dc.creatorMantari, J.L.
dc.creatorOre, M.
dc.date.accessioned2017-11-28T12:37:09Z
dc.date.available2017-11-28T12:37:09Z
dc.date.created2017-11-28T12:37:09Z
dc.date.issued2015-11
dc.identifier0263-8223
dc.identifierhttps://hdl.handle.net/20.500.12815/48
dc.identifierhttps://doi.org/10.1016/j.compstruct.2015.06.035
dc.identifierComposite Structures
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.
dc.languageeng
dc.publisherElsevier
dc.rightshttp://creativecommons.org/licenses/by-nc-nd/4.0/
dc.rightsinfo:eu-repo/semantics/openAccess
dc.sourceRepositorio Institucional UTEC
dc.sourceUniversidad de Ingeniería y Tecnología - UTEC
dc.subjectLaminated composite plates
dc.subjectFSDT
dc.subjectFundamental frequencies
dc.subjectAnalytical solution
dc.titleFree vibration of single and sandwich laminated composite plates by using a simplified FSDT
dc.typeinfo:eu-repo/semantics/article


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