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气氢亚燃冲压发动机燃烧室氢和空气增混技术及稳焰方案 被引量:1

H_2/AIR MIXING ENHANCEMENT AND FLAME STABILIZING SCHEMES IN GASEOUS HYDROGEN SUBSONIC COMBUSTOR OF RAMJET
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摘要 定性分析了设计气氢亚燃冲压发动机燃烧室所遇到的两个问题:氢和空气扩散火焰的混合增强和稳焰技术,综合了可用于氢和空气扩散火焰的几种混合增强方案和稳焰方案。 Two problems encountered in design of gaseous hydrogen subsonic combustion of ramjet were analysed which were mixing enhancement and flame stabilizing of H2/air.Several schemes to enhance mixing and stabilize flame was described in this paper.
机构地区 航天工业总公司
出处 《推进技术》 EI CAS CSCD 北大核心 1996年第3期6-9,共4页 Journal of Propulsion Technology
关键词 冲压发动机 燃烧室 氢燃料 稳定燃烧 Ramjet engine,Combustor,Hydrogen fuel,Subsonic combustion,Mixing,Stable combustion
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  • 1王卫东,推进技术,1996年,17卷,2期 被引量:1

同被引文献6

  • 1TROY A GIESE.Experimental investigation of the influence of molecular weight on mixing and penetration in supersonic dissimilar gaseous injection into a supersonic cross-flow[D].Air Force Institute of Technology,1997. 被引量:1
  • 2SCHETZ J A.Injection and mixing in turbulent flow[J].Progress in Astronautics and Aeronautics,1980,68:145-164. 被引量:1
  • 3MCDANIEL J C,GRAVES JR J.A laser-induced-fluorescence visualization study of transverse,sonic fuel injection in a nonreacting supersonic combustor[R].AIAA Paper86-0507. 被引量:1
  • 4WANG T S.Thermo-kinetics characterization of kerosene/RP-1 combustion[R].AIAA Paper96-2887. 被引量:1
  • 5WESTBROOK C K,DRYER F L.Simplified reaction mechanisms for the oxidation of hydrocarbon fuels in flames[J].Combustion Science and Technology.1981.(27):31-43. 被引量:1
  • 6梁剑寒,王正华,王承尧.超燃发动机垂直燃料喷射的数值研究[J].推进技术,2000,21(1):12-14. 被引量:4

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