T300/QY8911单向板湿热性能模拟与损伤分析  

Hygrothermal properties simulation and damage analysis of T300/QY8911 undirectional laminates

作　　者：齐忠新[1] 燕瑛[1] 刘玉佳[1] 何明泽[1] 

机构地区：[1]北京航空航天大学航空科学与工程学院,北京100191

出　　处：《北京航空航天大学学报》2012年第7期947-952,共6页Journal of Beijing University of Aeronautics and Astronautics

基　　金：国家973计划资助项目(2011CB606105)

摘　　要：测试了不同湿热条件下T300/QY8911单向板的弯曲性能,建立了湿热条件下复合材料单向板的弯曲有限元模型,模拟了湿热条件下T300/QY8911单向板的弯曲性能,开发了复合材料损伤演化仿真模块,对湿热条件下T300/QY8911单向板弯曲损伤演化过程进行了仿真.结果表明:湿热条件下T300/QY8911单向板的弯曲模量具有较高的保持率,弯曲强度随湿热条件的变化差异较大,模量和强度的模拟结果与试验值的误差分别小于6%和2%,建立的弯曲有限元模型,能够比较准确地预测不同湿热条件下复合材料单向板的弯曲性能.Flexural properties of T300/QY8911 undirectional laminates were tested under different hygrothermal conditions.Finite element models of composite undirectional laminates under hygrothermal conditions were built.The flexural properties of T300/QY8911 undirectional laminates tested in experimentation were simulated.Plus,a damage evolution simulation module of composite was developed.The integrated damage evolution process of T300/QY8911 undirectional laminates under hygrothermal conditions was simulated.Results show that,the flexural modulus of T300/QY8911 undirectional laminates remains unchanged under different hygrothermal conditions,but the flexural strength changes greatly with conditions.For flexural modulus,the error between simulation values and test results is less than 6%,and for flexural strength,it is less than 2%.The finite element models can predict flexural properties of composite undirectional laminates under different hygrothermal conditions relative exactly.

关 键 词：单向板 湿热条件 弯曲性能 损伤演化 渐进失效 

分 类 号：V214.8[航空宇航科学与技术—航空宇航推进理论与工程]