| Citation: | ZHAO Qin, WU Yun, LI Ying-hong, ZHAO Xiao-hu, ZHANG Hai-deng. Experiment of flow separation control in highly loaded compressor cascade corner by endwall plasma aerodynamic actuation[J]. Journal of Aerospace Power, 2013, 28(9): 2129-2139.
|
| [1] |
Mailach R,Vogeler K.Aerodynamic blade row interactions in an axial compressor:Part Ⅱ unsteady profile pressure distrubtion and blade forces[J].Jourmal of Turbomachinery,2004,126(1):45-51.
|
| [2] |
Gbadebo S A,Cumpsty N A,Hynes T P.Three-dimensional separations in axial compressors[J].Journal of Turbomachinery,2005,127(2):331-339.
|
| [3] |
Wang S T,Qiang X D,Lin W C,et al.Highly-loaded low-reaction boundary layer suction axial flow compressor[R].ASME Paper GT2007-28191,2007.
|
| [4] |
刘艳明,钟兢军,黄洪雁,等.端壁翼刀控制压气机叶栅 二次流的机理研究[J].空气动力学报,2005,23(4):431-436. LIU Yanming,ZHONG Jingjun,HUANG Hongyan,et al.The mechanism of end-wall fence in controlling secondary flow of compressor cascade[J].Acta Aerodynamica Sinica,2005,23(4):431-436.(in Chinese)
|
| [5] |
钟兢军,刘艳明,冯国泰.端壁翼刀控制压气机叶栅二次流的数值研究[J].航空动力学报,2004,19(6):817-821. ZHONG Jingjun,LIU Yanming,FENG Guotai.Numerical investigation of the secondary flow control in a compressor cascade using endwall fences[J].Journal of Aerospace Power,2004,19(6):817-821.(in Chinese)
|
| [6] |
Dorfner C,Hergt A,Nicke E,et al.Advanced non-axisymmetric endwall contouring for axial compressors by generating an aerodynamic separator:Part Ⅰ principal cascade design and compressor application[R].ASME Paper GT2009-59383,2009.
|
| [7] |
Hergt A,Dorfner C,Steinert W,et al.Advanced non-axisymmetric endwall contouring for axial compressors by generating an aerodynamic separator:Part Ⅱ experimental and numerical cascade investigation[R].ASME Paper GT2009-59384,2009.
|
| [8] |
Hage W,Meyer R,Paschereit S O.Control of secondary flow in a high loaded compressor stage by means of a groove structure on the sidewalls[R].AIAA 2007-4278,2007.
|
| [9] |
Roth J R,Dai X,Rahel J,et al.The physics and phenomenology of paraelectric one atmosphere uniform glow dscharge plasma (OAUGDPTM) actuators for aerodynamic flow control[R].AIAA-2005-781,2005.
|
| [10] |
Porter C O,McLaughlin T E,Enloe C L,et al.Boundary layer control using a DBD plasma actuator[R].AIAA-2007-786,2007.
|
| [11] |
Rethmel C,Little J,Takashima K,et al.Flow separation control over an airfoil with nanosecond pulse driven DBD plasma actuators[R].AIAA-2011-487,2011.
|
| [12] |
Cristofolini A,Neretti G,Roveda F,et al.Experimental and numerical investigation on a DBD actuator for airflow control[R].AIAA-2011-3912,2011.
|
| [13] |
Kelley C L,Bowles P,Cooney J,et al.High Mach number leading-edge flow separation control using AC DBD plasma actuators[R].AIAA-2012-906,2012.
|
| [14] |
吴云,李应红,朱俊强,等.等离子体气动激励抑制压气机叶栅角区流动分离的仿真与实验[J].航空动力学报,2009,24(4):830-835. WU Yun,LI Yinghong,ZHU Junqiang,et al.Computational and experimental investigation of plasma aerodynamic actuation based corner flow separation control in a compressor cascade[J].Journal of Aerospace Power,2009,24(4):830-835.(in Chinese)
|
| [15] |
LI Yinghong,WU Yun,ZHOU Ming,et al.Control of the corner separation in a compressor cascade by steady and unsteady plasma aerodynamic actuation[J].Experiments in Fluids,2010,48(6):1015-1023.
|
| [16] |
Baughn J W,Porter C O,Peterson B L.Momentum transfer for an aerodynamic plasma actuator with an imposed boundary layer[R].AIAA-2006-168,2006.
|
| [17] |
Opaits D F,Neretti G,Likhanskii A V,et al.Experimental investigation of DBD plasma actuators driven by repetitive high voltage nanosecond pulses with DC or low-frequency sinusoidal bias[R].AIAA-2007-4532,2007.
|
DownLoad: