Effects of airflow split and primary holes arrangement on lean blowout limits of combustor with dual-axial swirlers

[1] Bahr D W．Technology for the design of high temperature rise combustors ．AIAA-85-1292,1985 [2] Lefebvre A H.Gas turbine combustion[M]．New York:McGraw-Hill,1983 [3] 袁怡祥,林宇震,刘高恩．旋流杯燃烧室头部流场与喷雾对贫油熄火的影响[J]．航空动力学报,2004,19(3):332-337 Yuan Yixiang,Lin Yuzhen,Liu Gaoen．The effect of flow field and fuel spray of combustor with swirl cup on lean blowout limit at idle condition[J]．Journal of Aerospace Power,2004,19(3):332-337(in Chinese) [4] Mellor A M．Design of modern turbine combustors[M].London:Academic Press,1990 [5] Ballal D R,Lefebvre A H．Weak extinction limits of turbulent flowing mixtures[J]．Journal of Engineering for Power,1979,101:343-348 [6] Ballal D R,Lefebvre A H．Weak extinction limits of turbulent heterogeneous fuel/air mixtures[J]．Journal of Engineering for Power,1980,102:416-421 [7] Lefebvre A H．Fuel effects on gas turbine combustion-ignition,stability,and combustion efficiency[J]．Transactions of the ASME,Journal of Engineering for Gas Turbines and Power,1985,107(1):24-37 [8] Ballal D R．Combustor stability & lean blowout ．AIAA-2004-3526,2004 [9] 徐浩鹏,王方,黄勇,等．头部气量分配对旋流杯结构燃烧室贫熄性能的影响[J]．航空动力学报,2009,24(2):347-352 Xu Haopeng,Wang Fang,Huang Yong,et al．Effects of flow split among swirlers and primary holes on the lean blow-off limits of a combustor with swirl cup[J]．Journal of Aerospace Power,2009,24(2):347-352(in Chinese) [10] 邓甜．多点喷射燃烧室数值模拟研究 .北京:北京航空航天大学能源与动力工程学院,2007 Deng Tian．Numerical simulation of multi-injection combustors ．Beijing: School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,2007(in Chinese) [11] Xie Fa,Huang Yong,Wang Fa,et al．Visualization of the lean blowout process in a model combustor with a swirl cup .ASME-GT-2010-22534,2010 [12] Rizk N K,Mongia H C．Three-dimensional analysis of gas turbine combustors[J]．Journal of Propulsion,1991,7(3): 445-451 [13] Rizk N K,Mongia H C．Three-dimensional combustor performance validation with high-density fuels[J]．Journal of Propulsion,1991,6(5):660-667 [14] Mongia H C,Reynolds S R,Srinivasan R．Multidimensional gas turbine combustion modeling: applications and limitations [J]．AIAA Journal,1986,24(6):890-904 [15] Rizk N K,Mongia H C．Gas turbine combustor design methodology ．AIAA-86-1531,1986 [16] Mongia H C．A synopsis of gas turbine combustor design methodology evolution of last 25 years ．ISABE-2001-1086,2001 [17] Mongia H C．Perspective of combustion modeling for gas turbine combustors ．AIAA-2004-156,2004 [18] Mongia H C．Recent progress in comprehensive modeling of gas turbine combustion ．AIAA-2008-1445,2008 [19] Ateshkadi A,McDonell V G,Samuelsen G S．Lean blowout model for a spray-fired swirl-stabilized combustor//Proceedings of the Combustion Institute,2000:1281-1288 [20] Ateshkadi A．The effect of fuel/air mixer design parameters on the continuous and discrete phase structure in the reaction-stabilizing region ．USA: Mechanical and Aerospace Engineering,University of California,Irvine,2000 [21] Mongia H C,Vermeersch M,Thomsen D D,et al．A simple reactor based approach for correlating lean blowout of turbo-propulsion engine combustors ．AIAA-2001-3240,2001 [22] Mongia H C,Michael L,Vermeersch M,et al．Data reduction and analysis (DRA) for emissions and lean blowout ．AIAA-2003-0823,2003 [23] 徐浩鹏．旋流杯结构燃烧室下游流场特性及贫油熄火特性研究 ．北京:北京航空航天大学能源与动力工程学院,2007 Xu Haopeng.A research of the downstream flowfields and lean blowout limits of combustors with swirl cups .Beijing: School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,2007(in Chinese) [24] 党新宪,赵坚行,吉洪湖．试验研究双旋流器头部燃烧室几何参数对燃烧性能影响[J]．航空动力学报,2007,22(10):1639-1645 Dang Xinxian,Zhao Jianxing,Ji Honghu．Experimental study of effects of geometric parameters on combustion performance of dual-stage swirler combustor[J]．Journal of Aerospace Power,2007,22(10):1639-1645(in Chinese) [25] 张玉芳．燃烧室贫油熄火性能研究 ．北京:北京航空航天大学能源与动力工程学院,2007 Zhang Yufang．A research of the lean blowout limits of combustors ．Beijing: School of Jet Propulsion,Bejing University of Aeronautics and Astronautics University,2007(in Chinese)