期刊文献+

射流预冷却涡轮基发动机的技术研究 被引量:6

Research on Techniques of Mass Injection and Precooling Engines
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摘要 射流预冷却涡轮基组合循环发动机(steamjet)是目前重点研究的一种高超音速飞行器用发动机。文中分析了射流预冷却涡轮基组合循环发动机的工作特点,与火箭发动机相比说明了其发展的优势,总结归纳了这种发动机技术特点和发展的关键技术,结合发动机研究实际分析了其发展的可能性。 The StesmJet is a new high Mach engine,which is based on existing turbojet developed in U.S.It is a precoo- ling turbine based combined cycle(PCTBCC)engines.This paper analyzed to stesmjet the work characteristics,ex- plained its development advantage compare with the rocket engine,the summary induced this kind of engine technique characteristics and the key technique of the development,joining together the our country aeroengine research actual a- nalysis the possibility of its development.
出处 《弹箭与制导学报》 CSCD 北大核心 2004年第S4期335-337,341,共4页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 涡轮基发动机 射流预冷却 高超音速 TBCC Mass injection and Precooling Hypersonic
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参考文献12

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同被引文献29

  • 1王占学,乔渭阳.预冷却涡轮基组合循环发动机发展现状及应用前景[J].燃气涡轮试验与研究,2005,18(1):53-56. 被引量:17
  • 2商旭升,蔡元虎,陈玉春,商旭红.高速飞行器用射流预冷却涡轮基发动机性能模拟[J].中国空间科学技术,2005,25(4):54-58. 被引量:15
  • 3商旭升,蔡元虎,肖洪.预冷却吸气式涡轮冲压膨胀循环发动机发展简介[J].兵工学报,2006,27(3):480-484. 被引量:4
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