摘要
本文根据复合材料结构可靠性分析的特点提出复合材料结构的基本元件层压板的可靠性分析的方法。在此基础上将常规的优化设计发展为在可靠性基础上的优化设计并提出在板层压可靠性基础上铺层优化设计的方法。最后提出复合材料结构系统可靠性分析方法和确认主要破坏模式的方法。
The laminate is a basic component of the Compositc structures. In this paper a method of reliability analysis of the laminate is presented. In the method the characteristics of composite structure are considered. A method of optimum design based on the reliability developed from general method of optimum design is suggested. Furthermore, the method of reliability analysis using to composite structural system is discussed.
出处
《宇航学报》
EI
CAS
CSCD
北大核心
1989年第3期96-100,95,共6页
Journal of Astronautics
关键词
复合材料
结构
可靠性
Composite material, Laminate, Structural reliability, Reliability analysis and design,
