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全流量补燃循环气气燃烧相似性缩尺试验研究

  • Yu Shan Gao*
  • , Xiao Yong Liu
  • , Ping Jin
  • *此作品的通讯作者
  • Xi'an Aerospace Propulsion Institute

科研成果: 期刊稿件文章同行评审

摘要

In order to guide the design of chamber injector for full-flow stage combustion engine, reduced-scale test of gas-gas combustion similarity in a chamber with quartz windows was conducted utilizing gaseous oxygen and gaseous hydrogen as propellants. The high-speed camera was used to obtain the combustion flame structure near the exit of the coaxial injector under the stable combustion and unstable combustion, and the frequency characteristics of unstable combustion were analyzed. The results show that, with the types of propellant, propellant temperature, propellant mixing ratio, combustion chamber and nozzle structure size unchanged, by increasing propellant flow rate, the stable and unstable combustion flame structure is similar to some extent, and the frequency of unstable combustion is the same.

投稿的翻译标题Reduced-Scale Test of Gas-Gas Combustion Similarity in Full-Flow Stage Combustion Engine
源语言繁体中文
页(从-至)1554-1559
页数6
期刊Tuijin Jishu/Journal of Propulsion Technology
40
7
DOI
出版状态已出版 - 1 7月 2019

关键词

  • Full flow stage combustion cycle engine
  • Gas-gas combustion
  • Injector
  • Reduced-scale
  • Similarity

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