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Postbuckling behaviour of optimized rectangular composite laminates

โœ Scribed by M.D. Pandey; A.N. Sherbourne

Publisher
Elsevier Science
Year
1993
Tongue
English
Weight
916 KB
Volume
23
Category
Article
ISSN
0263-8223

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A non-linear finite element analysis including a new flat shell element has been developed to examine the response of laminated panels going through large deflections and rotations under uniform temperature change. The equilibrium path describing the relationship between temperature and deflection i