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A progressive damage model of textile composites on meso-scale using finite element method: Fatigue damage analysis

机译:纺织品复合材料中尺度渐进损伤模型的有限元分析:疲劳损伤分析

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A finite element (FE) approach for tension tension fatigue damage in textile reinforced composites on meso-scale level (fabric unit cell) is proposed. S N curves of a unidirectional composite (UD) out of the fatigue tests in fibre, transverse-fibre, in-plane-shear and out-of-plane-shear directions are used as the input for the impregnated yarns. The algorithm of multi-axial fatigue is applied to matrix-dominated fatigue, while the fibre-dominated fatigue is separately considered. The continuum damage mechanics method is used to describe the properties' deterioration. The stress redistribution introduced by stiffness degradation conjugates the damage evolution. Averaged mechanical properties of the unit cell in pre- and post-fatigue damage stages are calculated at predefined load cycle numbers, using a numerical homogenization technique. The numerical results are validated by experiments of two types of carbon/ epoxy plain weave composites, which have the same fibre/resin system but different textile structures. The validation showed good agreement between modelling and experiment. (C) 2015 Elsevier Ltd. All rights reserved.
机译:提出了一种在中尺度水平(织物晶胞)上对纺织品增强复合材料进行拉伸疲劳破坏的有限元(FE)方法。在纤维,横向纤维,面内剪切和面外剪切方向的疲劳测试中,单向复合材料(UD)的S N曲线用作浸渍纱线的输入。将多轴疲劳算法应用于基体主导的疲劳,而纤维主导的疲劳则单独考虑。连续损伤力学方法用于描述性能的劣化。刚度降低引起的应力重新分布会破坏损伤。使用数值均化技术,以预定义的载荷循环次数计算疲劳前后损伤阶段的晶胞平均力学性能。通过对两种具有相同纤维/树脂体系但织物结构不同的碳/环氧平纹编织复合材料的实验,验证了数值结果。验证表明建模与实验之间具有良好的一致性。 (C)2015 Elsevier Ltd.保留所有权利。

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