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    Finite Element Analysis of Shear Deformable Laminated Composite Plates

    Source: Journal of Energy Resources Technology:;1993:;volume( 115 ):;issue: 001::page 41
    Author:
    T. Y. Kam
    ,
    R. R. Chang
    DOI: 10.1115/1.2905968
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A shear deformable finite element is developed for the analysis of thick laminated composite plates. The finite element formulation is based on Mindlin’s plate theory in which shear correction factors are derived from the exact expressions for orthotropic materials. The element is used to solve a variety of problems on deflection, stress distribution, natural frequency and buckling of laminated composite plates. The effects of material properties, plate aspect ratio, length-to-thickness ratio, number of layers and lamination angle on the mechanical behaviors of laminated composite plates are investigated. Optimal lamination arrangements of layers for laminated composite plates of particular applications are determined.
    keyword(s): Composite materials , Shear (Mechanics) , Finite element analysis , Plates (structures) , Laminations , Thickness , Buckling , Deflection , Mechanical behavior , Stress concentration AND Materials properties ,
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      Finite Element Analysis of Shear Deformable Laminated Composite Plates

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/111854
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    contributor authorT. Y. Kam
    contributor authorR. R. Chang
    date accessioned2017-05-08T23:41:13Z
    date available2017-05-08T23:41:13Z
    date copyrightMarch, 1993
    date issued1993
    identifier issn0195-0738
    identifier otherJERTD2-26448#41_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111854
    description abstractA shear deformable finite element is developed for the analysis of thick laminated composite plates. The finite element formulation is based on Mindlin’s plate theory in which shear correction factors are derived from the exact expressions for orthotropic materials. The element is used to solve a variety of problems on deflection, stress distribution, natural frequency and buckling of laminated composite plates. The effects of material properties, plate aspect ratio, length-to-thickness ratio, number of layers and lamination angle on the mechanical behaviors of laminated composite plates are investigated. Optimal lamination arrangements of layers for laminated composite plates of particular applications are determined.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFinite Element Analysis of Shear Deformable Laminated Composite Plates
    typeJournal Paper
    journal volume115
    journal issue1
    journal titleJournal of Energy Resources Technology
    identifier doi10.1115/1.2905968
    journal fristpage41
    journal lastpage46
    identifier eissn1528-8994
    keywordsComposite materials
    keywordsShear (Mechanics)
    keywordsFinite element analysis
    keywordsPlates (structures)
    keywordsLaminations
    keywordsThickness
    keywordsBuckling
    keywordsDeflection
    keywordsMechanical behavior
    keywordsStress concentration AND Materials properties
    treeJournal of Energy Resources Technology:;1993:;volume( 115 ):;issue: 001
    contenttypeFulltext
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