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contributor authorChuen-Yuan Chia
date accessioned2017-05-08T23:26:17Z
date available2017-05-08T23:26:17Z
date copyrightDecember, 1988
date issued1988
identifier issn0003-6900
identifier otherAMREAD-25569#439_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103370
description abstractAdvances in the understanding of static large deflection, postbuckling, and nonlinear dynamic response by using the analytical method are summarized for laminated elastic plates. In the case of symmetric laminates, bending-stretching coupling vanishes. The classical nonlinear theory of orthotropic or anisotropic plates applies, and references are also presented for these plates. A nonlinear shear-deformable theory of generally laminated plates and a general method of solution are briefly reviewed for a wide class of boundary conditions. Several effects, which complicate the geometric nonlinear behavior of composite plates, discussed in this survey paper are: transverse shear and normal stresses, rotatory and in-plane inertia, initial in-plane edge forces, geometric imperfections, cutouts, and nonclassical boundary conditions.
publisherThe American Society of Mechanical Engineers (ASME)
titleGeometrically Nonlinear Behavior of Composite Plates: A Review
typeJournal Paper
journal volume41
journal issue12
journal titleApplied Mechanics Reviews
identifier doi10.1115/1.3151873
journal fristpage439
journal lastpage451
identifier eissn0003-6900
keywordsComposite materials
keywordsPlates (structures)
keywordsBoundary-value problems
keywordsShear (Mechanics)
keywordsDeflection
keywordsDynamic response
keywordsElastic plates
keywordsLaminates
keywordsStress
keywordsInertia (Mechanics) AND Force
treeApplied Mechanics Reviews:;1988:;volume( 041 ):;issue: 012
contenttypeFulltext


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