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    Postbuckling of Polar Orthotropic Circular Plates Retrospective

    Source: Journal of Engineering Mechanics:;1992:;Volume ( 118 ):;issue: 010
    Author:
    Archibald N. Sherbourne
    ,
    Mahesh D. Pandey
    DOI: 10.1061/(ASCE)0733-9399(1992)118:10(2087)
    Publisher: American Society of Civil Engineers
    Abstract: The postbuckling analysis of cylindrically orthotropic circular plates is a theoretically challenging problem characterized by singularities due to ortho‐tropy and axisymmetry of deformations. In addition, geometric nonlinearities and strong coupling between the in‐plane and transverse displacements make an explicit treatment difficult. The subject matter has attracted considerable attention due to recent interest in circular delamination buckling, a critical failure mode in fibrous composite laminates. A comprehensive initial‐value formulation is presented where a transformation of problem variables is introduced to include cylindrical ortho‐tropy; the resulting nonlinear, ordinary differential equations are numerically integrated using the Runge‐Kutta‐Merson method where general boundary conditions can be easily accommodated. Optimal forms of material orthotropy and their implications in pre‐ and postbuckling are examined. It is shown that the buckling load, as well as postbuckling stiffness, can be improved by increasing the orthotropy ratio, i.e., the ratio of circumferential to radial elastic modulus.
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      Postbuckling of Polar Orthotropic Circular Plates Retrospective

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    http://yetl.yabesh.ir/yetl1/handle/yetl/83606
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    contributor authorArchibald N. Sherbourne
    contributor authorMahesh D. Pandey
    date accessioned2017-05-08T22:36:29Z
    date available2017-05-08T22:36:29Z
    date copyrightOctober 1992
    date issued1992
    identifier other%28asce%290733-9399%281992%29118%3A10%282087%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/83606
    description abstractThe postbuckling analysis of cylindrically orthotropic circular plates is a theoretically challenging problem characterized by singularities due to ortho‐tropy and axisymmetry of deformations. In addition, geometric nonlinearities and strong coupling between the in‐plane and transverse displacements make an explicit treatment difficult. The subject matter has attracted considerable attention due to recent interest in circular delamination buckling, a critical failure mode in fibrous composite laminates. A comprehensive initial‐value formulation is presented where a transformation of problem variables is introduced to include cylindrical ortho‐tropy; the resulting nonlinear, ordinary differential equations are numerically integrated using the Runge‐Kutta‐Merson method where general boundary conditions can be easily accommodated. Optimal forms of material orthotropy and their implications in pre‐ and postbuckling are examined. It is shown that the buckling load, as well as postbuckling stiffness, can be improved by increasing the orthotropy ratio, i.e., the ratio of circumferential to radial elastic modulus.
    publisherAmerican Society of Civil Engineers
    titlePostbuckling of Polar Orthotropic Circular Plates Retrospective
    typeJournal Paper
    journal volume118
    journal issue10
    journal titleJournal of Engineering Mechanics
    identifier doi10.1061/(ASCE)0733-9399(1992)118:10(2087)
    treeJournal of Engineering Mechanics:;1992:;Volume ( 118 ):;issue: 010
    contenttypeFulltext
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