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    Dynamic Instability of Laminated Composite and Sandwich Plates Using a New Inverse Hyperbolic Zigzag Theory

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 004
    Author:
    Rosalin Sahoo
    ,
    B. N. Singh
    DOI: 10.1061/(ASCE)AS.1943-5525.0000440
    Publisher: American Society of Civil Engineers
    Abstract: The present study deals with the dynamic stability behavior of laminated composite and sandwich plates subjected to in-plane static and periodic compressive loads based on a recently developed inverse hyperbolic zigzag theory by the authors. The present model satisfies the traction-free boundary conditions on the surfaces of the plate and interlaminar continuity conditions at the layer interfaces, thus obviating the need for a shear correction factor. An efficient
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      Dynamic Instability of Laminated Composite and Sandwich Plates Using a New Inverse Hyperbolic Zigzag Theory

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    http://yetl.yabesh.ir/yetl1/handle/yetl/72235
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    contributor authorRosalin Sahoo
    contributor authorB. N. Singh
    date accessioned2017-05-08T22:08:41Z
    date available2017-05-08T22:08:41Z
    date copyrightJuly 2015
    date issued2015
    identifier other32949703.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/72235
    description abstractThe present study deals with the dynamic stability behavior of laminated composite and sandwich plates subjected to in-plane static and periodic compressive loads based on a recently developed inverse hyperbolic zigzag theory by the authors. The present model satisfies the traction-free boundary conditions on the surfaces of the plate and interlaminar continuity conditions at the layer interfaces, thus obviating the need for a shear correction factor. An efficient
    publisherAmerican Society of Civil Engineers
    titleDynamic Instability of Laminated Composite and Sandwich Plates Using a New Inverse Hyperbolic Zigzag Theory
    typeJournal Paper
    journal volume28
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000440
    treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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