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    Effect of Normal Strains in Buckling of Thick Orthotropic Shells

    Source: Journal of Aerospace Engineering:;2000:;Volume ( 013 ):;issue: 003
    Author:
    George A. Kardomateas
    DOI: 10.1061/(ASCE)0893-1321(2000)13:3(85)
    Publisher: American Society of Civil Engineers
    Abstract: An improved elasticity solution to the problem of buckling of orthotropic cylindrical shells subjected to external pressure is presented. The 2D axisymmetric cylindrical shell is studied (ring approximation). Specifically, in the development of the governing equations and boundary conditions for the buckling state, the solution includes the terms with the prebuckling normal strains and stresses as coefficients (i.e., the terms
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      Effect of Normal Strains in Buckling of Thick Orthotropic Shells

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    http://yetl.yabesh.ir/yetl1/handle/yetl/44925
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    contributor authorGeorge A. Kardomateas
    date accessioned2017-05-08T21:16:02Z
    date available2017-05-08T21:16:02Z
    date copyrightJuly 2000
    date issued2000
    identifier other%28asce%290893-1321%282000%2913%3A3%2885%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44925
    description abstractAn improved elasticity solution to the problem of buckling of orthotropic cylindrical shells subjected to external pressure is presented. The 2D axisymmetric cylindrical shell is studied (ring approximation). Specifically, in the development of the governing equations and boundary conditions for the buckling state, the solution includes the terms with the prebuckling normal strains and stresses as coefficients (i.e., the terms
    publisherAmerican Society of Civil Engineers
    titleEffect of Normal Strains in Buckling of Thick Orthotropic Shells
    typeJournal Paper
    journal volume13
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2000)13:3(85)
    treeJournal of Aerospace Engineering:;2000:;Volume ( 013 ):;issue: 003
    contenttypeFulltext
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