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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。
According to the research and test results of aero-to-air missile engine, the Monte-Carlo method was used for computer simulation. Then the reliability of engine structure was evaluated by stress-strength interference theory. The results show that the simulation results are consistent with the actual results and reliable Sexual assessment results are reasonable and effective.