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dc.contributor.authorChuen-Yuan Chia
dc.date.accessioned2017-05-08T23:26:17Z
dc.date.available2017-05-08T23:26:17Z
dc.date.copyrightDecember, 1988
dc.date.issued1988
dc.identifier.issn0003-6900
dc.identifier.otherAMREAD-25569#439_1.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl/handle/yetl/103370
dc.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.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleGeometrically Nonlinear Behavior of Composite Plates: A Review
dc.typeJournal Paper
dc.journal.volume41
dc.journal.issue12
dc.journal.titleApplied Mechanics Reviews
dc.identifier.doi10.1115/1.3151873
dc.journal.fristpage439
dc.journal.lastpage451
dc.identifier.eissn0003-6900
dc.keywordsComposite materials
dc.keywordsPlates (structures)
dc.keywordsBoundary-value problems
dc.keywordsShear (Mechanics)
dc.keywordsDeflection
dc.keywordsDynamic response
dc.keywordsElastic plates
dc.keywordsLaminates
dc.keywordsStress
dc.keywordsInertia (Mechanics) AND Force
dc.treeApplied Mechanics Reviews:;1988:;volume( 041 ):;issue: 012
dc.contenttypeFulltext


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