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Progressive damage modeling of plain weave E-glass/phenolic composites

机译:平纹电子玻璃/酚醛复合材料的渐进损伤建模

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An optimized set of material properties and parameters for E-glass/phenolic composites is determined for use in the rate dependent composite damage model MAT162 in LS-DYNA. The model requires 39 material properties and parameters, and is able to capture the seven different damage modes and post damage softening behavior of composites. The unknown MAT162 parameters were determined by conducting parametric simulations of low velocity impact (LVI), depth of penetration (DOP), and ballistic impacts. The modulus reduction parameter OMGMX is found by simulating LVI tests and varying the values of OMGMX to find the best agreement with LVI experimental data. The limit of compressive volume strain for element eroding was found by simulating DOP experiments and comparing the results to the experimental data. Then the element eroding axial strain E_LIMT and EEXPN were determined by simulating ballistic impact experiments. When the optimized values were determined, analysis of ballistic experiments were conducted and compared to the experimental impact versus residual velocity curve. The results of the simulations were in excellent agreement with the experimental data.
机译:确定了用于电子玻璃/酚醛复合材料的一组优化的材料性能和参数,以用于LS-DYNA中与速率相关的复合材料损伤模型MAT162。该模型需要39种材料属性和参数,并且能够捕获七种不同的损伤模式并发布复合材料的损伤软化行为。未知的MAT162参数是通过对低速撞击(LVI),穿透深度(DOP)和弹道撞击进行参数模拟确定的。通过模拟LVI测试并更改OMGMX的值以找到与LVI实验数据的最佳一致性,可以找到模量降低参数OMGMX。通过模拟DOP实验并将结果与​​实验数据进行比较,得出了元素侵蚀的压缩体积应变极限。然后通过模拟弹道冲击实验确定了腐蚀元件的轴向应变E_LIMT和EEXPN。确定最佳值后,将进行弹道实验分析,并将其与实验冲击对残余速度的曲线进行比较。模拟结果与实验数据非常吻合。

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