跳到主要导航 跳到搜索 跳到主要内容

Comparison of combustion characteristics for GO2/CH4 and GH2/GO2 injectors

  • Beihang University
  • Xi’an Aerospace Propulsion Institute

科研成果: 期刊稿件文章同行评审

摘要

In order to obtain the differences and connections of the GO2/CH4 and GH2/GO2 combustion characteristics, to provide experience of the GH2/GO2 injector for guiding GO2/CH4 injector design, comparison of GO2/CH4 and GH2/GO2 combustion characteristics for shear-coaxial injectors was conducted in the same combustion chamber by numerical simulation and experiment. The results show that under the similar design parameters, the size of GO2/CH4 injector is almost equal to that of GH2/GO2 injector. On condition that the pressure at design point and dimensions are the same, in order to produce the same thrust, the mass flow rate of GO2/CH4 (mixture ratio 3.5) is about 1.27 times as GH2/GO2 (mixture ratio 6.0). Furthermore, combustion characteristic length of GO2/CH4 is approximately 1.48 times as much as GH2/GO2 combustion chamber, and the thermal load of the GO2/CH4 combustion chamber is about half of the GH2/GO2 combustion chamber.

源语言英语
页(从-至)775-780
页数6
期刊Tuijin Jishu/Journal of Propulsion Technology
34
6
出版状态已出版 - 6月 2013

指纹

探究 'Comparison of combustion characteristics for GO2/CH4 and GH2/GO2 injectors' 的科研主题。它们共同构成独一无二的指纹。

引用此