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    Geometrically Nonlinear Behavior of Composite Plates: A Review

    Source: Applied Mechanics Reviews:;1988:;volume( 041 ):;issue: 012::page 439
    Author:
    Chuen-Yuan Chia
    DOI: 10.1115/1.3151873
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Advances 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.
    keyword(s): Composite materials , Plates (structures) , Boundary-value problems , Shear (Mechanics) , Deflection , Dynamic response , Elastic plates , Laminates , Stress , Inertia (Mechanics) AND Force ,
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      Geometrically Nonlinear Behavior of Composite Plates: A Review

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/103370
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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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