Eigenfrequencies of rectangular plate assemblies

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dc.contributor.authorBercin A.N.
dc.date.accessioned2020-06-25T15:13:10Z
dc.date.available2020-06-25T15:13:10Z
dc.date.issued1997
dc.departmentKırıkkale Üniversitesi
dc.description.abstractThe dynamic stiffness method, which yields exact results for certain class of plate structures, is used to analyse free vibration frequencies of various plate assemblies. The constituent plates of the systems are considered either to lie in planes at right angles to each other or coupled via stiffeners. The method is found to work extremely well and excellent agreement is obtained when a comparison is made between computed results and earlier published data. In-plane degrees of freedom are also taken into account in the calculations and it is seen that while for the directly coupled plate assemblies the in-plane effects are negligible for low-order modes, for the stiffened plate assembly the effect of in-plane motion is to reduce the free vibration frequencies. © 1997 Elsevier Science Ltd.en_US
dc.identifier.doi10.1016/S0045-7949(96)00348-3
dc.identifier.endpage711en_US
dc.identifier.issn00457949
dc.identifier.issue5en_US
dc.identifier.scopus2-s2.0-0031354276
dc.identifier.scopusqualityQ1
dc.identifier.startpage703en_US
dc.identifier.urihttps://doi.org/10.1016/S0045-7949(96)00348-3
dc.identifier.urihttps://hdl.handle.net/20.500.12587/1616
dc.identifier.volume65en_US
dc.identifier.wosWOS:000071280800008
dc.identifier.wosqualityQ2
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherElsevier Ltden_US
dc.relation.ispartofComputers and Structures
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.titleEigenfrequencies of rectangular plate assembliesen_US
dc.typeArticle

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