摘要
讨论弹用涡喷发动机启动加速过程的试验研究 ,并分析了某弹用涡喷发动机启动加速过程的有关问题 ,通过地面模拟试验建立了该发动机启动加速的数值模型。
The process of starting and accelerating the missile turbojet engine was discussed.Some problems of the turbojet engine in starting and accelerating were analysed in details and the numerical models for the process were built based on the tests that simulated the missile flight condition.
出处
《推进技术》
EI
CAS
CSCD
北大核心
2000年第4期5-8,共4页
Journal of Propulsion Technology
