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The in situ matrix cracking behavior in cross-ply laminates under out-of-plane shear loading

机译:面外剪切荷载作用下交叉层合板的原位基体开裂行为

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摘要

The in situ effect on cross-ply laminates under out-of-plane shear loading is firstly studied with a twodimensional RVE-based computational micromechanics method. High fidelity simulations of the interface debounding and crack propagation in laminates are performed, which shows good consistency with experimental observation. The matrix cracking behaviors and micro-mechanical response demonstrate that an in situ effect exists in cross-ply composites under out-of-plane shearing. Specifically, thinner ply laminates provide higher shear strength and stronger damage resistance due to the delay effect of transverse cracking and delamination. The analytical predictions on interlaminar shear strength of cross-ply laminates agree well with the existing theoretical criteria. A parametric study is performed to explore the possibility of acquiring stronger fiber-reinforced composites. The coupled load analysis sheds useful insights on the failure mechanism and optimization design of multi-layer composites.
机译:首先采用基于二维RVE的计算微观力学方法研究了面外剪切荷载作用下交叉层合板的原位效应。对层合板中的界面脱边界和裂纹扩展进行了高保真模拟,结果与实验结果吻合较好。基体开裂行为和微观力学响应表明,在面外剪切作用下,交叉层复合材料存在原位效应。具体来说,由于横向开裂和分层的延迟效应,较薄的层压板具有更高的剪切强度和更强的抗损伤性。对交叉层合板层间剪切强度的解析预测与现有的理论准则吻合较好。进行了参数研究,以探索获得更强的纤维增强复合材料的可能性。耦合载荷分析为多层复合材料的破坏机理和优化设计提供了有益的见解。

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