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    Zeroth-Order Shear Deformation Theory for Laminated Composite Plates

    Source: Journal of Applied Mechanics:;2018:;volume( 070 ):;issue: 003::page 374
    Author:
    Ray, M. C.
    DOI: 10.1115/1.1558077
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper a zeroth-order shear deformation theory has been derived for static and dynamic analysis of laminated composite plates. The responses obtained by the theory for symmetric and antisymmetric laminates are compared with the existing solutions. The comparison firmly establishes that this new shear deformation theory can be used for both thick and thin laminated composite plates with high accuracy.
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      Zeroth-Order Shear Deformation Theory for Laminated Composite Plates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4251999
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    contributor authorRay, M. C.
    date accessioned2019-02-28T11:02:26Z
    date available2019-02-28T11:02:26Z
    date copyright6/11/2003 12:00:00 AM
    date issued2018
    identifier issn0021-8936
    identifier other374_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251999
    description abstractIn this paper a zeroth-order shear deformation theory has been derived for static and dynamic analysis of laminated composite plates. The responses obtained by the theory for symmetric and antisymmetric laminates are compared with the existing solutions. The comparison firmly establishes that this new shear deformation theory can be used for both thick and thin laminated composite plates with high accuracy.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleZeroth-Order Shear Deformation Theory for Laminated Composite Plates
    typeJournal Paper
    journal volume70
    journal issue3
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.1558077
    journal fristpage374
    journal lastpage380
    treeJournal of Applied Mechanics:;2018:;volume( 070 ):;issue: 003
    contenttypeFulltext
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