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陶瓷基复合材料高精度宏细观统一本构模型研究

高希光 宋迎东 孙志刚

高希光, 宋迎东, 孙志刚. 陶瓷基复合材料高精度宏细观统一本构模型研究[J]. 航空动力学报, 2008, 23(9): 1617-1622.
引用本文: 高希光, 宋迎东, 孙志刚. 陶瓷基复合材料高精度宏细观统一本构模型研究[J]. 航空动力学报, 2008, 23(9): 1617-1622.
GAO Xi-guang, SONG Ying-dong, SUN Zhi-gang. Multi-scale constitute model for ceramic matrix composite by high fidelity generalized method of cell[J]. Journal of Aerospace Power, 2008, 23(9): 1617-1622.
Citation: GAO Xi-guang, SONG Ying-dong, SUN Zhi-gang. Multi-scale constitute model for ceramic matrix composite by high fidelity generalized method of cell[J]. Journal of Aerospace Power, 2008, 23(9): 1617-1622.

陶瓷基复合材料高精度宏细观统一本构模型研究

基金项目: 航空科学基金(05C52013);973项目

Multi-scale constitute model for ceramic matrix composite by high fidelity generalized method of cell

  • 摘要: 基于高精度通用单胞模型(HFGMC)建立了陶瓷基复合材料(CMCs)的宏细观统一本构模型.首先基于CMCs的细观结构和损伤特点建立代表体元(RVE)并定义细观损伤变量.然后采用HFGMC模型计算细观损伤变量的演化,由此获得宏观应力应变曲线,从而建立了CMCs的宏细观统一本构模型.采用该本构模型预测了CMCs的宏观应力应变曲线,与实验结果吻合良好.结果表明该本构模型能够模拟CMCs的拉伸与损伤行文,为CMCs强度分析提供了有效手段.

     

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出版历程
  • 收稿日期:  2007-09-06
  • 修回日期:  2007-11-23
  • 刊出日期:  2008-09-28

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