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Tensile properties of 3D multi-layer wrapping braided composite: Progressive damage analysis

机译:3D多层包裹编织复合材料的拉伸性能:渐进式损伤分析

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摘要

An experimental and numerical study on mechanical properties and damage behavior of 3D multi-layer wrapping braided composite under axial tensile load is presented. The braiding process of this material is introduced and its tensile properties are obtained in tensile tests. Numerical simulations employ periodical boundary conditions, with interface elements between yarns and matrix added to improve the accuracy of prediction. 3D Hashin-type criteria and Von-Mises stress criterion are employed as damage initiation criteria for yams and matrix, respectively. The obtained numerical results show a good agreement with the experimental data. The load-bearing capacity and failure mechanisms of 3D multi-layer wrapping braided composites under axial tensile loading are also discussed. A stress distribution shows that the axial yarns are the main load-bearing component of the composite. The main failure mode of the yams is the yam-matrix tensile cracking in the width direction, followed by the yam-matrix tensile cracking in the thickness direction and fibre tensile failure. When the fibres in axial yams begin to break, the material loses its load-bearing capacity.
机译:给出了3D多层包裹编织复合材料在轴向拉伸载荷下的力学性能和损伤行为的实验和数值研究。引入了这种材料的编织工艺,并在拉伸试验中获得了其拉伸性能。数值模拟采用周期性边界条件,并在纱线和基体之间添加了界面元素,以提高预测的准确性。 3D Hashin型准则和Von-Mises应力准则分别用作山药和基质的破坏起始准则。数值结果与实验数据吻合良好。还讨论了3D多层包裹编织复合材料在轴向拉伸载荷下的承载能力和破坏机理。应力分布表明,轴向纱线是复合材料的主要承载组件。纱线的主要破坏方式是沿宽度方向的纱线-基体拉伸裂纹,然后是沿厚度方向的纱线-基体拉伸裂纹和纤维拉伸破坏。当轴向纱线中的纤维开始断裂时,该材料将失去其承重能力。

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