| Citation: | Numerical simulation and experiment of triple swirler combustor[J]. Journal of Aerospace Power, 2017, 32(11): 2568-2575. doi: 10.13224/j.cnki.jasp.2017.11.002
|
| [1] |
BAHR D W.Technology for the design of high temperature rise combustors［R］.AIAA 85-1292,1985.
|
| [2] |
KRESS E J.Multiple swirler dome combustor for high temperature rise applications［R］.AIAA 90-2159,1990.
|
| [3] |
LI Guoqiang,GUTMARK E J.Flow field measurements of triple swirler spray combustor［R］.AIAA-2002-4010,2002.
|
| [4] |
LI Gouqiang,ANGIER S,LAMBOLEZ O,et al.Experimental study of velocity flow field for a multiple swirl spray combustor［R］.AIAA-2002-0618,2002.
|
| [5] |
GRINSTEIN F F,YONG T R,MONGIA H C.Computational and experimental analysis of the flow dynamics in a mutiswirler combustor ［R］.AIAA-2002-1006,2002.
|
| [6] |
MANSOUR A,BENJAMIIN M.A new hybrid air blast nozzle for advanced gas turbine combustor［R］.ASME Paper 2000-GT-0117,2000.
|
| [7] |
吴振宇,王成军,王丹丹.三级旋流器的设计及其流场模拟［J］.沈阳航空工业学院学报,2010,27(5):38-41.WU Zhenyu,WANG Chengjun,WANG Dandan.Triple swirler design and fluid numerical simulation［J］.Journal of Shenyang Institute of Aeronautical Engineering,2010,27(5):38-41.(in Chinese)
|
| [8] |
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):332-336.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):332-336.(in Chinese)
|
| [9] |
彭云晖,林宇震,刘高恩.三旋流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)
|
| [10] |
王纯,刘艳梅,周涛,等.基于ICEM CFD对汽轮机末级三维叶片流场网格划分方法的优化［J］.汽轮机技术,2012,54(5):324-326.WANG Chun,LIU Yanmei,ZHOU Tao,et al.Optimization of mesh generation of steam turbine last stage 3D blade field based on ICEM CFD［J］.Turbine Technology,2012,54(5):324-326.(in Chinese)
|
| [11] |
陶文铨.数值传热学［M］.西安:西安交通大学出版社,2011.
|
| [12] |
刘厚林,刘明明,董亮,等.网格类型对离心泵数值计算精度的影响［J］.华中科技大学学报(自然科学版),2013,41(10):64-73.LIU Houlin,LIU Mingming,DONG Liang,et al.Effects of types of grids on numerically calculating accuracy of centrifugal pumps［J］.Journal of Huazhong University of Science and Technology (Natural Science Edition),2013,41(10):64-73.(in Chinese)
|
| [13] |
纪兵兵,陈金瓶.ANSYS ICEM CFD网格划分技术实例详解［M］.北京:中国水利水电出版社,2012.
|
| [14] |
FLUENT Incorporation FLUENT 63 users guide［M］.New Hampshire,UK:Fluent Incorporation,2006:1-96.
|
| [15] |
金戈,张志学,顾铭企.QD128航改燃气轮机燃烧室数值模拟［J］.航空发动机,2008,34(2):30-35.JIN Ge,ZHANG Zhixue,GU Mingqi.Numerical simulation of QD128 aeroderivative gas turbine combustor［J］.Aeroengine,2008,34(2):300-35.(in Chinese)
|
| [16] |
蒲宁.航空发动机燃烧室数值仿真中湍流模型的比较研究［D］.沈阳:沈阳航空工业学院,2009.PU Ning.Comparison of turbulent models for aeroengine combustor numerical simulation［D］.Shenyang:Shenyang Institute of Aeronautical Engineering,2009.(in Chinese)
|
| [17] |
吴超.湍流燃烧模型在燃烧室数值计算中的应用研究［D］.沈阳:沈阳航空工业学院,2009.WU Chao.Study on applicability of turbulent combustion model in the numerical calculation of combustor［D］.Shenyang:Shenyang Institute of Aeronautical Engineering,2009.(in Chinese)
|
| [18] |
金如山.航空燃气轮机燃烧室［M］.北京:宇航出版社.1985.
|
| [19] |
莫妲,程明,张成凯,等.三旋流器加装外套环对燃烧性能的影响［J］.航空动力学报,2016,31(7):1569-1574.MO Da,CHENG Ming,ZHANG Chengkai,et al.Effect of triple swirler with an outer ring on combustion performance［J］.Journal of Aerospace Power,2016,31(7):1569-1574.(in Chinese)
|
| [20] |
《航空发动机设计手册》总编委会.航空发动机设计手册:第9册 主燃烧室［M］.北京:航空工业出版社,2000.
|
| [21] |
李亚娟,王明瑞,葛新,等.基于燃气分析法的航空发动机燃烧室性能研究［J］.航空发动机,2016,42(1):37-41.LI Yajuan,WANG Mingrui,GE Xin,et al.Research on aeroengine combustor performance based on gas analysis method［J］.Aeroengine,2016,42(1):37-41.(in Chinese)
|
DownLoad: