Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/58314
DC FieldValue
dc.titleFree vibration analysis of laminated composite cylindrical shells by DQM
dc.contributor.authorShu, C.
dc.contributor.authorDu, H.
dc.date.accessioned2014-06-17T05:13:12Z
dc.date.available2014-06-17T05:13:12Z
dc.date.issued1997
dc.identifier.citationShu, C.,Du, H. (1997). Free vibration analysis of laminated composite cylindrical shells by DQM. Composites Part B: Engineering 28 (3) : 267-273. ScholarBank@NUS Repository.
dc.identifier.issn13598368
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/58314
dc.description.abstractIn this paper, free vibrations of laminated composite cylindrical shells are investigated by the global method of generalized differential quadrature (GDQ). The GDQ method was developed to improve the differential quadrature (DQ) method for the computation of weighting coefficients. The differential equations of motion are formulated using Love's first approximation classical shell theory. The spatial derivatives in both the governing equations and the boundary conditions are discretized by the GDQ method. The GDQ method is examined by comparing its results with those available in the literature. It is demonstrated that, with the use of the GDQ method, the natural frequencies can be easily and accurately obtained by using a considerably small number of grid points. © 1997 Elsevier Science Limited.
dc.sourceScopus
dc.subjectA. layered structures
dc.subjectB. vibration
dc.subjectCylindrical shells
dc.subjectGeneralized differential quadrature
dc.subjectGlobal method
dc.typeArticle
dc.contributor.departmentMECHANICAL & PRODUCTION ENGINEERING
dc.description.sourcetitleComposites Part B: Engineering
dc.description.volume28
dc.description.issue3
dc.description.page267-273
dc.description.codenCPBEF
dc.identifier.isiutNOT_IN_WOS
Appears in Collections:Staff Publications

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