| Citation: | LUO Guo-liang, SONG Shuang-wen, HU Hao-sheng, PENG Jian-yong. Influences of the swirl cup flares design on the small combustor ignition performances[J]. Journal of Aerospace Power, 2011, 26(8): 1708-1712. |
| [1] |
Sampath P,Verhiel J,McCaldon K.Low emissions technology for small aviation gas turbines.AIAA 2003-2564,2003.
|
| [2] |
彭云晖,林宇震,许全宏,等.双旋流空气雾化喷嘴喷雾、流动和燃烧性能[J].航空学报,2008,29(1):1-14. PENG Yunhui,LIN Yuzhen,XU Quanhong,et al.Review of atomization,aerodynamics and combustion performance of swirl cup[J].Acta Aeronautica et Astronaution Sinica,2008,29(1):1-14.(in Chinese)
|
| [3] |
方昌德.世界航空发动机手册[M].北京:航空工业出版社,1996.
|
| [4] |
Wang H Y,McDonell V G,Samuelsen G S.Influence of hardware design on the flow field structures and the patterns of droplet dispersion Part Ⅰ:mean quantities[J].Journal of Engineering for Gas Turbines and Power,1995,117(2):282-289.
|
| [5] |
Lang H J,Huang Y,Guo Z H.The flow fields in a model combustor with primary holes after different swirl cups.ASME GT2006-90489,2006.
|
| [6] |
Mongia H C,AI-Roub M,Danis A,et al.Swirl cup modeling Part Ⅰ.AIAA-2001-3576,2001.
|
| [7] |
Ateshkadi A,McDonell V G,Samuelsen G S.Effect of mixer geometry on fuel spray distribution,emissions and stability.AIAA 98-0247,1998.
|
| [8] |
徐华胜,黄义勇,王秀兰.喷嘴供油特性对双涡流器头部气动雾化效果的影响研究[J].燃气涡轮试验与研究,2004,17(2):14-17. XU Huasheng,HUANG Yiyong,WANG Xiulan.Study on the effect of fuel jet characteristics on airblast atomization performance for device with two stage swirler[J].Gas Turbine Experiment and Research,2004,17(2):14-17.(in Chinese)
|
| [9] |
Mongia H C,Gore J P,Grinstein F F,et al.Combustion research needs for helping development of next generation advanced combustors.AIAA 2001-3853,2001.
|
| [10] |
袁怡祥,林宇震,刘高恩,等.燃油周向分级对贫油熄火油气比的影响[J].航空动力学报,2003,18(5):639-644. YUAN Yixiang,LIN Yuzhen,LIU Gaoen,et al.The effect of fuel-circumferential staging on lean blowout limit at idle condition[J].Journal of Aerospace Power,2003,18(5):639-644.(in Chinese)
|
| [11] |
林宇震,林培华,许全宏,等.套筒空气雾化喷嘴燃烧室点火研究[J].航空动力学报,2007,22(3):342-346. LIN Yuzhen,LIN Peihua,XU Quanhong,et al.Research on ignition performance of a hybrid airblast atomizer combustor with convergent-divergent sleeve[J].Journal of Aerospace Power,2007,22(3):342-346.(in Chinese)
|
| [12] |
Lefebvre A H.Gas turbine combustion[M].Phiadelphia,PA,USA:Taylor & Francis Press,1999.
|