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Damage Prediction of A Composite Laminate Under Quasi-Static Indentation Force

机译:准静态压痕力作用下复合材料层合板的损伤预测

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Composite laminates were tested by using the quasistatic indentation test method. The damage onset and propagation on the laminates was recorded and modeled by using solid46 element of ANSYS. According to the test results,the first unloading point on the contact force/indenter displacement curve doesn't correspond to the initiation of delamination. By using the solid46 element of ANSYS and failure criteria,the finite element model can predict the linear section of the contact force/indenter displacement curve and the contact force of the first unloading point with good accuracy.
机译:通过使用准静态压痕测试方法测试复合材料层压板。使用ANSYS的solid46元素记录并模拟了层压板上的损伤起因和蔓延。根据测试结果,接触力/压头位移曲线上的第一个卸载点并不对应于分层的开始。通过使用ANSYS的solid46元素和破坏准则,有限元模型可以准确地预测接触力/压头位移曲线的线性截面和第一个卸载点的接触力。

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