摘要
In order to investigate the performance of the hydrogen-rich/oxygen-rich gas-gas injector in the full flow staged combustion (FFSC) engine, the combustion flow fields of the combustors with a shear coaxial injector, a coaxial injector for the oxidizer injector with expansion angle, a coaxial injector for the fuel injector with contraction angle, a coaxial injector for the oxidizer injector with a column in the center and a shear dual-coaxial injector were simulated. The propellant of the injectors was hydrogen-rich gas in temperature of 758K and oxygen-rich gas in temperature of 676K. The results of the numerical simulation show that, the shear dual-coaxial injector has the best combustion performance. The results can provide the reliable criterion for the design and experiment of hydrogen-rich/oxygen-rich gas-gas injector.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 835-840 |
| 页数 | 6 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 25 |
| 期 | 4 |
| 出版状态 | 已出版 - 4月 2010 |
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