| Citation: | HU Jia-guo, WANG Ru-gen, LI Shao-wei, GAN Tian. Radial vortex phenomenon and instability mechanism of transonic axial-flow compressor[J]. Journal of Aerospace Power, 2014, 29(9): 2239-2246. doi: 10.13224/j.cnki.jasp.2014.09.030
|
| [1] |
Schlechtriem W E,Lotzerich M.Breakdown of tip leakage vortices in compressors at flow conditions close to stall[R].ASME Paper 97-GT-41,1997.
|
| [2] |
Hoffman W H,Ballman J.Some aspects of tip vortex behavior in a transonic turbo compressor[R].International Society for Air Breathing Engines,ISABE Paper 2003-1223,2003.
|
| [3] |
Hoffman W H,Ballman J.Flow mechanisms in a transonic turbo compressor at conditions near stall[R].International Society for Air Breathing Engines,ISABE Paper 2005-1139,2005.
|
| [4] |
Hah C,Rabe D C.Role of tip clearance flows on flow instability in axial flow compressors[R].International Society for Air Breathing Engines,ISABE Paper 2001-1223,2001.
|
| [5] |
张燕峰,楚武利,卢新根.跨音速轴流压气机近失速状态的间隙泄漏流流动特性[J].航空动力学报,2008,23(7):1293-1298. ZHANG Yanfeng,CHU Wuli,LU Xingen.Numerical simulation of the flow characteristic of tip leakage flow in a transonic axial-flow compressor at a near stall condition[J].Journal of Aerospace Power,2008,23(7):1293-1298.(in Chinese)
|
| [6] |
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 its passive control strategies in axial-compressor[D].Xi'an:Northwestern Polytechnical University,2007.(in Chinese)
|
| [7] |
周敏.低雷诺数下跨音速压气机流动失稳及附面层控制策略研究[D].西安:空军工程大学,2009. ZHOU Min.Flow instability mechanism of transonic compressor at low Reynolds number and boundary layer control strategies[D].Xi'an:Air Force Engineering University,2009.(in Chinese)
|
| [8] |
王沛,朱俊强,黄伟光,等.间隙流触发压气机内部流动失稳机制及周向槽扩稳机理[J].航空动力学报,2008,23(6):1067-1071. WANG Pei,ZHU Junqiang,HUANG Weiguang,et al.Role of tip leakage flow on flow instability and its control with circumferential groove casing treatment[J].Journal of Aerospace Power,2008,23(6):1067-1071.(in Chinese)
|
| [9] |
Merchant A A.Design and analysis of axial aspirated compressor stage[D].Cambridge,US:Massachusetts Institute of Technology,1999.
|
| [10] |
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)
|
| [11] |
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,2009,24(2):414-419. 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,2009,24(2):414-419.(in Chinese)
|
| [12] |
周敏,王如根,白云,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过程研究[J].航空动力学报,2009,24(6):1379-1384. ZHOU Min,WANG Rugen,BAI Yun,et al.Research on flow instability triggering process at stall condition of transonic compressor rotor at low Reynolds number[J].Journal of Aerospace Power,2009,24(6):1379-1384.(in Chinese)
|
| [13] |
Reid L,Moore R D.Design and overall performance of four highly-loaded,high-speed inlet stages for an advanced,high-pressure-ratio core compressor[R].NASA TP-1337,1978.
|
| [14] |
Boretti A.Experimental and computational analysis of a transonic compressor rotor[R].Auckland:17th Australasian Fluid Mechanics Conference,2010.
|
| [15] |
Dawes W N.A numerical analysis of the three-dimensional viscous flow in a transonic compressor rotor and comparison with experiment[J].Journal of Turbomachinery,1987,109(3):83-90.
|
| [16] |
于宏军,刘宝杰,刘火星.设计状态下压气机转子叶尖泄漏涡流动研究[J].航空学报,2004,25(1):1-8. YU Hongjun,LIU Baojie,LIU Huoxing.Investigation of tip leakage vortex in compressor on design condition[J].Acta Aeronautica et Astronautica Sinica,2004,25(1):1-8.(in Chinese)
|
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