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Verification of a micro-mechanical approach for the investigation of progressive damage in composite laminates

机译:验证复合层压板逐步损伤的微机械方法

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摘要

In this paper, micro-damage mechanics (MIDM) and macro-damage mechanics (MADM) are employed to study the progressive damage in composite laminates. Firstly, a novel method for progressive damage modeling of composite laminates is proposed based on MADM rules. In the MADM method, a new exponential behavior for the softening regime of damaged plies is proposed from comprehensive experimental tests on glass/epoxy composite laminates with a variety of the stacking sequence. Then, a MIDM model is employed to study the mechanical behavior of composite laminates with micro-cracks. The effective elastic moduli and Poisson's ratio in damaged composite laminates containing a large number of micro-cracks are determined by utilizing variational methods. Finally, the proposed exponential behavior of damaged plies based on MADM rules is verified by utilizing a MIDM model. The resulting coincidence of MADM and MIDM proves that the proposed method can accurately simulate the behavior of damaged plies in glass/epoxy composite laminates.
机译:本文采用微损伤力学(MIDM)和宏观损伤力学(MADM)来研究复合层压板中的渐进损伤。首先,提出了一种基于MADM规则的复合层压板的渐进损伤建模的新方法。在MADM方法中,从玻璃/环氧复合层压板上的综合实验试验提出了一种新的损坏层制度的新指数行为,具有各种堆叠序列。然后,采用MIDM模型来研究复合层压板与微裂纹的力学行为。通过利用变分方法确定含有大量微裂纹的受损复合层压板中的有效弹性模和泊松比。最后,通过利用MIDM模型来验证基于MADM规则的受损层的拟议指数行为。 MADM和MINM的由此产生的巧合证明,该方法可以准确地模拟玻璃/环氧复合材料层压板中受损损坏的行为。

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