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dc.contributor.authorPanda, S K-
dc.contributor.authorMahapatra, T R-
dc.identifier.citationACUN6 –Composites and Nanocomposites in Civil, Offshore and Mining Infrastructure 2012, Monash University, Clayton Campus, Melbourne, Australiaen
dc.descriptionCopyright for this article belongs to proceeding publisheren
dc.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
dc.format.extent129584 bytes-
dc.titleGeometric Nonlinear Vibration Analysis of Heated Laminateden
Appears in Collections:Conference Papers

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