摘要 : Results of numerical simulation and principles of designing a mixer in the secondary zone of the flame tube when adjusting the rich-lean combustion chamber emission in the gas turbine engines are presented.
| 作者 | A. A. Inozemtsev V. G. Avgustinovich V. V. Tsatiashvili |
|---|---|
| 作者单位 | |
| 期刊名称 | 《Russian Aeronautics 》 |
| 总页数 | 7 |
| 语种/中图分类号 | 英语 / V2 |
| 关键词 | Gas turbine engine Combustion chamber Nitric oxide Diffusion combustion Flame front Mixer of the secondary zone Flame tube |
| 馆藏号 | N2008EPST0005607 |
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