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Progressive damage and failure analysis of fiber-reinforced laminated composites containing a hole

机译:含有孔的纤维增强层压复合材料的渐进损伤及失效分析

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A progressive damage and failure model for fiber reinforced laminated composites is developed in combination of finite element procedure and micromechanical model based on a unit cell. The micromechanical model can be used to evaluate failure criteria at the micro-level with fiber and matrix material properties. Once either of the constituents has damaged, the corresponding material properties are degraded by the damage factor. The micromechanical model and the damage theory are implemented in the finite software ABAQUS by using the user material subroutine UMAT and VUMAT, to model the damage progression and compute the ultimate strength of the composite laminates containing a hole. The predicted strengths for this model is compared with the experimental results, and a well agreement in the simulation and experimental resulted is revealed.
机译:基于单元电池的有限元手术和微机械模型的组合开发了纤维增强层压复合材料的渐进损伤和故障模型。微机械模型可用于评估微液的故障标准,纤维和基质材料性能。一旦两种成分损坏,相应的材料特性被损伤因子降低。微机械模型和损坏理论通过使用用户材料子程序UMAT和VUMAT在有限软件ABAQU中实现,以模拟损坏进展,并计算含有孔的复合层压板的极限强度。将该模型的预测强度与实验结果进行比较,并揭示了模拟和实验结果的良好一致性。

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