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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers, Part C. Journal of mechanical engineering science >Numerical modeling of diffuse transverse cracks and induced delamination using cohesive elements
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Numerical modeling of diffuse transverse cracks and induced delamination using cohesive elements

机译:弥散横向裂纹和诱发分层的数值模拟

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摘要

This article is devoted to the modeling of spread kind of damages such as matrix cracking and induced delamination in symmetric and asymmetric cross-ply laminates of composite materials using cohesive elements. For matrix crack modeling, parallel rows of cohesive elements are used between every row of 2D elements in 90° layers. Delamination is also modeled by cohesive elements at the 90°/0° interface. Since matrix cracking is a diffuse kind of damage mechanism, application of cohesive elements is not straightforward, and special techniques are necessary to resolve the modeling difficulties. For this purpose, two techniques of "bisecting" and "random distribution of strength of cohesive elements" are proposed here. Both techniques are applied to various symmetric laminates of [0/90_3]_s and [90_n/0]_s (n = 1 to 3). The predicted stiffness and damage progresses from both techniques are in good agreement with the experimental results. Then, asymmetric cross-ply laminates of [90_n/0] (n = 1 to 3) are analyzed to show the capability of this method in progressive damage analyses. The proposed method is less restricted in comparison with available micromechanical methods and is able to predict damage initiation, propagation and damage-mode transition for any symmetric and asymmetric cross-ply sequence. Therefore, this method can be used for development of "in-plane damage" of constitutive laws especially when specimens are subjected to complex loading and boundary conditions.
机译:本文致力于对使用粘性元件的复合材料的对称和非对称交叉铺层层压板中的蔓延损伤进行建模,例如基体开裂和诱发分层。对于矩阵裂缝建模,在90°层中的每行2D元素之间使用平行行的粘合元素。脱层还通过90°/ 0°界面处的粘性元素进行建模。由于基体开裂是一种弥散性的损伤机制,因此内聚元素的应用并不简单,需要专门的技术来解决建模难题。为此,在此提出了“平分”和“粘结元件强度的随机分布”的两种技术。两种技术都应用于[0 / 90_3] _s和[90_n / 0] _s(n = 1到3)的各种对称层压板。两种技术的预测刚度和损伤进展与实验结果非常吻合。然后,对[90_n / 0](n = 1至3)的不对称交叉层压材料进行分析,以显示该方法在渐进式损伤分析中的能力。与可用的微机械方法相比,该方法的局限性较小,并且能够预测任何对称和非对称交叉层序列的损伤引发,传播和损伤模式转变。因此,该方法可用于发展本构定律的“面内损伤”,尤其是当样品承受复杂的载荷和边界条件时。

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