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考虑孔隙的针刺C/SiC复合材料弹性参数计算

李龙 高希光 史剑 宋迎东

李龙, 高希光, 史剑, 宋迎东. 考虑孔隙的针刺C/SiC复合材料弹性参数计算[J]. 航空动力学报, 2013, 28(6): 1257-1263.
引用本文: 李龙, 高希光, 史剑, 宋迎东. 考虑孔隙的针刺C/SiC复合材料弹性参数计算[J]. 航空动力学报, 2013, 28(6): 1257-1263.
LI Long, GAO Xi-guang, SHI Jian, SONG Ying-dong. Calculation of needled C/SiC composite elastic parameters in consideration of the porosity[J]. Journal of Aerospace Power, 2013, 28(6): 1257-1263.
Citation: LI Long, GAO Xi-guang, SHI Jian, SONG Ying-dong. Calculation of needled C/SiC composite elastic parameters in consideration of the porosity[J]. Journal of Aerospace Power, 2013, 28(6): 1257-1263.

考虑孔隙的针刺C/SiC复合材料弹性参数计算

基金项目: 自然科学基金(51105195,51075204); 航空科学基金(2011ZB52024)

Calculation of needled C/SiC composite elastic parameters in consideration of the porosity

  • 摘要: 基于针刺陶瓷基复合材料试件(CMCs)光学显微照片的微观型貌,并选择恰当的代表体积单元(RVE),建立了针刺陶瓷基复合材料弹性性能预测的单胞模型.考虑了孔隙率对基体和纤维束弹性性能的影响,采用混合率计算出纤维束的弹性常数,然后将纤维束和基体的弹性参数代入到单胞模型中,通过有限元法计算得到复合材料的整体弹性常数.开展了材料拉伸试验和孔隙率测定试验,测得材料的开孔孔隙率为7.33%,闭孔孔隙率为10.67%,弹性性能的计算结果与试验吻合较好,误差为3.1%.

     

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出版历程
  • 收稿日期:  2012-06-21
  • 刊出日期:  2013-06-28

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