A Simple Analysis on Buckling of Composite Laminated Cylindrical Shells Subjected to Simultaneous Loading with Hydrostatic Pressure and Torsion

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In general, composite laminated cylindrical shells exhibit the effect of lamination constitution due to anisotropy and unsymmetry of lamination. In this paper, the buckling problems of carbon-fiber/epoxy (CFRP) cross-ply and angle-ply laminated cylindrical shells subjected to simultaneous loading with hydrostatic pressure and torsion are considered. The effects of stacking sequence, number of layers, lamination angle, buckling modes, load ratio and dimension of cylinders, on the buckling value are analysed by assuming the buckling patterns which satisfy the Donnell-type equilibrium equations.

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詳細情報 詳細情報について

  • CRID
    1570854176830081792
  • NII論文ID
    110000030887
  • NII書誌ID
    AA11060702
  • ISSN
    03880788
  • 本文言語コード
    en
  • データソース種別
    • CiNii Articles

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