| Citation: | HU Hao-sheng, ZHAO Jian-xing, ZHONG Jian-ping, JIANG Rong-wei, YIN Mei-zhi. A new adjustment method of combustor outlet temperature field[J]. Journal of Aerospace Power, 2007, 22(8): 1222-1226. |
| [1] |
Lefebvre A H.Gas turbine combusiion[M].Philadelphia:Taylor-Francis,1999.
|
| [2] |
Chen Y,Scarborough D,Liang S,et al.Manipulating pattern factor using synthetic jet actuators[R].AIAA 2000-1023,2000.
|
| [3] |
John C D,Kevin J B,Joseph R S,et al.Active combustion control for aircraft gas turbine engines[R].AIAA 2000-3500,2000.
|
| [4] |
郑严,沈倍毅.弹用涡喷发动机燃烧室出口温度场试验与分析[J].推进技术,2001,22(3):187-190.ZHENG Yan,SHEN Beiyi.Tests and analysis of exit temperature distribution of the combustor for missile turbojet[J].Journal of Propulsion Technology,2001,22 (3):187-190.
|