摘要
The turbulent Navier-Stokes equations in combination with two equation k-ε turbulence models were used to simulate the flow field of shear dual-coaxial single element GO2/GH2injector chamber. The results show that: the shear dual-coaxial injector has two shear combustion surfaces, enabling to achieve a high combustion efficiency at the condition of large mass flowrate, the oxygen injection velocity and the velocity ratio of hydrogen to oxygen are key parameters for shear dual-coaxial injector design, a lower oxygen injection velocity makes the combustion location far away from the faceplate, while a higher velocity ratio makes the combustion location closer to the faceplate. Compared with the gas-liquid shear coaxial injector, a faster oxygen injection velocity and proper velocity ratio of hydrogen to oxygen are preferable choice for design of shear dual-coaxial injector.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 829-834 |
| 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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