| タイトル | Effects of nozzle lip geometry on spray atomization and emissions advanced gas turbine combustors |
| 著者（英） | Roychoudhury, Subir; Nguyen, H. L.; Micklow, Gerald J. |
| 著者所属（英） | NASA Lewis Research Center; Florida Univ. |
| 発行日 | 1991-06-01 |
| 言語 | eng |
| 内容記述 | A parametric study is conducted to investigate the effect of nozzle lip geometry on nozzle fuel distribution, emissions and temperature distribution for a rich burn section of a rich burn/quick quench/lean burn combustor. It is seen that the nozzle lip geometry greatly affects the fuel distribution, emissions and temperature distribution. It is determined that at an equivalence ratio of 1.6 the NO concentration could be lowered by a factor greater than three by changing the nozzle lip geometry. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 91A44153
AIAA PAPER 91-2201 |
| 権利 | Copyright |
