en_US
dc.identifier.urihttps://doi.org/10.1016/j.compstruct.2017.05.041
dc.identifier.urihttps://hdl.handle.net/11363/7687
dc.identifier.volume176en_US
dc.identifier.wosWOS:000405590500033en_US
dc.identifier.wosqualityQ1en_US
dc.indekslendigikaynakWeb of Scienceen_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.snmz20240903_Gen_US
dc.subjectComposite and sandwich beamsen_US
dc.subjectQuasi-3D theoryen_US
dc.subjectNormal and shear deformationen_US
dc.subjectFinite element methoden_US
dc.titleFlexural analysis of laminated composite and sandwich beams using a four-unknown shear and normal deformation theoryen_US
dc.typeArticleen_US

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