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双燃烧室冲压发动机为动力的高超声速飞行器 被引量：8

Hypersonic Vehicle with Dual-Combustor Ramjet
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摘要 介绍了双燃烧室冲压发动机的研究进展及特点,并较详细地论述了以双燃烧室冲压发动机为动力的高超声速飞行器的主要技术,对其机理研究和工程应用有一定的参考价值。 Development and characteristics of dual-combustor ramjet （DCR） are introduced. Some techniques valuable for the study of mechanism and engineering application of hypersonic vehicle with dual combustor ramjet are discussed in detail.
作者 于江飞 晏至辉 刘卫东
机构地区 国防科学技术大学
出处 《导弹与航天运载技术》 北大核心 2008年第5期26-30,共5页 Missiles and Space Vehicles
关键词 冲压发动机 双燃烧室 高超声速飞行器 Ramjet Dual-combustor Hypersonic vehicle
分类号 V43 [航空宇航科学与技术—航空宇航推进理论与工程]
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参考文献24

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二级参考文献33

共引文献69

同被引文献58

  • 1谭慧俊,郭荣伟.高超声速混合模块冲压发动机亚燃模块进气道的高焓风洞试验研究[J].航空学报,2007,28(4):783-790. 被引量：15
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导弹与航天运载技术
2008年 第5期

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