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Stable numerical simulations of propagations of complex damages in composite structures under transverse loads

机译:横向载荷下复合结构复杂损伤传播的稳定数值模拟

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摘要

In this paper, to deal with complex damage propagations in various composite structures under quasi-static transverse loads, a numerical simulation methodology based on the three-dimensional (3D) finite element method (FEM) is proposed. In this numerical model, two categories of damage patterns existing in composite structures under transverse loads are tackled independently. First, a kind of stress-based criteria is adopted to deal with the first category, which includes various in-plane damages, such as fiber breakage, transverse matrix cracking, matrix crushing, etc. Second, a bi-linear cohesive interface model is employed to deal with the second category, i.e., interface damages, such as delaminations. Also, to overcome the numerical instability problem when using the cohesive model, a simple and useful technique is proposed. In this technique, the move-limit in the cohesive zone is built up to restrict the displacement increments of nodes in the cohesive zone of laminates after delaminations occurred. The effectiveness of this method is illustrated using a DCB example and its characteristic is discussed in detail. This numerical model is further applied to various composite structures, such as 2D laminated plates and 3D laminated shells under transverse loads. The results of the numerical simulations are compared with the experimental results and good agreements are observed. The obtained information is helpful for understanding the propagation mechanisms of various damages in composite structures.
机译:本文针对准静态横向载荷作用下各种复合结构的复杂损伤传播问题,提出了一种基于三维有限元方法的三维数值模拟方法。在该数值模型中,独立解决了复合结构在横向载荷下存在的两种损坏模式。首先,采用一种基于应力的准则来处理第一类,包括各种平面内损伤,例如纤维断裂,横向基体开裂,基体破碎等。第二,建立双线性内聚界面模型。用于处理第二类,即界面损坏(例如分层)。另外,为了克服使用内聚模型时的数值不稳定性问题,提出了一种简单而有用的技术。在该技术中,建立内聚区中的移动限制以限制分层后发生层压的内聚区中节点的位移增量。使用DCB示例说明了该方法的有效性,并详细讨论了其特性。该数值模型进一步应用于各种复合结构,例如横向载荷下的2D层压板和3D层压壳。将数值模拟的结果与实验结果进行比较,并观察到良好的一致性。所获得的信息有助于理解复合结构中各种损伤的传播机理。

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