| Citation: | Effect of nozzle damage on performance of annular backflow combustor[J]. Journal of Aerospace Power, 2017, 32(6): 1335-1341. doi: 10.13224/j.cnki.jasp.2017.06.008
|
| [1] |
姚四伟， 张力先，李建军.某型发动机涡轮叶片烧蚀故障分析与预防［J］.失效分析与预防,2006,1(4):27-29.YAO Siwei,ZHANG Lixian,LI Jianjun.Analysis and prevention for ablation failure of turbine blade in aeroengine［J］.Failure Analysis and Prevention,2006,1(4):27-29.(in Chinese)
|
| [2] |
周茂军.考虑性能衰退的航空发动机总体性能裕度设计研究［J］.航空动力学报,2008,23(10):1868-1874.ZHOU Maojun.Research on aeroengine performance ma-rgin design considering performance deteroration in utility［J］.Journal of Aerospace Power,2008,23(10):1868-1874.(in Chinese)
|
| [3] |
CORPORAN E,MINUS D K,WILLIAMS T F.Studies of decal in as a suppressor of pyrolytic deposits in JP-8+100［R］.AIAA 99-2213,1999.
|
| [4] |
李范,朱岳麟,黄艳斐,等.发动机喷嘴表面化学改性抗结焦积碳［J］.北京航空航天大学学报,2014,40(4):564-568.LI Fan，ZHU Yuelin，HUANG Yanfei，et al.Anti-coking performance of nozzle materials surface chemical modification［J］.Journal of Beijing University of Aeronautics and Astronautics,2014,40(4):564-568.(in Chinese)
|
| [5] |
黄艳斐,朱岳麟,熊常健,等.航空发动机喷嘴结焦积碳的性质［J］.北京航空航天大学学报,2011,37(6):753-756.HUANG Yanfei,ZHU Yuelin,XIONG Changjian,et al.Coking properties of aircraft enginesnozzle［J］.Journal of Beijing University of Aeronautics and Astronautics,2011,37(6):753-756.(in Chinese)
|
| [6] |
《高效节能发动机文集》编委会.高效节能发动机文集：第4分册 燃烧室设计与试验［M］.北京:航空工业出版社,1991.
|
| [7] |
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.Atomization,aerodynamics and combudtion performance of swirl cup［J］.Acta Aeronautica et Astronutica Sinica,2008,29 (1):1-14.(in Chinese)
|
| [8] |
裴毅强,陈皓,秦静,等.直喷汽油机喷嘴积碳对喷雾的影响［J］.天津大学学报(自然科学与工程技术版)，2015，48(4):334-340.PEI Yiqiang,CHEN Hao,QIN Jing,et al.Effect of GDI engine injector coking on spray［J］.Journal of Tianjin University (Science and Technology),2015,48(4):334-340.(in Chinese)
|
| [9] |
谈军华.喷嘴积碳对GDI汽油机喷雾特性影响的实验研究［D］.南宁：广西大学,2014.TAN Huajun.Experimental study of the influence of the GDI gasoline injection deposit on the spray characteristics［D］.Nanning:University of Guangxi,2014.(in Chinese)
|
| [10] |
甘晓华.航空燃气轮机燃油喷嘴技术［M］.北京:国防工业出版社,2006.
|
| [11] |
SHIH T H,LIOU W W，SHABBIR A,et al.A new k -ε eddy viscosity model for high Reynolds number turbulent flow ［J］.Computers and Fluids,1995,24(3):227-238.
|
| [12] |
YAKHOT V,ORSSSZAG S A,THANGAM S,et al.Development of turbulence model for shear flows by a double expansion technique［J］.Physics of Fluids A (Fluid Dynamics),1992,4(7):1510-1520.
|
| [13] |
PETERS N.Turbulent combustion［M］.London:Cambridge University Press,2000.
|
| [14] |
GUO Junjiang,HUA Xiaoxiao,WANG Fan,et al.System approach to automatic construction of high-temperture combustion mechnisms of alkanes［J］.Acta Physico-Chimica Sinica，2014,30(6):1027-1041.
|
| [15] |
王慧汝,金捷.采用不同航空煤油反应机理模拟模型燃烧室两相燃烧流场［J］.燃气涡轮试验与研究,2013,26(4):22-27.WANG Huiru,JIN Jie.Numerical simulation of two-phase combustion field in a model combustor using two different chemical reaction mechanisms of jet fuel［J］.Gas Turbine Experiment and Research,2013,26(4):22-27.(in Chinese)
|
| [16] |
王慧汝,金捷,刘大响.过渡工况下环形燃烧室热态三维数值［J］.航空动力学报,2010,25(2):316-319.WANG Huiru,JIN Jie,LIU Daxiang.Numerical simula-tion of three-dimension combustion in an annular com-bustor during a transient state［J］.Jounal of Aerospace Power,2010,25(2):316-319.(in Chinese)
|
| [17] |
《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.
|
| [18] |
黄勇.燃烧与燃烧室［M］.北京:北京航空航天大学出版社,2009.
|
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