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基于多尺度方法的平纹机织SiC/SiC复合材料力学性能预测

Prediction of Mechanical Properties Using Multi-scale Approach for Plain Woven SiC/SiC Composites

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【作者】 胡元杰; 陈绍雄; 朱书华; 徐志胜; 杨发建;

【Author】 HU Yuan-jie;CHEN Shao-xiong;ZHU Shu-hua;College of Aerospace Engineering, Nanjing University of Aeronautics & Astronautics;

【机构】 南京航空航天大学航空学院;

【摘要】 本文基于平纹机织SiC/SiC复合材料的多尺度特性以及微观结构的周期性,建立了微观尺度(纤维尺度)和中观尺度(纱线尺度)的单胞模型,利用Abaqus软件计算得出纤维尺度模型的力学性能参数,将这些参数导入纱线尺度模型中,同时编写相应的UMAT子程序来判断材料的损伤起始和损伤演化过程,模拟了平纹机织SiC/SiC复合材料在单向拉伸时的损伤演化以及破坏过程。结果表明X向拉伸应力应变曲线与试验曲线吻合良好,有效地预测了平纹机织SiC/SiC复合材料的强度性能和损伤演化过程。

【Abstract】 Based on the multi-scale characteristics and the periodicity of microstructure of plain woven SiC/SiC composites, the unit cell models of microscale(fiber-scale) and mesoscale(yarn-scale) are established. The mechanical properties parameters of the microscale model were calculated by Abaqus software, which were then introduced into the yarn-scale model. The corresponding UMAT subroutine was written to judge the damage initiation and damage evolution process of the material. The damage evolution and failure process of plain woven SiC/SiC composites under uniaxial tension were simulated. The results show that the X-direction tensile stress-strain curve is in good agreement with the experimental curve. The strength properties and damage evolution of plain woven SiC/SiC composites are predicted.

【基金】 国家科技重大专项资助项目(Y2019-I-0018-0017)
  • 【文献出处】 航空精密制造技术 ,Aviation Precision Manufacturing Technology , 编辑部邮箱 ,2024年03期
  • 【分类号】TB332
  • 【下载频次】56
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