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Simulation and experimental study of mechanical and fracture behavior of 2.5D woven C-fiber/aluminum composites under warp directional tension loading

机译:探测型扭转张力下轧件2.5D编织C-纤维/铝复合材料的机械和断裂行为的仿真及实验研究

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The mechanical and fracture behavior of innovative 2.5D woven fabric/aluminum composites under warp directional tension were investigated via micro-mechanical simulation and experiments. The tensile curves from the simulation correspond well with the testing curves, where calculation errors of the elastic modulus, ultimate strength, and fracture strain are 3.96%, 1.40%, and -5.49%, respectively. The warp yarn interface and neighboring matrix are damaged during the initial tension process. The accumulation and interaction of these damage zones lead to successive failures of the interface, matrix, and weft yarns. The axial fracture of warp yarns ultimately induces failure of the composite, which exhibits transverse crack of weft yarns with interfacial debonding and axial fracture of warp yarns with fiber pulling out. The elastic modulus and ultimate strength increased with an increase in the weft yarn layer spacing or a decrease in the warp yarn layer spacing, whereas the fracture strain decreased with an increase in the layer spacing of the warp or weft yarns.
机译:通过微机械仿真和实验研究了经线方向张力下的创新2.5D织物/铝复合材料的机械和断裂行为。来自模拟的拉伸曲线与测试曲线很好,其中弹性模量,极性强度和断裂菌株的计算误差分别为3.96%,1.40%和-5.49%。在初始张力过程中,经纱界面和相邻矩阵损坏。这些损伤区域的累积和相互作用导致界面,矩阵和纬纱的连续故障。经线纱线的轴向骨折最终诱导复合材料的故障,这表现出纬纱的横裂裂纹,具有纤维拉出的横向剥离和轴向骨折。弹性模量和极限强度随着纬纱层间距的增加或经纱层间距的减小而增加,而断裂应变随着经纱或纬纱的层间距的增加而降低。

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