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Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/162

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contributor.authorSahu, S K-
contributor.authorAsha, A V-
contributor.authorMishra, R N-
date.accessioned2005-10-21T07:47:07Z-
date.available2005-10-21T07:47:07Z-
date.issued2005-
identifier.citationJournal of Reinforced Plastics and Composites, Vol 24, No 12, P 1327-1334en
identifier.urihttp://hdl.handle.net/2080/162-
descriptionCopyright for this article belongs to Sage Publications DOI: 10.1177/0731684405049856en
description.abstractThis article deals with the stability analysis of angle-ply laminated composite twisted panels using the finite element method. Here, a eight-noded isoparametric quadratic shell element is used to develop the finite element procedure. To investigate the vibration and stability behavior of twisted panels, the effect of various geometrical parameters like angle of twist, aspect ratio, lamination parameters, shallowness ratio, etc. are studied. The influence of various parameters on the vibration and stability characteristics of twisted panels have been examined. Numerical results are presented to show the effects of pretwist angles, geometry, and lamination details on the stability characteristics of twisted plates.en
format.extent125547 bytes-
format.mimetypeapplication/pdf-
language.isoen-
publisherSageen
subjectstabilityen
subjectvibrationen
subjectcomposite and twisted panelsen
titleStability of Laminated Composite Pretwisted Cantilever Panelsen
typeArticleen
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