期刊文献+

纤维增强陶瓷基复合材料热结构综合强度与渐进损伤分析方法研究 被引量:1

Integrated strength and progressive damage analysis for fiber reinforced ceramic matrix composites
下载PDF
导出
摘要 针对纤维增强陶瓷基复合材料热结构力学性能特点,基于Tsai-Wu强度准则,提出了一种适用于纤维增强陶瓷基复合材料热结构综合强度分析的三维实体型渐进损伤分析方法;基于ANSYS软件APDL语言完成了分析方法的程序开发和实现,并通过与文献经典算例及典型热结构强度试验结果的对比分析,验证了本文方法的合理性和正确性。研究结果表明:本文方法可有效分析和预示纤维增强陶瓷基复合材料热结构的承载能力和损伤失效形式,具有很高仿真分析精度,解决了力热综合条件下复杂热结构强度预示与渐进损伤分析评估技术难题。 Aiming at the mechanical property of fiber reinforced ceramic matrix composites thermalstructure,basing on the Tsai-wu strength criterion,the integrated strengh and progressive damage analysisfor three dimensional solid model of fiber reinforced ceramic matrix composites thermal structure wasproposed.The calculation program of the presented method was developed basing on the APDL of ANSYS.The correctness and rationality of the presented method was verified by comparing with classical model ofliterature and experimentation result of thermal Structures.The results show that the presented method iseffective and accurate on indicating the integrated strengh and damage of fiber reinforced ceramic matrixcomposites thermal structure,especially for complicated loads cases.
作者 吴勇军 屈强 许小静 辛健强 董永朋 WU Yongjun;QU Qiang;XU Xiaojing;XIN Jianqiang;DONG Yongpeng(Research and Development Center, China Academy of Launch Vehicle Technology, Beijing 100076, China)
出处 《强度与环境》 2017年第1期43-50,共8页 Structure & Environment Engineering
基金 国家自然科学基金项目资助(11572353 51572298 11502306)
关键词 纤维增强陶瓷基复合材料 热结构 强度分析 渐进损伤 fiber reinforced ceramic matrix composites thermal structure strength analysis progressive damage
  • 相关文献

参考文献3

二级参考文献42

  • 1王丹勇,温卫东,崔海涛.复合材料单钉接头三维逐渐损伤破坏分析[J].复合材料学报,2005,22(3):168-174. 被引量:41
  • 2华玉,郦正能,冠长河,罗小东,何庆芝.复合材料单钉接头的损伤累积模拟[J].航空学报,1995,16(2):153-159. 被引量:10
  • 3张爽,王栋,郦正能,寇长河,章怡宁.复合材料层合板机械连接结构累积损伤模型和挤压性能试验研究[J].复合材料学报,2006,23(2):163-168. 被引量:23
  • 4徐焜,许希武.三维编织复合材料渐进损伤的非线性数值分析[J].力学学报,2007,39(3):398-407. 被引量:31
  • 5Chang F K, Chang K Y. A progressive damage model for laminated composites containing stress concentrations [J]. Journal of Composite Materials, 1987, 21(9): 834-855.
  • 6Chang F K, Chang K Y. Post failure analysis of bolted eomposite joints in tension or shear out mode failure [J].Journal of Composite Materials, 1987, 21(9): 809-833.
  • 7Chang K Y, Lessard L B. Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings Ⅰ: Analysis [J]. Journal of Composite Materials, 1991, 25(1): 2-43.
  • 8Tan S C. A progressive failure model for composite laminates containing openings [J]. Journal of Composite Materials, 1991, 25(5): 556-577.
  • 9Tan S C, Perez J. Progressive failure of laminated composites with a hole under compressive loading[J]. Journal of Reinforced Plastics and Composites, 1993, 12(10): 1043-1057.
  • 10Sleight D W. Progressive failure analysis methodology for laminated composite structures, NASA/TP - 1999 - 209107[R]. Washington: NASA, 1999: 1-25.

共引文献88

同被引文献6

引证文献1

二级引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部