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

单向陶瓷基复合材料单轴拉伸强度研究
引用本文:李龙彪,宋迎东,孙志刚.单向陶瓷基复合材料单轴拉伸强度研究[J].航空动力学报,2010,25(10):2177-2187.
作者姓名:李龙彪  宋迎东  孙志刚
作者单位:南京航空航天大学 能源与动力学院, 南京 210016
基金项目:南京航空航天大学博士论文创新与创优基金,江苏省普通高校研究生创新基金,博士点基金 
摘    要:采用细观力学方法对单向纤维增强陶瓷基复合材料单轴拉伸强度进行研究.采用剪滞模型描述复合材料出现损伤后的细观应力场,结合基体随机开裂模型、断裂力学界面脱黏准则确定基体裂纹间距及界面脱黏长度.当基体裂纹达到饱和后,假设纤维强度服从威布尔分布,完好纤维和断裂纤维承载满足总体载荷承担法则,采用纤维随机失效模型确定继续加载过程中纤维断裂概率及断裂位置,当纤维承载达到最大时,复合材料失效.讨论了基体威布尔模量和特征强度、纤维/基体界面剪应力和界面脱黏能、纤维威布尔模量和特征强度对纤维失效,进而对复合材料拉伸失效强度的影响.与试验数据对比表明:提出的模型是有效的. 

关 键 词:陶瓷基复合材料    基体开裂    界面脱黏    纤维失效    拉伸强度
收稿时间:9/4/2009 12:00:00 AM
修稿时间:2010/2/27 0:00:00

Study on uniaxial tensile strength of unidirectional ceramic matrix composites
LI Long-biao,SONG Ying-dong and SUN Zhi-gang.Study on uniaxial tensile strength of unidirectional ceramic matrix composites[J].Journal of Aerospace Power,2010,25(10):2177-2187.
Authors:LI Long-biao  SONG Ying-dong and SUN Zhi-gang
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:A study on uniaxial tensile strength of the unidirectional ceramic matrix composites was presented in this paper using micromechanical approach.The shear lag model was used to obtain the micro stress field of the damaged composites.The statistical matrix cracking model and fracture mechanics interface debonding criterion were used to determine matrix crack spacing and interface debonding length.After the saturation of matrix cracking,the fiber failure probabilities and fracture locations during tensile loading were determined by fiber statistical failure model based on the assumption that fiber strength is subject to Weibull distribution,and the loads carried by the broken and intact fibers meet the global load shearing criterion.The composites can no longer support the applied load when the total force supported by broken and intact fibers reaches its maximum.The effects of matrix Weibull modulus and characteristic strength,fiber/matrix interface shear stress and interface debonding energy,fiber Weibull modulus and characteristic strength on fiber failure and the tensile strength of ceramic matrix composites were discussed.The predicted results agree well with experimental data,proving the efficiency of the present model.
Keywords:ceramic matrix composites  matrix cracking  interface de-bonding  fiber failure  tensile strength
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