| 中国超燃冲压发动机研究回顾 |
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| 引用本文： | 刘兴洲.中国超燃冲压发动机研究回顾[J].推进技术,2008,29(4):385-395. |
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| 作者姓名： | 刘兴洲 |
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| 作者单位： | 北京动力机械研究所 |
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| 摘 要： | 回顾了中国近年来在超燃冲压发动机领域的研究进展。首先是高超声速进气道的研究进展,包括高超声速进气道中激波与附面层干扰、起动和再起动、隔离段、进气道附面层抽吸、进气道通道内外压缩比、侧压式进气道、Busemann进气道等。其次是超声速燃烧方面的研究及模型超燃冲压发动机研究。最后对研究工作进行了评述。
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| 关 键 词： | 超燃冲压发动机 高超声速进气道 超声速燃烧 超燃冲压发动机试验 |
Review of scramjet research in China |
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| LIU Xing-zhou.Review of scramjet research in China[J].Journal of Propulsion Technology,2008,29(4):385-395. |
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| Authors: | LIU Xing-zhou |
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| Institution: | LIU Xing-zhou(Beijing Power Machinery Research Inst.,Beijing 100074,China) |
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| Abstract: | The scramjet research in China in recent years is reviewed.Firstly,studies for hypersonic inlets are reviewed,including issues related to interaction between boundary and shock wave in hypersonic inlet,unstarting/ restarting phenomena,isolator,boundary bleeding for hypersonic inlet,internal/external compression ratio for inlet,inlets with sidewall compression,etc..Secondly,supersonic combustion research is reviewed.Then,investigation for scramjet engine model is summarized.Finally,some comments on the research works are given. |
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| Keywords: | Scramjet Hypersonic inlet Supersonic combustion Scramjet test |
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