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dc.contributor.authorMantari, J.L.-
dc.contributor.authorOre, M.-
dc.date.accessioned2017-11-28T12:37:09Z-
dc.date.available2017-11-28T12:37:09Z-
dc.date.issued2015-11-
dc.identifier.urihttp://repositorio.utec.edu.pe/handle/UTEC/48-
dc.description.abstractThis paper presents a simplified first order shear deformation theory (FSDT) for laminated composite and sandwich plates. Unlike the existing FSDT, the present one has a novel displacement field which include undetermined integral terms and contains only four unknowns. Equations of motion and boundary conditions are derived from the Hamilton’s principle. Navier-type analytical solution is obtained in closed form and by solving the eigenvalue equation. The comparison of the present results with the available elasticity solutions and the results computed independently using the FSDTs available in the literature shows that this theory predicts the fundamental frequencies with good accurately. It can be concluded that the proposed theory is accurate and simple in solving the dynamic behavior of single and sandwich laminated composite plates.es_PE
dc.formatapplication/pdfes_PE
dc.language.isoenges_PE
dc.publisherElsevier B.V.es_PE
dc.rightsinfo:eu-repo/semantics/openAccesses_PE
dc.sourceUniversidad de Ingeniería y Tecnología - UTECes_PE
dc.source.uriRepositorio Institucional UTECes_PE
dc.subjectLaminated composite plateses_PE
dc.subjectFSDTes_PE
dc.subjectFundamental frequencieses_PE
dc.subjectAnalytical solutiones_PE
dc.titleFree vibration of single and sandwich laminated composite plates by using a simplified FSDTes_PE
dc.typeinfo:eu-repo/semantics/articlees_PE
dc.subject.ocdeIngeniería Mecánicaes_PE
dc.identifier.doi10.1016/j.compstruct.2015.06.035-
dc.identifier.journalComposite Structureses_PE
Aparece en las colecciones: Ingeniería Mecánica

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