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    Elastic Buckling of Multilayered Anisotropic Conical Shells

    Source: Journal of Aerospace Engineering:;2001:;Volume ( 014 ):;issue: 001
    Author:
    Chih-Ping Wu
    ,
    Chih-Wei Chen
    DOI: 10.1061/(ASCE)0893-1321(2001)14:1(29)
    Publisher: American Society of Civil Engineers
    Abstract: On the basis of 3D elasticity, asymptotic solutions for buckling analysis of multilayered anisotropic conical shells under axial compression are presented. By means of proper nondimensionalization, asymptotic expansion, and successive integration, the classical shell theory is derived as a first-order approximation to the 3D theory. Because the governing equations for various orders consist of partial differential equations with variable coefficients, the use of analytical techniques is restricted. The method of differential quadrature is adopted in the present study. The modifications of the buckling loads and associated buckling modes can be determined in a consistent and hierarchic manner by considering the solvability and normalization conditions for various orders. The critical loads of cross-ply conical shells with simply supported–simply supported boundary conditions are studied to demonstrate the performance of the present asymptotic theory.
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      Elastic Buckling of Multilayered Anisotropic Conical Shells

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    http://yetl.yabesh.ir/yetl1/handle/yetl/44935
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    contributor authorChih-Ping Wu
    contributor authorChih-Wei Chen
    date accessioned2017-05-08T21:16:03Z
    date available2017-05-08T21:16:03Z
    date copyrightJanuary 2001
    date issued2001
    identifier other%28asce%290893-1321%282001%2914%3A1%2829%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44935
    description abstractOn the basis of 3D elasticity, asymptotic solutions for buckling analysis of multilayered anisotropic conical shells under axial compression are presented. By means of proper nondimensionalization, asymptotic expansion, and successive integration, the classical shell theory is derived as a first-order approximation to the 3D theory. Because the governing equations for various orders consist of partial differential equations with variable coefficients, the use of analytical techniques is restricted. The method of differential quadrature is adopted in the present study. The modifications of the buckling loads and associated buckling modes can be determined in a consistent and hierarchic manner by considering the solvability and normalization conditions for various orders. The critical loads of cross-ply conical shells with simply supported–simply supported boundary conditions are studied to demonstrate the performance of the present asymptotic theory.
    publisherAmerican Society of Civil Engineers
    titleElastic Buckling of Multilayered Anisotropic Conical Shells
    typeJournal Paper
    journal volume14
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2001)14:1(29)
    treeJournal of Aerospace Engineering:;2001:;Volume ( 014 ):;issue: 001
    contenttypeFulltext
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