[1] Ballal D R, Zelina J. Progress in Aeroengine Technology (1939-2003)[J]. Journal of Aircraft, 2004, 41: 43-50.
[2] Lakshminarayana B. Fluid Dynamics and Heat Transfer in Turbomachinery[M]. New York: John Wiley and Sons, 1996.
[3] Gbadebo S A, Cumpsty N A, Hynes T P. Three-Dimensional Separations in Axial Compressors[J]. Journal of Turbomachinery, 2005, 127: 331-339.
[4] Lei V-M, Spakovszky Z S, Greitzer E M. A Criterion for Axial Compressor Hub-Corner Stall[J]. Journal of Turbomachinery, 2008, 130(3).
[5] Hah C, Loellbach J. Development of Hub Corner Stall and its Influence on the Performance of Axial Compressor Blade Rows[J]. Journal of Turbomachinery, 1999, 121: 67-77.
[6] Zhang H, Wang S, Wang Z. Variation of Vortex Structure in a Compressor Cascade at Different Incidences[J]. Journal of Propulsion and Power, 2007, 23: 221-226.
[7] Zhang Y, MahallatiA, Benner M. Experimental and Numerical Investigation of Corner Stall in a Highly-Loaded Compressor Cascade[R]. ASME GT 2014-27204.
[8] Merchant A, Kerrebrock J, Adamczyk J, et al. Experimental Investigation of a High Pressure Ratio Aspirated Fan Stage[J]. Journal of Turbomachinery, 2005, 127:43-51.
[9] Gbadebo S A, Cumpsty N A, Hynes T P. Control of Three-Dimensional Separation in Axial Compressors by Tailored Boundary Layer Suction[J]. Journal of Turbomachinery, 2008, 130(1).
[10] Godard A, Bario F, Burguburu S, et al. Experimental and Numerical Study of a Subsonic Aspirated Cascade [R]. ASME GT 2012-69011.
[11] 王掩刚, 牛楠, 赵龙波, 等. 端壁抽吸位置对压气机叶栅角区分离控制的影响[J]. 推进技术, 2010, 31(4): 433-437. (WANG Yan-gang, NIU Nan, ZHAO Long-bo, et al. Effect on Corner Separation Control for High Load Compressor Cascade with Different End-Wall BLS Position[J]. Journal of Propulsion Technology, 2010, 31(4): 433-437.)
[12] 茅晓晨, 刘波, 张鹏, 等. 组合抽吸对高负荷压气机叶栅流动分离控制的研究[J]. 推进技术, 2016, 37(1): 8-17. (MAO Xiao-chen, LIU Bo, ZHANG Peng, et al. Research on Flow Separation Control for a Highly Loaded Compressor Cascade with Combined Boundary Layer Suction[J]. Journal of Propulsion Technology, 2016, 37(1): 8-17.)
[13] Ma W, Ottavy X, Lu L, et al. Intermittent Corner Separation in a Linear Compressor Cascade[J]. Experiments in Fluids, 2013, 54(6): 1-17.
[14] Devenport W J, Simpson R L. Time-Dependent and Time-Averaged Turbulence Structure near the Nose of a Wing-Body Junction[J]. Journal of Fluid Mechanics, 1990, 210: 23-55.
[15] Tian Q, Simpson R L. Experimental Study of Tip Leakage Flow in the Linear Compressor Cascade: Part I: Stationary Wall [R]. AIAA 2007-269.
[16] Gand F, Deck S, Brunet V, et al. Flow Dynamics Pass a Simplified Wing Body Junction[J]. Physics of Fluids, 2010, 22(11).
[17] Spalart P R. Detached-Eddy Simulation[J]. Annual Review of Fluid Mechanics, 2009, 41: 181-202.
[18] Spalart P R, Deck S, Shur M L, et al. A New Version of Detached-Eddy Simulation, Resistant to Ambiguous Grid Densities[J]. Theoretical and Computational Fluid Dynamics, 2006, 20(3): 181-195.
[19] Ma W. Experimental Investigation of Corner Stall in a Linear Compressor Cascade[D]. France: Ecole Centrale de Lyon, 2012.
[20] Hunt J C R. Eddies, Streams, Convergence Zones in Turbulent Flows[J]. Studying Turbulence Using Numerical Simulation Databases, 1988, (2): 193-208. * 收稿日期:2016-09-16;修订日期:2016-11-04。基金项目:国家自然科学基金(51506121)。作者简介:张策,男,硕士生,研究领域为流动稳定性。E-mail: zhangce@sjtu.edu.cn(编辑:史亚红)
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