Volume 15, Issue 3 (September 1993)

    Buckling Analyses of Fiber-Composite Laminate Shells with Material Nonlinearity

    CODEN: CTROAD

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    Abstract

    A nonlinear material constitutive model, including a nonlinear in-plane shear formulation and a failure criterion, for fiber-composite laminate materials is employed to carry out finite-element buckling analyses for composite shells under hydrostatic compressive loads. It has been shown that the nonlinear in-plane shear together with the failure criterion have significant influence on the buckling behavior of composite shells.


    Author Information:

    Hu, H-T
    Associate professor, National Cheng Kung University, Tainan, Taiwan,


    Stock #: CTR10370J

    ISSN: 0884-6804

    DOI: 10.1520/CTR10370J

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    Author
    Title Buckling Analyses of Fiber-Composite Laminate Shells with Material Nonlinearity
    Symposium , 0000-00-00
    Committee D30