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    Nonlinear Static Response and Free Vibration Analysis of Doubly Curved Cross-Ply Panels

    Source: Journal of Aerospace Engineering:;2007:;Volume ( 020 ):;issue: 001
    Author:
    J. Girish
    ,
    L. S. Ramachandra
    DOI: 10.1061/(ASCE)0893-1321(2007)20:1(45)
    Publisher: American Society of Civil Engineers
    Abstract: In this paper, the nonlinear static and free vibration analyses of doubly curved cross-ply laminated panels subjected to thermomechanical loading are examined. The shell theory adopted in the present case is an extension of Reissner’s shallow shell simplifications that accounts for parabolic distribution of the transverse shear strains through thickness of the shell and tangential stress-free boundary conditions. A multiterm Galerkin’s method is adopted to solve the governing nonlinear partial differential equations. The static equilibrium paths are traced using the Newton-Raphson method in conjunction with the Riks approach to overcome the limit points. The free vibration frequencies about a static equilibrium state of a deformed panel are reported by solving the linear eigenvalue problem. Analytical results are presented for symmetric [0/90/0] and antisymmetric [0/90] cross-ply laminated doubly curved panels that illustrate the influence of geometric properties, in-plane edge boundary conditions, lateral distributed load and temperature field on the nonlinear behavior and natural frequencies.
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      Nonlinear Static Response and Free Vibration Analysis of Doubly Curved Cross-Ply Panels

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    http://yetl.yabesh.ir/yetl1/handle/yetl/45079
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    contributor authorJ. Girish
    contributor authorL. S. Ramachandra
    date accessioned2017-05-08T21:16:18Z
    date available2017-05-08T21:16:18Z
    date copyrightJanuary 2007
    date issued2007
    identifier other%28asce%290893-1321%282007%2920%3A1%2845%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45079
    description abstractIn this paper, the nonlinear static and free vibration analyses of doubly curved cross-ply laminated panels subjected to thermomechanical loading are examined. The shell theory adopted in the present case is an extension of Reissner’s shallow shell simplifications that accounts for parabolic distribution of the transverse shear strains through thickness of the shell and tangential stress-free boundary conditions. A multiterm Galerkin’s method is adopted to solve the governing nonlinear partial differential equations. The static equilibrium paths are traced using the Newton-Raphson method in conjunction with the Riks approach to overcome the limit points. The free vibration frequencies about a static equilibrium state of a deformed panel are reported by solving the linear eigenvalue problem. Analytical results are presented for symmetric [0/90/0] and antisymmetric [0/90] cross-ply laminated doubly curved panels that illustrate the influence of geometric properties, in-plane edge boundary conditions, lateral distributed load and temperature field on the nonlinear behavior and natural frequencies.
    publisherAmerican Society of Civil Engineers
    titleNonlinear Static Response and Free Vibration Analysis of Doubly Curved Cross-Ply Panels
    typeJournal Paper
    journal volume20
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2007)20:1(45)
    treeJournal of Aerospace Engineering:;2007:;Volume ( 020 ):;issue: 001
    contenttypeFulltext
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