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Displacement Rate Effects on the Mode II Shear Delamination Behavior of Carbon Fiber/Epoxy Composites

机译:对碳纤维/环氧复合材料的模式II剪切分层行为的位移率效应

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摘要

This paper studies the influence of displacement rate on mode II delamination of unidirectional carbon/epoxy composites. End-notched flexure test is performed at displacement rates of 1, 10, 100 and 500 mm/min. Experimental results reveal that the mode II fracture toughness GIIC increases with the displacement, with a maximum increment of 45% at 100 mm/min. In addition, scanning electron micrographs depict that fiber/matrix interface debonding is the major damage mechanism at 1 mm/min. At higher speeds, significant matrix-dominated shear cusps are observed contributing to higher GIIC. Besides, it is demonstrated that the proposed rate-dependent model is able to fit the experimental data from the current study and the open literature generally well. The mode II fracture toughness measured from the experiment or deduced from the proposed model can be used in the cohesive element model to predict failure. Good agreement is found between the experimental and numerical results, with a maximum difference of 10%. The numerical analyses indicate crack jump occurs suddenly after the peak load is attained, which leads to the unstable crack propagation seen in the experiment.
机译:本文研究了位移率对单向碳/环氧复合材料的模式II分层的影响。端缺口弯曲试验以1,10,100和500mm / min的位移速率进行。实验结果表明,模式II断裂韧性Giic随偏移的增加,最大增量为45%,100mm / min。此外,扫描电子显微照片描绘了光纤/矩阵界面剥离是1毫米/分钟的主要损伤机制。在较高的速度下,观察到有助于更高的Giic的显着基质占状剪切尖端。此外,证明所提出的速率依赖模型能够符合目前研究和公开文学的实验数据。从实验中测量的模式II裂缝韧性或从所提出的模型中推导的粘性韧性可用于粘性元素模型以预测失败。在实验和数值结果之间发现了良好的一致性,最大差异为10%。数值分析表明峰值载荷之后突然发生裂纹跳跃,这导致实验中看到的不稳定裂纹繁殖。

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