| Citation: | ZHANG Zhen-kui, ZHONG Hua-gui, FENG Da-qiang, WANG Fang-ping. Experimental study on outlet temperature field in multipoint injection combustor-sector[J]. Journal of Aerospace Power, 2011, 26(12): 2661-2666. |
| [1] |
Koutsenko I G,Onegin S F, Sipatov A M.Application of CFD-based analysis technique for design and optimization of gas turbine combustors[R]. ASME Paper GT2004-53398,2004.
|
| [2] |
Tacina R,Wey C,Laing P,et al.Sector tests of a low NOx lean direct injection multipoint integrated module combustor concept[R].ASME Paper GT2002-30089,2002.
|
| [3] |
Tacina R,Wey C.A low NOx lean-direct injection,multipoint integrated module combustor concept for advanced aircraft gas turbines[R].NASA//TM-2002-211347,2002.
|
| [4] |
Cai J,Jeng S M,Tacina R.Mult-swirler aerodynamics:comparison of different configuration[R].ASME Paper GT2002-30466,2002.
|
| [5] |
Iannetti A,Tacina R,Jeng S M,et al.Towards accurate prediction of turbulent,three-dimensional,recirculating flows with the NCC[R].AIAA-2001-0809,2001.
|
| [6] |
Applenton J P,Heywood J B.The effects of imperfect fuel-air mixing in a burner on NO formation from nitrogen in the air and fuel l[C]//The 14th Symposium (International) on Combustion.Pennsylvania State University,PA USA: Elsevier,1973:777-786.
|
| [7] |
Iannetti A,Tacina R,Jeng S M,et al.Mult-swirler aerodynamics:CFD predictions[R]. AIAA Paper 2001-3575,2001.
|
| [8] |
Cai J,Jeng S M,Tacina R.Mult-swirler aerrodynamics:experiment measurements[R]. AIAA Paper 2001-3754,2001.
|
| [9] |
Yang S L,Siow Y K,Tacina R R,et al.Numerical simulation of LDI combustor with discrete-jet swirlers using Re stress model in the KIVE code[R].Detrit,USA:Tenth Internation Multidimensional Engine Modeling User''s Group Meeting,2000.
|
| [10] |
张群,徐华胜,钟华贵,等.多旋流器阵列贫油直喷燃烧室 流场的数值模拟[J].航空动力学报,2009,24(3):484-487. ZHANG Qun,XU Huasheng,ZHONG Huagui,et al.Numerical simulation of flow field in a multi-swirler array lean direct injection combustor[J].Journal of Aerospace Power,2009,24(3):483-487.(in Chinese)
|
| [11] |
Lefebvre A H.Gas turbine combustion[M].Washington DC USA:Taylor & Francis,1998.
|
| [12] |
刘凯,张宝成,蔡九菊,等.某重型燃气轮机燃烧室出口温度场试验[J].航空动力学报,2010,25(1):23-27. LIU Kai,ZHANG Baocheng,CAI Jiuju,et al.Experiment study on outlet temperature field for combustor of heavy-duty gas turbine[J].Journal of Aerospace Power,2010,25(1):23-27.(in Chinese)
|
| [13] |
彭云辉,林宇震,刘高恩.三旋流器燃烧器燃烧室出口温度分布的初步试验研究[J].航空动力学报,2007,22(4):554-558. PENG Yunhui,LIN Yuzhen,LIU Gaoen.A preliminary experimental study of pattern factor for a triple swirler combustor[J].Journal of Aerospace Power,2007,22(4):554-558.(in Chinese)
|
| [14] |
钟华贵,吉洪湖,李继保.燃气分析测量高温燃气温度的方法[J].航空动力学报,2005,20(3):460-466. ZHONG Huagui,JI Honghu,LI Jibao.Methods for gas temperature measure by gas analysis[J].Journal of Aerospace Power,2005,20(3):460-466.(in Chinese)
|