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    Design of Composite Cylindrical Panels for Maximum Axial and Shear Buckling Capacity

    Source: Journal of Energy Resources Technology:;1991:;volume( 113 ):;issue: 003::page 204
    Author:
    N. Kumar
    ,
    T. R. Tauchert
    DOI: 10.1115/1.2905806
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Response of a cylindrical panel made of layers of composite material and subjected to in-plane loads is investigated. Prebuckling deformations are determined for antisymmetric angle-ply and cross-ply panels having simply supported boundary conditions. Buckling solutions are obtained via the Rayleigh-Ritz method. Nonlinear programming is used to optimize the designs. Design variables are taken as fiber orientations and/or thicknesses of different layers. Numerical results are presented for different materials and different geometrical parameters, including aspect ratio and curvature-to-length ratio.
    keyword(s): Composite materials , Shear (Mechanics) , Design , Buckling , Nonlinear programming , Rayleigh-Ritz methods , Deformation , Boundary-value problems , Fibers AND Stress ,
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      Design of Composite Cylindrical Panels for Maximum Axial and Shear Buckling Capacity

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/108452
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    • Journal of Energy Resources Technology

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    contributor authorN. Kumar
    contributor authorT. R. Tauchert
    date accessioned2017-05-08T23:35:22Z
    date available2017-05-08T23:35:22Z
    date copyrightSeptember, 1991
    date issued1991
    identifier issn0195-0738
    identifier otherJERTD2-26439#204_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108452
    description abstractResponse of a cylindrical panel made of layers of composite material and subjected to in-plane loads is investigated. Prebuckling deformations are determined for antisymmetric angle-ply and cross-ply panels having simply supported boundary conditions. Buckling solutions are obtained via the Rayleigh-Ritz method. Nonlinear programming is used to optimize the designs. Design variables are taken as fiber orientations and/or thicknesses of different layers. Numerical results are presented for different materials and different geometrical parameters, including aspect ratio and curvature-to-length ratio.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDesign of Composite Cylindrical Panels for Maximum Axial and Shear Buckling Capacity
    typeJournal Paper
    journal volume113
    journal issue3
    journal titleJournal of Energy Resources Technology
    identifier doi10.1115/1.2905806
    journal fristpage204
    journal lastpage209
    identifier eissn1528-8994
    keywordsComposite materials
    keywordsShear (Mechanics)
    keywordsDesign
    keywordsBuckling
    keywordsNonlinear programming
    keywordsRayleigh-Ritz methods
    keywordsDeformation
    keywordsBoundary-value problems
    keywordsFibers AND Stress
    treeJournal of Energy Resources Technology:;1991:;volume( 113 ):;issue: 003
    contenttypeFulltext
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