Dynamic analysis of a laminated composite beam under harmonic load

dc.authorid0000-0001-5327-3406en_US
dc.contributor.authorAkbaş, Şeref Doğuşcan
dc.date.accessioned2021-03-20T20:09:14Z
dc.date.available2021-03-20T20:09:14Z
dc.date.issued2020
dc.departmentBTÜ, Mühendislik ve Doğa Bilimleri Fakültesi, İnşaat Mühendisliği Bölümüen_US
dc.description.abstractDynamic responses of a laminated composite cantilever beam under a harmonic are investigated in this study. The governing equations of problem are derived by using the Lagrange procedure. The Timoshenko beam theory is considered and the Ritz method is implemented in the solution of the problem. The algebraic polynomials are used with the trivial functions for the Ritz method. In the solution of dynamic problem, the Newmark average acceleration method is used in the time history. In the numerical examples, the effects of load parameter, the fiber orientation angles and stacking sequence of laminas on the dynamic responses of the laminated beam are investigated.en_US
dc.identifier.doi10.12989/csm.2020.9.6.563
dc.identifier.endpage573en_US
dc.identifier.issn2234-2184
dc.identifier.issn2234-2192
dc.identifier.issue6en_US
dc.identifier.scopus2-s2.0-85105032196
dc.identifier.scopusqualityQ3
dc.identifier.startpage563en_US
dc.identifier.urihttp://doi.org/10.12989/csm.2020.9.6.563
dc.identifier.urihttps://hdl.handle.net/20.500.12885/322
dc.identifier.volume9en_US
dc.identifier.wosWOS:000614672800004
dc.identifier.wosqualityN/A
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.institutionauthorAkbaş, Şeref Doğuşcan
dc.language.isoenen_US
dc.publisherTechno-Pressen_US
dc.relation.ispartofCoupled Systems Mechanicsen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectdynamic analysisen_US
dc.subjectlaminated composite beamsen_US
dc.subjectRitz methoden_US
dc.titleDynamic analysis of a laminated composite beam under harmonic load
dc.typeArticle

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