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Damage modelling in woven-fabric CFRP laminates under large-deflection bending

机译:大挠度弯曲下机织物CFRP层压板的损伤建模

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摘要

In this paper, various damage modes in woven carbon fabric reinforced polymer (CFRP) laminates are studied using experimental material characterisation and numerical simulations. Experimental tests are carried out to assess the mechanical behaviour of these materials under tension, compression and large-deflection bending. To obtain in-plane shear properties of laminates, tensile tests are performed using a full-field strain-measurement digital image correlation technique. Two-dimensional finite-element models are implemented in the commercial code Abaqus to study the deformation behaviour and damage in large-deflection bending of CFRP laminates. In these models, multiple layers of bilinear cohesive-zone elements are employed between elements of each fabric ply to analyse the onset and progression of inter-ply delamination. Intra-ply fabric fracture is modelled by inserting a transverse layer of cohesive elements at the laminate centre. The developed numerical models are capable to simulate these damage features as well as their subsequent mode coupling observed in tests. The obtained results of simulations show good agreement with experimental data, thus demonstrating that the proposed methodology can be used for simulations of discrete damage mechanisms and their interaction during the ultimate fracture of composites in bending.
机译:在本文中,使用实验材料表征和数值模拟研究了机织碳纤维增强聚合物(CFRP)层压板的各种损伤模式。进行实验测试以评估这些材料在拉伸,压缩和大挠度弯曲下的机械性能。为了获得层压板的面内剪切性能,使用全场应变测量数字图像相关技术进行拉伸测试。在商业代码Abaqus中实现了二维有限元模型,以研究CFRP层压板在大挠度弯曲中的变形行为和损伤。在这些模型中,在每个织物帘布层的元素之间采用了多层双线性粘合区元素,以分析层间分层的发生和进展。层内织物断裂是通过在层压材料中心插入一个横向的粘合元件层来模拟的。开发的数值模型能够模拟这些损坏特征以及在测试中观察到的其后续模式耦合。仿真结果与实验数据吻合良好,表明所提出的方法可用于复合材料弯曲破坏过程中离散损伤机理及其相互作用的仿真。

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