摘要
研究了基于网格理论的纤维缠绕壳体结构可靠性数字仿真方法及程序。以乘同余法产生伪随机数用于仿真计算，并对所产生的伪随机数进行了检验，对某发动机纤维缠绕壳体进行了结构可靠性数字仿真计算，得出了其结构可靠性。
The digital simulation for structural reliability of the filament - wound case is studied based on the grids theory. The pscudorandom numbers for simulation computer generated by the method of multiplying coremainder are inspected. A filament-wound case of SRM is simulated and its structural reliability is obtained.
出处
《固体火箭技术》
EI
CAS
CSCD
1996年第1期12-17,共6页
Journal of Solid Rocket Technology
关键词
固体推进剂
火箭发动机
仿真
缠绕结构
壳体
Solid propellant rocket engine Reliability simulation Filament wound structure Rocket engine case Grids method
