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Dynamic Analysis on Composite Laminates Subjected to Low-velocity Impact Damage

机译:低速冲击损伤复合材料层合板的动力分析

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摘要

The hierarchical and heterogeneous structure characteristics of composite laminates give rise to the difficulty in the study of the composite laminates damage under low-velocity impact. A numerical method for the evaluation of the impact damage was proposed on the basis of the continuum damage mechanics (CDM) and the cohesive zone model (CZM). The method can bring stable simulations and can effectively establish the relation between the mesoscale structure and the macroscopic response under impact. The evolution of the impact damage and the effect of single ply orientation on the impact damage resistance were investigated. It is found that the tangential delamination is the dominant form of the interface damage and more orientation of fiber can make the impact resistance improved. The prediction has a good agreement with the experimental results. The dynamic analysis is helpful for a thorough understanding of the evolution of low-velocity impact damages in composite laminates.
机译:复合材料层合板的层级和非均质结构特征使得研究复合材料层合板在低速冲击下的损伤变得困难。在连续损伤力学(CDM)和内聚力区模型(CZM)的基础上,提出了一种冲击损伤评估的数值方法。该方法可以带来稳定的模拟,并可以有效地建立冲击作用下中尺度结构与宏观响应之间的关系。研究了冲击损伤的演变以及单层取向对冲击损伤阻力的影响。发现切向分层是界面损伤的主要形式,纤维更多的取向可以提高抗冲击性。该预测与实验结果吻合良好。动态分析有助于全面了解复合材料层压板中低速冲击损伤的演变。

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