Failure Analysis of Variable鄄Stiffness Composite LaminatesWith Curvilinear Fiber Placement
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    Abstract:

    This paper presents the variable鄄stiffness composite laminates with curvilinear fiber placement finite
    element modeling method. According to the curvilinear placement rule definition of every unit of the real constant, the
    variable鄄stiffness composite laminates with curvilinear fiber placement modeling was established. Bending and compres鄄
    sion failure of two kinds of different boundary conditions was discussed, through the Tsai鄄Wu failure criterion, the
    maximum inverse strength radio index 1/ R was calculated. Taking 1/ R =1 as the critical load of failure,bending con鄄
    dition of critical failure load is increased by 16% and 21%, compression condition of failure load is increased by
    51% and 19%. The results show that variable stiffness composite can improve failure properties.

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  • Received:
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  • Online: November 28,2016
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