摘要
介绍了玻璃基复合材料的特点,根据 McCartney 模型编制了一套计算程序以选择合适的基体。利用该程序可以计算各种条件下复合材料内的应力分布、应力分配系数。最后探讨了玻璃基复合材料基体对力学与损伤行为的影响。
The characteristics of glass matrix composite are introduced. A piece of computer program is devel- oped based on the MeCartney model for the selection of matrix, which can be used to calculate the stress distribution in the composite and the coefficient of the stress distribution in the fiber and in the matrix. The mechanical behavior as well as damage behavior of glass matrix composite are also investigated in the paper.
出处
《航空工艺技术》
1997年第2期3-6,共4页
Aeronautical Manufacturing Technology
关键词
玻璃基
复合材料
应力分配系数
损伤行为
Glass matrix composite
Fiber
Expansion coefficient
Stress distribution coefficient