首页 | 本学科首页   官方微博 | 高级检索  
     检索      

陶瓷基复合材料基体裂纹偏转能量释放率研究
引用本文:张鸿,宋迎东.陶瓷基复合材料基体裂纹偏转能量释放率研究[J].航空动力学报,2007,22(10):1730-1736.
作者姓名:张鸿  宋迎东
作者单位:南京航空航天大学,能源与动力学院,南京,210016;南京航空航天大学,能源与动力学院,南京,210016
摘    要:采用虚裂纹闭合技术(VCCT)计算了基体裂纹在界面处不同传播路径的能量释放率,并结合基于能量释放率的裂纹偏转准则对陶瓷基复合材料基体裂纹偏转进行了研究.计算了弹性错配参数α和β、基体裂纹扩展长度a、基体裂纹相对扩展长度ad/ap对裂纹偏转的影响,并将VCCT计算结果与积分法的计算结果进行比较.结果表明:VCCT能够准确计算基体裂纹扩展时的能量释放率,计算结果可为研究陶瓷基复合材料失效机制提供一定参考. 

关 键 词:航空、航天推进系统  裂纹偏转  虚裂纹闭合技术  陶瓷基复合材料  能量释放率
文章编号:1000-8055(2007)10-1730-07
收稿时间:2006/9/19 0:00:00
修稿时间:2006年9月19日

Study of energy release rates for crack deflection of ceramic matrix composites
ZHANG Hong and SONG Ying-dong.Study of energy release rates for crack deflection of ceramic matrix composites[J].Journal of Aerospace Power,2007,22(10):1730-1736.
Authors:ZHANG Hong and SONG Ying-dong
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:The energy release rates of different crack paths at interfaces were estimated by using virtual crack closure technique(VTTC).An energy criterion based on the energy release rates was used to study the crack deflection of ceramic matrix composites.Meanwhile, and the effects of elastic mismatch parameters α and β, the crack growth length a and the relative crack growth length ad/ap on the crack deflection were analyzed.The VCCT results were compared with those obtained by integration method.The results show that, VCCT can accurately calculate the energy release rates of crack growth, providing a reference for study of failure mechanism of ceramic matrix composites. 
Keywords:aerospace propulsion system  crack deflection  virtual crack closure technique  ceramic matrix composites  energy release rates
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号