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    Multiobjective Design of Symmetrically Laminated Plates

    Source: Journal of Mechanical Design:;1992:;volume( 114 ):;issue: 004::page 620
    Author:
    N. Kumar
    ,
    T. R. Tauchert
    DOI: 10.1115/1.2917052
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Multiobjective optimization of a symmetrically laminated composite plate is presented. Designs are obtained to realize maximum in-plane compressive load, maximum in-plane shear load, maximum bending strength, and maximum stiffness, two criteria being considered at a time. Design variables are fiber orientations and thicknesses of different layers. It is observed that nonconvex sets appear in the problem and consequently the weighting min-max method, rather than the pure weighting method, is used to reduce the vector maximum problem to a scalar one. Search for the optimum is then accomplished by a general nonlinear programming algorithm. Since exact solutions for the structural response are not available, the Rayleigh-Ritz method is employed to obtain approximate solutions. Numerical results are presented for different materials and various combinations of clamped, free and simply supported boundary conditions.
    keyword(s): Design AND Plates (structures) ,
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      Multiobjective Design of Symmetrically Laminated Plates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/110584
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    contributor authorN. Kumar
    contributor authorT. R. Tauchert
    date accessioned2017-05-08T23:39:03Z
    date available2017-05-08T23:39:03Z
    date copyrightDecember, 1992
    date issued1992
    identifier issn1050-0472
    identifier otherJMDEDB-27601#620_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110584
    description abstractMultiobjective optimization of a symmetrically laminated composite plate is presented. Designs are obtained to realize maximum in-plane compressive load, maximum in-plane shear load, maximum bending strength, and maximum stiffness, two criteria being considered at a time. Design variables are fiber orientations and thicknesses of different layers. It is observed that nonconvex sets appear in the problem and consequently the weighting min-max method, rather than the pure weighting method, is used to reduce the vector maximum problem to a scalar one. Search for the optimum is then accomplished by a general nonlinear programming algorithm. Since exact solutions for the structural response are not available, the Rayleigh-Ritz method is employed to obtain approximate solutions. Numerical results are presented for different materials and various combinations of clamped, free and simply supported boundary conditions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMultiobjective Design of Symmetrically Laminated Plates
    typeJournal Paper
    journal volume114
    journal issue4
    journal titleJournal of Mechanical Design
    identifier doi10.1115/1.2917052
    journal fristpage620
    journal lastpage625
    identifier eissn1528-9001
    keywordsDesign AND Plates (structures)
    treeJournal of Mechanical Design:;1992:;volume( 114 ):;issue: 004
    contenttypeFulltext
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