Stability of Laminated Composite Pretwisted Cantilever Panels

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

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DC Field	Value	Language
dc.contributor.author	Sahu, S K	-
dc.contributor.author	Asha, A V	-
dc.contributor.author	Mishra, R N	-
dc.date.accessioned	2005-10-21T07:47:07Z	-
dc.date.available	2005-10-21T07:47:07Z	-
dc.date.issued	2005	-
dc.identifier.citation	Journal of Reinforced Plastics and Composites, Vol 24, No 12, P 1327-1334	en
dc.identifier.uri	http://hdl.handle.net/2080/162	-
dc.description	Copyright for this article belongs to Sage Publications DOI: 10.1177/0731684405049856	en
dc.description.abstract	This 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
dc.format.extent	125547 bytes	-
dc.format.mimetype	application/pdf	-
dc.language.iso	en	-
dc.publisher	Sage	en
dc.subject	stability	en
dc.subject	vibration	en
dc.subject	composite and twisted panels	en
dc.title	Stability of Laminated Composite Pretwisted Cantilever Panels	en
dc.type	Article	en
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