摘要
采用混合同余法与变换抽样法对固体火箭发动机纤维缠绕燃烧室压强的多种随机分布进行了模拟,并结合蒙特卡罗随机有限元方法分析了该结构在正态分布压强作用下的力学响应。其结果可用于此类结构的可靠性评估与设计。
Several stochastic distributions of chamber pressure have been simulated by mixed congruence method and conversion sampling method. SRM chamber structure mechanics response under the action of normal distribution chamber pressure has been analyzed by used of Monte Carlo stochastic finite element method.The simulation result can be used in the evalution and design of SRM structure reliability.
出处
《固体火箭技术》
EI
CAS
CSCD
1998年第1期20-25,共6页
Journal of Solid Rocket Technology
关键词
固体火箭发动机
燃烧室
压强
正态分布
有限元
Rocket combustion chamber Normal distribution Simulation Monto Carlo method Finite element method