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

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contributor.authorPanda, S K-
contributor.authorMahapatra, T R-
date.accessioned2012-12-05T15:43:51Z-
date.available2012-12-05T15:43:51Z-
date.issued2012-11-
identifier.citationACUN6 –Composites and Nanocomposites in Civil, Offshore and Mining Infrastructure 2012, Monash University, Clayton Campus, Melbourne, Australiaen
identifier.urihttp://hdl.handle.net/2080/1787-
descriptionCopyright for this article belongs to proceeding publisheren
description.abstractGeometrically 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
format.extent129584 bytes-
format.mimetypeapplication/pdf-
language.isoen-
titleGeometric Nonlinear Vibration Analysis of Heated Laminateden
typeArticleen
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