| Citation: | HU Jia-guo, WANG Ru-gen, LI Kun, GUO Fei-fei. Vortex structure of secondary flow in transonic axial compressor with low Reynolds number[J]. Journal of Aerospace Power, 2015, 30(10): 2472-2480. doi: 10.13224/j.cnki.jasp.2015.10.021
|
| [1] |
Enomoto S,Hah C.Numerical and experimental investigation of low Reynolds number effects on laminar flow separation and transition in a cascade of compressor blades[R].ASME Paper 2000-GT-276,2000.
|
| [2] |
Schreiber H A,Steinert W,Küsters B.Effects of Reynolds number and free stream turbulence on boundary layer transition in a compressor cascade[R].ASME Paper 2000-GT-0263,2000.
|
| [3] |
Sonoda T,Yamaguchi Y,Arima T,et al.Advanced high turning compressor airfoils for low Reynolds number condition:Part 1 design and optimization[R].ASME Paper GT2003-38458,2003.
|
| [4] |
Schreiber H A,Steinert W,Sonoda T,et al.Advanced high turning compressor airfoils for low Reynolds number condition:Part 2 experimental and numerical analysis[R].ASME Paper GT2003-38477,2003.
|
| [5] |
凌代军,王晖,马昌友.低雷诺数亚声速扩压平面叶栅试验[J].航空动力学报,2013,28(1):171-179. LING Daijun,WANG Hui,MA Changyou.Subsonic compressor plane cascade experiment at low Reynolds number[R].Journal of Aerospace Power,2013,28(1):171-179.(in Chinese)
|
| [6] |
王如根,周敏,赵英武,等.跨声速压气机低雷诺数下流动失稳机制研究[J].航空动力学报,2008,23(12):1903-1907. WANG Rugen,ZHOU Min,ZHAO Yingwu,et al.Research on flow instability mechanism of transonic compressor at low Reynolds number[J].Journal of Aerospace Power,2008,23(12):1903-1907.(in Chinese)
|
| [7] |
周敏,王如根,赵英武,等.低雷诺数下跨声速压气机转子失速工况时流动失稳触发机制研究[J].航空动力学报,2009,24(2):414-418. ZHOU Min,WANG Rugen,ZHAO Yingwu,et al.Research on flow instability mechanism of transonic compressor at low Reynolds number[J].Journal of Aerospace Power,2009,24(2):414-418.(in Chinese)
|
| [8] |
夏钦斌,王如根,周敏.低雷诺数下跨音速转子流动失稳及附面层抽吸扩稳研究[J].航空动力学报,2009,24(7):1610-1615. XIA Qinbin,WANG Rugen,ZHOU Min.Research on flow instability of transonic compressor rotor and boundary suction effect at low Reynolds number[J].Journal of Aerospace Power,2009,24(7):1610-1615.(in Chinese)
|
| [9] |
夏钦斌,王如根,周敏,等.低雷诺数条件下跨音速转子轴向倾斜缝处理机匣扩稳研究[J].航空动力学报,2010,25(6):1389-1394. XIA Qinbin,WANG Rugen,ZHOU Min,et al.Research on the effects of a transonic compressor rotor with axial skewed slots casing treatment at low Reynolds number[J].Journal of Aerospace Power,2010,25(6):1389-1394.(in Chinese)
|
| [10] |
Cornish J J.Vortex flows[R].AIAA 83-1812.1983.
|
| [11] |
Kang S.Investigation of the three dimensional flow within a compressor cascade with and without tip clearance[D].Belgium:Vrije Universiteit Brussel,1993.
|
| [12] |
赵小虎,吴云,李应红,等.高负荷压气机叶栅分离结构及 其等离子体流动控制[J].航空学报,2012,33(2):208-219. ZHAO Xiaohu,WU Yun,LI Yinghong,et al.Separation structure and plasma flow control on highly load compressor[J].Acta Aeronautica et Astronautica Sinica,2012,33(2):208-219.(in Chinese)
|
| [13] |
Inoue M,Kuroumaru M.Three-dimensional structure and decay of vortices behind an axial flow rotation blade row[R].ASME Paper 83-GT-69,1983.
|
| [14] |
Gbadebo S A,Cumpsty N A.Three-dimensional separations in axial compressors[R].ASME Paper GT-2004-53617,2004.
|
| [15] |
Suder K L,Celestina M L.Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor[R].NASA TM-106711,1994.
|
| [16] |
卢新根.轴流压气机内部流动失稳及其被动控制策略研究[D].西安:西北工业大学,2007. LU Xingen.Flow instability and tis passive control strategies in axial-compressor[D].Xi'an:Northwestern Polytechnical University,2007.(in Chinese)
|
| [17] |
Jeong J,Hussain F.On the identification of a vortex[J].Journal of Fluid Mechanics,1995,285:69-94.
|
| [18] |
胡子俊,张楠,姚惠之,等.涡判据在孔腔涡旋流动拓扑结构分析中的应用[J].船舶力学,2012,16(8):839-846. HU Zijun,ZHANG Nan,YAO Huizhi,et al.Vortex identification in the analysis on topology structure vortical flow in cavity[J].Journal of Ship mechanics,2012,16(8):839-846.(in Chinese)
|
| [19] |
Maskell E C.Flow separation in three dimensions[R].Royal Aeronautical Establishment,RAE Aero,Rept2565,1955.
|
| [20] |
张涵信,邓小刚.二维定常分离流和涡运动的定性分析研究[J].空气动力学学报,1992,10(1):8-19. ZHANG Hanxin,DENG Xiaogang.Qualitative research on two-dimensional steady separation flow and vortex movement[J].Acta Aerodynamica Sinica,1992,10(1):8-19.(in Chinese)
|
DownLoad: