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 |
| 卷 | 34 |
| 期 | 6 |
| 出版状态 | 已出版 - 6月 2013 |
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