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    Three-Dimensional Solutions for Antisymmetrically Laminated Anisotropic Plates

    Source: Journal of Applied Mechanics:;1990:;volume( 057 ):;issue: 001::page 182
    Author:
    Ahmed K. Noor
    ,
    W. Scott Burton
    DOI: 10.1115/1.2888300
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Analytic three-dimensional elasticity solutions are presented for the stress and free vibration problems of multilayered anisotropic plates. The plates are assumed to have rectangular geometry and antisymmetric lamination with respect to the middle plane. A mixed formulation is used with the fundamental unknowns consisting of the six stress components and the three displacement components of the plate. Each of the plate variables is decomposed into symmetric and antisymmetric components in the thickness direction, and is expressed in terms of a double Fourier series in the Cartesian surface coordinates. Extensive numerical results are presented showing the effects of variation in the lamination and geometric parameters of composite plates on the importance of the transverse stress and strain components.
    keyword(s): Plates (structures) , Stress , Laminations , Thickness , Elasticity , Composite materials , Displacement , Fourier series , Free vibrations AND Geometry ,
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      Three-Dimensional Solutions for Antisymmetrically Laminated Anisotropic Plates

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/106526
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    contributor authorAhmed K. Noor
    contributor authorW. Scott Burton
    date accessioned2017-05-08T23:31:58Z
    date available2017-05-08T23:31:58Z
    date copyrightMarch, 1990
    date issued1990
    identifier issn0021-8936
    identifier otherJAMCAV-26318#182_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106526
    description abstractAnalytic three-dimensional elasticity solutions are presented for the stress and free vibration problems of multilayered anisotropic plates. The plates are assumed to have rectangular geometry and antisymmetric lamination with respect to the middle plane. A mixed formulation is used with the fundamental unknowns consisting of the six stress components and the three displacement components of the plate. Each of the plate variables is decomposed into symmetric and antisymmetric components in the thickness direction, and is expressed in terms of a double Fourier series in the Cartesian surface coordinates. Extensive numerical results are presented showing the effects of variation in the lamination and geometric parameters of composite plates on the importance of the transverse stress and strain components.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThree-Dimensional Solutions for Antisymmetrically Laminated Anisotropic Plates
    typeJournal Paper
    journal volume57
    journal issue1
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2888300
    journal fristpage182
    journal lastpage188
    identifier eissn1528-9036
    keywordsPlates (structures)
    keywordsStress
    keywordsLaminations
    keywordsThickness
    keywordsElasticity
    keywordsComposite materials
    keywordsDisplacement
    keywordsFourier series
    keywordsFree vibrations AND Geometry
    treeJournal of Applied Mechanics:;1990:;volume( 057 ):;issue: 001
    contenttypeFulltext
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