首页> 中文期刊>海军航空工程学院学报 >三维J积分理论在固体火箭发动机裂纹研究中的应用

三维J积分理论在固体火箭发动机裂纹研究中的应用

     

摘要

针对固体火箭发动机药柱上裂纹的三维性和受力复杂性,文章提出采用三维J积分理论和数值仿真来计算药柱上裂纹缝线上的J积分值,并给出了三维J积分的体积分表达式和有限元数值分析方法;通过对固体火箭发动机药柱上在燃烧室星角处的一条典型裂纹——横向贯穿楔形裂纹仿真计算,得出裂纹缝线上J积分值呈现中间高两端低的非均匀分布特点,证明了三维J积分理论在固体火箭发动机装药裂纹危险性研究上的适用性。%Aiming to the 3-D characteristics of the crack and its force application complexity in solid rocket motor grain, the application of 3-D J-integral theory and numerical simulation to calulate the J-integral values at the Gauss integration points of the crack line was proposed in the dissertation, and the 3-D volumic J-integral expression and the finite-element numerical analysis method were given out. The wedge crack which traversed through the projection of star grain was simu⁃lated as a typical crack in solid rocket motor. As shown in the calculation results, the J-integral distribution along the crack front line behaved as the varying characteristics of high value at the center and low value in both sides, which proved that 3-D J-integral calculation method was suitable to reasearch the risk of solid rocket motor grain crack.

著录项

相似文献

  • 中文文献
  • 外文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号