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From diffuse damage to discrete crack: A coupled failure model for multi-stage progressive damage of composites

机译:来自离散裂缝的漫反射损伤:复合材料多阶段逐行损伤的耦合故障模型

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The multi-stage failure process and the coupled failure mechanisms have posed great challenges to damage analyses of fibre-reinforced composite laminates. In this study, a coupled failure model (CFM) is proposed which incorporates both smeared crack model (SCM) and discrete crack model (DCM) through an energy-consistent thermodynamic framework. While SCM is well suited for describing crack nucleation and diffuse damage at initial failure stage, DCM offers a great tool to model the subsequent crack growth and its interaction with other failure modes. A hybrid SCM/DCM formulation is developed for CFM, so that the progressive failure process from diffuse damage to propagation of major cracks is characterized. Furthermore, inherent limitations of each standalone model, such as convergence difficulty and computational inefficiency, are effectively resolved by the proposed approach. Performance of CFM is demonstrated through a few numerical examples, including element validation, Off-axis tensile and open-hole tension tests of composite laminates. (C) 2021 Elsevier B.V. All rights reserved.
机译:多级故障过程和耦合失效机制对纤维增强复合材料层压板的损伤分析构成了极大的挑战。在该研究中,提出了一种耦合故障模型(CFM),其通过能量 - 一致的热力学框架将涂抹裂缝模型(SCM)和离散裂缝模型(DCM)结合起来。虽然SCM非常适合于描述初始故障阶段的裂缝成核和漫反射损伤,但DCM提供了一种伟大的工具,可以模拟随后的裂缝增长及其与其他故障模式的互动。开发了一种用于CFM的杂交SCM / DCM配方,从而表征了主要裂缝传播的逐渐失效过程。此外,通过所提出的方法有效地解决了每个独立模型的固有局限,例如收敛难度和计算效率。通过几个数值示例来证明CFM的性能,包括元件验证,轴外拉伸和复合层压板的轴外拉伸张力试验。 (c)2021 Elsevier B.v.保留所有权利。

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