Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/1787
Full metadata record
DC FieldValueLanguage
dc.contributor.authorPanda, S K-
dc.contributor.authorMahapatra, T R-
dc.date.accessioned2012-12-05T15:43:51Z-
dc.date.available2012-12-05T15:43:51Z-
dc.date.issued2012-11-
dc.identifier.citationACUN6 –Composites and Nanocomposites in Civil, Offshore and Mining Infrastructure 2012, Monash University, Clayton Campus, Melbourne, Australiaen
dc.identifier.urihttp://hdl.handle.net/2080/1787-
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.format.mimetypeapplication/pdf-
dc.language.isoen-
dc.titleGeometric Nonlinear Vibration Analysis of Heated Laminateden
dc.typeArticleen
Appears in Collections:Conference Papers

Files in This Item:
File Description SizeFormat 
001_Geometric_Panda.pdf126.55 kBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.