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Article: Finite element analysis of multilayer sandwich plates and shells

TitleFinite element analysis of multilayer sandwich plates and shells
Authors
Khatua, TPCheung, YK
Issue Date1974
AbstractThe paper conducts an investigation in which the assumption of common shear angle in all the core layers is done away with. Arbitrary in-plane displacements are prescribed in all stiff layers resulting in a more rigorous analysis. A study is made of the bending and free vibration behavior of axisymmetric multilayer sandwich plates, cones and cylinders using the finite element method. A conical element is developed to solve these structures. Several standard problems are solved in order to test the extent of accuracy of the element. Refs.
Persistent Identifierhttp://hdl.handle.net/10722/149811

 

DC FieldValueLanguage
dc.contributor.authorKhatua, TPen_US
dc.contributor.authorCheung, YKen_US
dc.date.accessioned2012-06-26T05:59:55Z-
dc.date.available2012-06-26T05:59:55Z-
dc.date.issued1974en_US
dc.identifier.urihttp://hdl.handle.net/10722/149811-
dc.description.abstractThe paper conducts an investigation in which the assumption of common shear angle in all the core layers is done away with. Arbitrary in-plane displacements are prescribed in all stiff layers resulting in a more rigorous analysis. A study is made of the bending and free vibration behavior of axisymmetric multilayer sandwich plates, cones and cylinders using the finite element method. A conical element is developed to solve these structures. Several standard problems are solved in order to test the extent of accuracy of the element. Refs.en_US
dc.languageengen_US
dc.titleFinite element analysis of multilayer sandwich plates and shellsen_US
dc.typeArticleen_US
dc.identifier.emailCheung, YK: hreccyk@hkucc.hku.hken_US
dc.identifier.authorityCheung, YK=rp00104en_US
dc.description.naturelink_to_subscribed_fulltexten_US
dc.identifier.scopuseid_2-s2.0-0016180827en_US
dc.identifier.scopusauthoridKhatua, TP=6603550166en_US
dc.identifier.scopusauthoridCheung, YK=7202111065en_US

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