摘要
应用商业有限元软件ABAQUS中的内聚单元,对复合材料T型接头的缘条/蒙皮界面失效进行分析,计算结果与试验数据吻合良好。基于有限元结果,提取缘条/蒙皮界面内力,研究结构的失效机理。以缘条和蒙皮厚度为参数进行参数化建模,研究缘条/蒙皮刚度比对界面失效乃至承载能力的影响。最后对缘条/蒙皮刚度比提出设计建议。
The failure of flange/skin interface of T-Joint was simulated by using the cohesive element in the com- mercial software ABAQUS, and the simulations agree well with experimental data. The internal forces on the flange/skin interface were extracted from FEM results, and then their failure mechanism was studied. The flange and skin thickness was considered as parameters to build a parameterized model for studying the effect of stiffness ratios of the flange and the skin on the interface debonding. Finally the design parameters of the stiffness ratio between the flange and the skin were suggested for the design.
出处
《民用飞机设计与研究》
2012年第B11期94-98,共5页
Civil Aircraft Design & Research
关键词
复合材料
T型接头
内聚单元
失效机理
刚度比
Composite
T-Joint
Cohesive for the design. Element
Failure Mechanism
Stiffness Ratio