摘要
根据某空-空导弹发动机的研制试验结果,用蒙特卡洛法进行了计算机模拟,然后再用应力-强度干涉理论进行了发动机结构可靠性评估,结果表明,模拟结果和实际结果相符,结构可靠性评估结果合理、有效。
Based on the firing test results of some air-to-air missile motor, its operation process is computer-simulated by the Monte-Carlo method, and then its structural reliability is evaluated based on the stress-intensity interference theory. The results show that the simulated results which agree well with the actual results exhibit the rational and effective structural reliability evaluation.
出处
《固体火箭技术》
EI
CAS
CSCD
1994年第4期30-34,共5页
Journal of Solid Rocket Technology
关键词
战术志弹
固体推进剂
火箭发动机
结构可靠性
Tactical missile Solid propellant rocket engine Structural reliability Monte-Carlo method Computerize simulation Stress-intensity factor