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    Postbuckling Behavior of 3D Braided Rectangular Plates Subjected to Biaxial Compression

    Source: Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 004
    Author:
    Zhi-Min
    ,
    Li
    ,
    Wei
    ,
    Gu
    ,
    Yi-Xi
    ,
    Zhao
    DOI: 10.1061/(ASCE)AS.1943-5525.0000164
    Publisher: American Society of Civil Engineers
    Abstract: Postbuckling behavior of three-dimensional (3D) braided rectangular plates subjected to biaxial compression is presented. The 3D braided composite may be treated as a cell system, and the geometry of each cell is deeply dependent on its position in the cross section of the plate. Based on Reddy’s higher-order shear deformation plate theory and general von Kármán–type equations that include the initial geometric imperfection of the plate, a perturbation technique is employed to determine postbuckling equilibrium paths of 3D braided rectangular plates. The results reveal that the geometric and physical properties have a significant effect on the postbuckling behavior of braided composite plates.
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      Postbuckling Behavior of 3D Braided Rectangular Plates Subjected to Biaxial Compression

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    https://yetl.yabesh.ir/yetl1/handle/yetl/56312
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    • Journal of Aerospace Engineering

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    contributor authorZhi-Min
    contributor authorLi
    contributor authorWei
    contributor authorGu
    contributor authorYi-Xi
    contributor authorZhao
    date accessioned2017-05-08T21:33:54Z
    date available2017-05-08T21:33:54Z
    date copyrightOctober 2012
    date issued2012
    identifier other%28asce%29as%2E1943-5525%2E0000164.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56312
    description abstractPostbuckling behavior of three-dimensional (3D) braided rectangular plates subjected to biaxial compression is presented. The 3D braided composite may be treated as a cell system, and the geometry of each cell is deeply dependent on its position in the cross section of the plate. Based on Reddy’s higher-order shear deformation plate theory and general von Kármán–type equations that include the initial geometric imperfection of the plate, a perturbation technique is employed to determine postbuckling equilibrium paths of 3D braided rectangular plates. The results reveal that the geometric and physical properties have a significant effect on the postbuckling behavior of braided composite plates.
    publisherAmerican Society of Civil Engineers
    titlePostbuckling Behavior of 3D Braided Rectangular Plates Subjected to Biaxial Compression
    typeJournal Paper
    journal volume25
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000164
    treeJournal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 004
    contenttypeFulltext
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