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    Dynamic Buckling of Laminated Anisotropic Spherical Caps

    Source: Journal of Applied Mechanics:;1995:;volume( 062 ):;issue: 001::page 13
    Author:
    M. Ganapathi
    ,
    T. K. Varadan
    DOI: 10.1115/1.2895879
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The dynamic axisymmetric behavior of clamped laminated composite spherical caps subjected to suddenly applied loads is investigated using an eight-noded quadrilateral doubly curved shear flexible shell element based on the field-consistency approach. Geometric nonlinearity is considered using von Karman’s strain-displacement relations. The solution is obtained using the Wilson-θ numerical integration scheme. The pressure corresponding to a sudden jump in the maximum average deflection in the time history of the shell structure is taken as dynamic buckling pressure. A detailed parametric study is carried out to bring out the effects of shell geometries and material properties, number of layers, lamination schemes, and type of loading on a dynamic buckling load.
    keyword(s): Buckling , Shells , Pressure , Stress , Shear (Mechanics) , Materials properties , Composite materials , Deflection , Displacement AND Laminations ,
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      Dynamic Buckling of Laminated Anisotropic Spherical Caps

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/114920
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    contributor authorM. Ganapathi
    contributor authorT. K. Varadan
    date accessioned2017-05-08T23:46:30Z
    date available2017-05-08T23:46:30Z
    date copyrightMarch, 1995
    date issued1995
    identifier issn0021-8936
    identifier otherJAMCAV-26361#13_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/114920
    description abstractThe dynamic axisymmetric behavior of clamped laminated composite spherical caps subjected to suddenly applied loads is investigated using an eight-noded quadrilateral doubly curved shear flexible shell element based on the field-consistency approach. Geometric nonlinearity is considered using von Karman’s strain-displacement relations. The solution is obtained using the Wilson-θ numerical integration scheme. The pressure corresponding to a sudden jump in the maximum average deflection in the time history of the shell structure is taken as dynamic buckling pressure. A detailed parametric study is carried out to bring out the effects of shell geometries and material properties, number of layers, lamination schemes, and type of loading on a dynamic buckling load.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDynamic Buckling of Laminated Anisotropic Spherical Caps
    typeJournal Paper
    journal volume62
    journal issue1
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2895879
    journal fristpage13
    journal lastpage19
    identifier eissn1528-9036
    keywordsBuckling
    keywordsShells
    keywordsPressure
    keywordsStress
    keywordsShear (Mechanics)
    keywordsMaterials properties
    keywordsComposite materials
    keywordsDeflection
    keywordsDisplacement AND Laminations
    treeJournal of Applied Mechanics:;1995:;volume( 062 ):;issue: 001
    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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