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contributor authorK. K. Shukla
contributor authorY. Nath
date accessioned2017-05-08T22:39:39Z
date available2017-05-08T22:39:39Z
date copyrightJanuary 2002
date issued2002
identifier other%28asce%290733-9399%282002%29128%3A1%2893%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/85463
description abstractPostbuckling analysis is presented for shear deformable cross-ply laminated composite rectangular plates subjected to the combination of in-plane edge compressive mechanical loading and thermal loads due to a linearly varying temperature across the thickness. The formulation is based on the first-order shear deformation theory and von-Karman-type nonlinearity. The analysis uses a quadratic extrapolation technique for linearization and Chebyshev polynomials for spatial discretization. An incremental iterative approach is employed to estimate the critical load. The boundary conditions consisting of clamped, simply supported, free edge, and their combinations are considered. The effects of the thinness ratio, aspect ratio, lamination scheme, the number of layers, and the modulus ratio on the critical load/limit load and postbuckling behavior are studied.
publisherAmerican Society of Civil Engineers
titleThermomechanical Postbuckling of Cross-Ply Laminated Rectangular Plates
typeJournal Paper
journal volume128
journal issue1
journal titleJournal of Engineering Mechanics
identifier doi10.1061/(ASCE)0733-9399(2002)128:1(93)
treeJournal of Engineering Mechanics:;2002:;Volume ( 128 ):;issue: 001
contenttypeFulltext


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