| Citation: | Influence of inlet distortion of different ranges on subsonic axial-flow compressor[J]. Journal of Aerospace Power, 2018, 33(4): 776-784. doi: 10.13224/j.cnki.jasp.2018.04.002
|
| [1] |
WALKER C L,SIVO J N,JANSEN E T.Effects of unequal air-flow distribution from twin inlet ducts on performance of an axial-flow turbojet engine［R］.NACA RM E54E13,1954.
|
| [2] |
HARRY D P,LUBICK R J.Inlet-air distortion effects on stall,surge and acceleration margin of a turbo-jet engine equipped with variable compressor inlet guide vanes［R］.NACA RM E54K26,1955.
|
| [3] |
LUEDKE J G.Use of nonlinear Volterra theory in predicting the propagation of non-uniform flow through an axial compressor［D］.Blacksburg,Virginia:Virginia Polytechnic Institute and State University,2001.
|
| [4] |
WALLACE R M.Modal response of a transonic fan blade to periodic inlet pressure distortion［D］.Blacksburg,Virginia:Virginia Polytechnic Instituted State University,2003.
|
| [5] |
HALE A,OBRIEN W.A three-dimensional turbine engine analysis compressor code (TEACC) for steady-state inlet distortion［J］.Journal of Turbomachinery,1998,120(3):422-430.
|
| [6] |
GONG Y,TAN C S,GORDON G S,et al.A computational model for short wavelength stall inception and development in multistage compressors［R］.Journal of Turbomachinery,1999,121(3):726-734.
|
| [7] |
郑宁,邹正平,徐立平.风扇进气畸变三维非定常数值模拟技术研究［J］.航空动力学报,2007,22(1):60-65．ZHENG Ning,ZOU Zhengping,XU Liping.3-D unsteady numerical simulation of fan/compressor with inlet distortion［J］.Journal of Aerospace Power,2007,22(1):60-65.(in Chinese)
|
| [8] |
尹超,胡骏,郭晋,等.进气畸变对压气机性能影响的三维彻体力模型［J］.航空动力学报,2015,30(9):2241-2250.YIN Chao,HU Jun,GUO Jin,et al.Three-dimensional body-force model for effect on compressor performance of inlet distortion［J］.Journal of Aerospace Power,2015,30(9):2241-2250.(in Chinese)
|
| [9] |
HIRAI K,KODAMA H,NOZAKI O,et al.Unsteady three-dimensional analysis of inlet distortion in turbomachinery［R］.AIAA 97-2735,1997.
|
| [10] |
张燕峰,楚武利,卢新根.进口总压畸变对亚音速轴流压气机流场影响数值研究［J］.西北工业大学学报,2009,27(1):12-16.ZHANG Yanfeng,CHU Wuli,LU Xingen.Numerical simulation of the effect of total pressure inlet distortion on a subsonic axial-flow compressor［J］.Journal of Northwestern Polytechnical University,2009,27(1):12-16.(in Chinese)
|
| [11] |
陈美宁,朴英,王大磊.总压进气畸变对压气机转子气动影响的数值模拟［J］.航空动力学报,2009,24(8):1792-1798.CHEN Meining,PIAO Ying,WANG Dalei.Numerical simulation of the effect of total pressure inlet distortion on a compressor rotor［J］.Journal of Aerospace Power,2009,24(8):1792-1798.(in Chinese)
|
| [12] |
LESSER A,ISELER J,NIEHUIS R.Numerical investigation of a highly loaded axial compressor stage with inlet distortions［R］.ASME Paper GT2011-46457,2011.
|
| [13] |
孙鹏,高海洋,都昆,等.两种形式总压畸变对超声速压气机流场影响的数值研究［J］.工程热物理学报,2013,34(5):830-835.SUN Peng,GAO Haiyang,DU Kun,et al.Numerical study of a supersonic compressor with two forms of inlet total pressure distortion［J］.Journal of Engineering Thermophysics,2013,34(5):830-835.(in Chinese)
|
| [14] |
KHALEGHI H,JALALY R.Effects of circumferential inlet distortion on the performance of a transonic fan together with the impact of tip injection［R］.ASME Paper 2016-GT-58145,2016.
|
| [15] |
张皓光.轴流压气机机匣处理的试验与数值研究［D］.西安:西北工业大学,2008.ZHANG Haoguang.Experimental and numerical investigation of casing treatment on an axial-flow compressor［D］.Xian:Northwestern Polytechnical University,2008.(in Chinese)
|
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