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Article: Approximate three-dimensional analysis of rectangular thick laminated plates: Bending, vibration and buckling

TitleApproximate three-dimensional analysis of rectangular thick laminated plates: Bending, vibration and buckling
Authors
Issue Date1993
PublisherPergamon. The Journal's web site is located at http://www.elsevier.com/locate/compstruc
Citation
Computers And Structures, 1993, v. 47 n. 2, p. 193-199 How to Cite?
AbstractA global-local approach is proposed to analyse thick laminated plates. This approach treats a thick laminated plate as a three-dimensional inhomogeneous anisotropic elastic body. The cross-section of a laminated plate is first discretized into conventional eight-node elements. The interpolation function along the span of the plate is defined by the cubic B3-spline function. The displacement functions can be expressed as the product of the usual isoparametric shape functions and the spline function. A set of global polynomials of an appropriate order is selected to transform the nodal variables of the cross-section to a much smaller set of generalized parameters associated with the polynomials. These parameters can be obtained by means of the standard Rayleigh-Ritz technique. The total number of unknowns involved is drastically reduced with a minor sacrifice of accuracy. The six components of stresses, the fundamental natural frequencies and the critical buckling loads can be determined with acceptable accuracy. Numerical examples are given to demonstrate the accuracy and effectiveness of the global-local procedures. © 1993.
Persistent Identifierhttp://hdl.handle.net/10722/150006
ISSN
2023 Impact Factor: 4.4
2023 SCImago Journal Rankings: 1.274
ISI Accession Number ID

 

DC FieldValueLanguage
dc.contributor.authorCheung, YKen_US
dc.contributor.authorKong, Jen_US
dc.date.accessioned2012-06-26T06:01:02Z-
dc.date.available2012-06-26T06:01:02Z-
dc.date.issued1993en_US
dc.identifier.citationComputers And Structures, 1993, v. 47 n. 2, p. 193-199en_US
dc.identifier.issn0045-7949en_US
dc.identifier.urihttp://hdl.handle.net/10722/150006-
dc.description.abstractA global-local approach is proposed to analyse thick laminated plates. This approach treats a thick laminated plate as a three-dimensional inhomogeneous anisotropic elastic body. The cross-section of a laminated plate is first discretized into conventional eight-node elements. The interpolation function along the span of the plate is defined by the cubic B3-spline function. The displacement functions can be expressed as the product of the usual isoparametric shape functions and the spline function. A set of global polynomials of an appropriate order is selected to transform the nodal variables of the cross-section to a much smaller set of generalized parameters associated with the polynomials. These parameters can be obtained by means of the standard Rayleigh-Ritz technique. The total number of unknowns involved is drastically reduced with a minor sacrifice of accuracy. The six components of stresses, the fundamental natural frequencies and the critical buckling loads can be determined with acceptable accuracy. Numerical examples are given to demonstrate the accuracy and effectiveness of the global-local procedures. © 1993.en_US
dc.languageengen_US
dc.publisherPergamon. The Journal's web site is located at http://www.elsevier.com/locate/compstrucen_US
dc.relation.ispartofComputers and Structuresen_US
dc.titleApproximate three-dimensional analysis of rectangular thick laminated plates: Bending, vibration and bucklingen_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-s2.0-0027575694en_US
dc.identifier.volume47en_US
dc.identifier.issue2en_US
dc.identifier.spage193en_US
dc.identifier.epage199en_US
dc.identifier.isiWOS:A1993LF23900003-
dc.publisher.placeUnited Kingdomen_US
dc.identifier.scopusauthoridCheung, YK=7202111065en_US
dc.identifier.scopusauthoridKong, J=7202290905en_US
dc.identifier.issnl0045-7949-

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