Geometric Nonlinear Vibration Analysis of Heated Laminated

Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/1787

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DC Field	Value	Language
dc.contributor.author	Panda, S K	-
dc.contributor.author	Mahapatra, T R	-
dc.date.accessioned	2012-12-05T15:43:51Z	-
dc.date.available	2012-12-05T15:43:51Z	-
dc.date.issued	2012-11	-
dc.identifier.citation	ACUN6 –Composites and Nanocomposites in Civil, Offshore and Mining Infrastructure 2012, Monash University, Clayton Campus, Melbourne, Australia	en
dc.identifier.uri	http://hdl.handle.net/2080/1787	-
dc.description	Copyright for this article belongs to proceeding publisher	en
dc.description.abstract	Geometrically nonlinear free vibration behaviour of laminated composite cylindrical panel in thermal environment is analysed. The mid-plane kinematics is based on the higher order shear deformation theory and the geometric nonlinearity is introduced in the strain displacement relation using Green-Lagrange type nonlinearity. The sets of governing equations are obtained using Hamilton’s principle and discretised using a nonlinear finite element approach. The results obtained using the proposed model is compared with those available in open literature.	en
dc.format.extent	129584 bytes	-
dc.format.mimetype	application/pdf	-
dc.language.iso	en	-
dc.title	Geometric Nonlinear Vibration Analysis of Heated Laminated	en
dc.type	Article	en
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