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    Postbuckling of FGM Cylindrical Panels Resting on Elastic Foundations Subjected to Axial Compression under Heat Conduction

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 004
    Author:
    Hui-Shen Shen
    ,
    Hai Wang
    DOI: 10.1061/(ASCE)AS.1943-5525.0000439
    Publisher: American Society of Civil Engineers
    Abstract: A postbuckling analysis is presented for functionally graded material (FGM) cylindrical panels resting on elastic foundations subjected to axial compression under heat conduction. Two kinds of micromechanics models, namely, Voigt model and Mori-Tanaka model, are considered. The material properties of FGMs are assumed to be graded in the thickness direction according to a simple power law distribution in terms of the volume fractions of the constituents and are assumed to be temperature-dependent. The formulations are based on a higher-order shear deformation theory with a von Kármán-type of kinematic nonlinearity. The panel-foundation interaction and thermal effects are also included. The nonlinear prebuckling deformations and initial geometric imperfections of the panel are both taken into account. A singular perturbation technique along with a two-step perturbation approach is employed to determine the buckling loads and postbuckling equilibrium paths. The effects of volume fraction index, temperature variation, foundation stiffness, panel curvature ratio as well as the in-plane boundary condition of straight edges on the postbuckling behavior of FGM cylindrical panels are discussed in detail.
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      Postbuckling of FGM Cylindrical Panels Resting on Elastic Foundations Subjected to Axial Compression under Heat Conduction

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    http://yetl.yabesh.ir/yetl1/handle/yetl/81066
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    contributor authorHui-Shen Shen
    contributor authorHai Wang
    date accessioned2017-05-08T22:27:56Z
    date available2017-05-08T22:27:56Z
    date copyrightJuly 2015
    date issued2015
    identifier other45845015.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/81066
    description abstractA postbuckling analysis is presented for functionally graded material (FGM) cylindrical panels resting on elastic foundations subjected to axial compression under heat conduction. Two kinds of micromechanics models, namely, Voigt model and Mori-Tanaka model, are considered. The material properties of FGMs are assumed to be graded in the thickness direction according to a simple power law distribution in terms of the volume fractions of the constituents and are assumed to be temperature-dependent. The formulations are based on a higher-order shear deformation theory with a von Kármán-type of kinematic nonlinearity. The panel-foundation interaction and thermal effects are also included. The nonlinear prebuckling deformations and initial geometric imperfections of the panel are both taken into account. A singular perturbation technique along with a two-step perturbation approach is employed to determine the buckling loads and postbuckling equilibrium paths. The effects of volume fraction index, temperature variation, foundation stiffness, panel curvature ratio as well as the in-plane boundary condition of straight edges on the postbuckling behavior of FGM cylindrical panels are discussed in detail.
    publisherAmerican Society of Civil Engineers
    titlePostbuckling of FGM Cylindrical Panels Resting on Elastic Foundations Subjected to Axial Compression under Heat Conduction
    typeJournal Paper
    journal volume28
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000439
    treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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