| S形进气道与小涡喷发动机在高空台的匹配试验研究 |
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| 引用本文： | 朱青,周仁德.S形进气道与小涡喷发动机在高空台的匹配试验研究[J].宇航学报,1993,14(2):55-60. |
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| 作者姓名： | 朱青 周仁德 |
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| 作者单位： | 北京动力机械研究所,北京动力机械研究所 北京 100074,北京 100074 |
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| 摘 要： |
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| 关 键 词： | 涡喷发动机 跨音速 进气道 |
EXPERIMENTAL INVESTIGATION OF COMPATIBILITY OF S-SHAPED INLET AND SMALL TURBOJET ENGINE IN THE SIMULATED ALTITUDE CHEMBER |
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| Zhu Qing Zhou Ren De.EXPERIMENTAL INVESTIGATION OF COMPATIBILITY OF S-SHAPED INLET AND SMALL TURBOJET ENGINE IN THE SIMULATED ALTITUDE CHEMBER[J].Journal of Astronautics,1993,14(2):55-60. |
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| Authors: | Zhu Qing Zhou Ren De |
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| Abstract: | The present paper describes the first testing conditions of compatibility of S- shaped inlet and small turbojet engine which is main power plant of a missile in the simulated altitude chamber. This paper describes measuring and testing technology and data processing methods for the flow parameters at jet exit of inlet. Meanwhile, the emphasis is placed on providing for testing results of inlet/engine compatibility. This testing proves that speific property of gas dynamics for S-shaped inlet of "HfwM2-1 D" is good. It will be satisfied with requesting for small trubojet engine of a missile in various flying conditions. |
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| Keywords: | Turbojet Engine Subsonic inlet Transonic inlet Testting equipment Measuring technology |
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