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界面层参数对陶瓷基复合材料单轴拉伸行为的影响
引用本文:孙志刚,李龙彪,朱彬,宋迎东.界面层参数对陶瓷基复合材料单轴拉伸行为的影响[J].航空动力学报,2010,25(3):597-602.
作者姓名:孙志刚  李龙彪  朱彬  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
基金项目:973计划;航空科学基金,南京航空航天大学校科研和教改项目,江苏省普通高校研究生创新基金,高等学校博士学科点专项科研基金 
摘    要:采用细观力学方法研究了界面层参数对陶瓷基复合材料单轴拉伸行为的影响.在剪滞模型基础上提出了考虑界面相与界面层效应的力学简化模型,结合临界基体应变能准则、最大剪应力准则、临界纤维应变能准则确定基体裂纹间距、界面脱黏长度和纤维失效百分数,对考虑界面层影响的陶瓷基复合材料拉伸应力-应变曲线进行了模拟,讨论了界面层体积分数、弹性模量及泊松比对拉伸行为的影响,并与试验结果进行了对比,发现考虑界面层及界面相的影响时,界面脱黏和纤维失效段应力-应变曲线与试验数据更接近,预测效果更好.

关 键 词:陶瓷基复合材料  界面层  基体开裂  界面脱黏  纤维失效  应力-应变曲线  剪滞模型
收稿时间:3/4/2009 12:00:00 AM
修稿时间:2009/9/30 0:00:00

Effect of interface layer parameters on uniaxial tensile behavior of ceramic matrix composites
SUN Zhi-gang,LI Long-biao,ZHU Bin and SONG Ying-dong.Effect of interface layer parameters on uniaxial tensile behavior of ceramic matrix composites[J].Journal of Aerospace Power,2010,25(3):597-602.
Authors:SUN Zhi-gang  LI Long-biao  ZHU Bin and SONG Ying-dong
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:The effect of interface layer parameters on the uniaxial tensile stress-strain behavior of ceramic matrix composites has been investigated using micro-mechanic approach.The simplified micro-mechanic model,which considered the effects of the interface layer on the mechanical properties of fiber reinforced ceramic composites,was proposed based on the classic shear-lag model.The critical matrix strain energy criterion,maximum interface shear stress criterion and the critical fiber strain energy criterion were used to determine the matrix crack space,interface debonding length and the fiber failure fraction.The stress-strain curve was modeled with consideration of the effects of interface layer.And the influences of interface layer volume fraction,elastic modulus and Poisson ratio on the stress-strain curve were also discussed.The stress-strain curve predicted by the present analysis with compared the experimental data,and it was found that the interface debonding and fiber failure part of the tensile stree-strain curve agree well with the experimental data on consideration of the effect of interface layer or interface phase.
Keywords:ceramic matrix composites  interface layer  matrix cracking  interface debonding  fiber failure  stress-strain curve  shear-lag model
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