推进技术 ›› 2000, Vol. 21 ›› Issue (4): 5-8.
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郑严
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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。
关键词: 涡轮喷气发动机;起动试验;发动机试验;地面试验
Abstract: 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.
Key words: Turbojet engine;Starting test;Engine test;Ground test
郑严. 弹用涡喷发动机启动加速过程试验[J]. 推进技术, 2000, 21(4): 5-8.
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