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A Blended Damage and Fracture Mechanics Model for Progressive Damage Analysis of Notched Composite Structures

机译:缺口复合结构渐进式损伤分析的混合损伤与断裂力学模型

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This paper presents a blended continuum damage and fracture mechanics finiteelement model for the progressive damage analysis of composite structures subjectedto quasi-static loading. Continuum damage modeling, utilizing the failure criterion ofPuck, was used to predict the damage initiation of matrix cracks and fibre failures,while fracture mechanics was used to model onset and propagation of delaminationand the propagation of matrix cracks. Numerical implementation was performed in thecommercial software ABAQUS, extended with user subroutines for materialconstitutive behaviour.The numerical framework was validated using experimental results found inliterature of open-hole specimens subjected to tensile loading. As the main focus wasgiven on the capability of the model to predict different failure patterns, the ply-blockeffect was investigated using a [45n/90n/-45n/0n]s with n=1,2,4,8 lay-up made ofIM7/8552 composite prepreg. The proposed model was benchmarked against a modelthat uses only continuum damage approach and it was found that it can predictaccurately the failure load the damage pattern especially when delamination is thedominant damage mechanism and interacts with matrix cracking, while the othermodel fails to predict even the failure load.
机译:本文提出了一种混合的连续损伤与断裂力学有限元 组合结构渐进式损伤分析的有限元模型 准静态负载。连续损伤建模,利用破坏准则 帕克(Puck)用于预测基体裂纹和纤维失效的破坏起因, 而断裂力学被用来模拟分层的开始和传播 以及基体裂纹的扩展。数值实现是在 商业软件ABAQUS,扩展了用户子例程以用于材料 本构行为。 使用在 裸眼试样承受拉伸载荷的文献。主要重点是 鉴于模型预测不同失效模式的能力,层板 使用[45n / 90n / -45n / 0n] s进行了研究,其中n = 1,2,4,8由 IM7 / 8552复合预浸料。提议的模型以模型为基准 仅使用连续损伤法,发现它可以预测 准确地讲,破坏载荷是损坏模式,尤其是当分层是 占主导地位的破坏机制,并与基体开裂相互作用,而另一个 模型甚至无法预测故障负荷。

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