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Three-Dimensional Progressive Damage Analysis of Composite Laminates Containing a Central hole Subjected to Compressive Loading

机译:含有压缩载荷的中央孔的复合层压板的三维渐进损伤分析

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A numerical method is developed for the application of three-dimensional progressive damage analyses in composite laminates containing an open hole with arbitrary geometry and stacking sequence subjected to static compressive loading. The method developed is included in the three-dimensional FEM stress analysis, failure analysis based on three-dimensional Hashin type criterion, the material property degradation rule of ply discount. It is capable of numerically simulating the whole process of failure initiation, propagation and catastrophic failure of the structure and of predicting the ultimate strengths and failure modes of composite laminates containing an open hole. Two different lay orientations and four different W/D with an open hole are analyzed for the ultimate strength and damage progression. On the other hand, four damage mechanisms and the correlation among the damage are studied and discussed in this paper. An excellent agreement was found between data obtained from this study and the existing literature.
机译:开发了一种数值方法,用于在包含具有任意几何形状和堆叠序列的复合孔中施加三维渐进损伤分析,其进行静态压缩载荷的任意几何形状和堆叠序列。所开发的方法包括在三维有限元应力分析,基于三维Hashin类型标准的故障分析中,材料属性降解规则的折扣。它能够在数值上模拟结构的故障启动,传播和灾难性故障的整个过程,以及预测含有开孔的复合层压板的最终强度和故障模式。分析了两种不同的铺面方向和四个不同的W / D,用于终极强度和损坏进展。另一方面,在本文中研究并讨论了四种损伤机制和损坏之间的相关性。从本研究中获得的数据与现有文献之间存在一个很好的协议。

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