[1] Chen S W, Guo S, Lu H W, et al. Analysis of the aerodynamic performance of a super highly loaded adsorption type compressor cascade. Journal of Engineering for Thermal Energy & Power, 2009, 24(1): 167-171. (in Chinese) 陈绍文, 郭爽, 陆华伟, 等. 超高负荷吸附式压气机叶栅气动性能分析. 热能动力工程, 2009, 24(1): 167-171.[2] Zheng X Q, Zhou X B, Zhou S. Investigation on a type of flow control to weaken unsteady separated flows by unsteady excitation in axial flow compressors. ASME Journal of Turbomachinery, 2005, 127(2): 489-496.[3] Zhang Y J, Chen F, Feng G T, et al. Influence of turning angle on flow field performance of linear bowed stator in compressor at low Mach number. Chinese Journal of Aeronautics, 2006, 19(4): 271-277.[4] Li Y H, Liang H, Ma Q Y, et al. Experimental investigation on airfoil suction side flow separation by pulse plasma aerodynamic actuation. Acta Aeronautica et Astronautica Sinica, 2008, 29(6): 1429-1435. (in Chinese) 李应红, 梁华, 马清源, 等. 脉冲等离子体气动激励抑制翼型吸力面流动分离的实验. 航空学报, 2008, 29(6): 1429-1435.[5] Perez-Blanco H, van Dyken R, Byerley A, et al. Turbine cascade flow control using a wake filling pulsed plasma actuator. ASME GT2005-68114.[6] Huang J H, Corke T C, Thomas F O. Unsteady plasma actuators for separation control of low-pressure turbine blades. AIAA Journal, 2006, 44(7): 1477-1487.[7] Wu Y, Li Y H, Zhu J Q, et al. Experimental investigation of a subsonic compressor with plasma actuation treated casing. AIAA-2007-3849, 2007.[8] Wu Y, Li Y H, Zhu J Q, et al. Experimental investigation of using plasma aerodynamic actuation to extend low-speed axial compressor's stability. Journal of Aerospace Power, 2007, 22(12): 2025-2030. (in Chinese) 吴云, 李应红, 朱俊强, 等. 等离子体气动激励扩大低速轴流压气机稳定性的实验研究. 航空动力学报, 2007, 22(12): 2025-2030.[9] Vo H D. Control of rotating stall in axial compressors using plasma actuators. AIAA-2007-3845, 2007.[10] Lewin E, Koulovic D, Stark U. Experimental and numerical analysis of hub-corner stall in compressor cascades. ASME GT2010-22704.[11] Nerger D, Saathoff H, Radespiel R, et al. Experimental investigation of endwall and suction side blowing in a highly loaded compressor stator cascade. ASME GT2010-22578.[12] Porter C O, Enloe C L, Mclaughlin T E, et al. Boundary layer control using a DBD plasma actuator. AIAA-2007-0786, 2007.[13] Dorfner C, Hergt A, Nicke E, et al. Advance non-axisymmetric endwall contouring for axial compressors by generating an aerodynamic separator—Part I: principal cascade design and compressor application. ASME GT2009-59383.[14] Benard N, Jolibois J, Moreau E. Lift and drag performances of an axisymmetric airfoil controlled by plasma actuator. Journal of Electrostatics, 2009, 67(2-3): 133-139.[15] Kang S, Wang Z Q. An application of topological analysis to studying the three-dimensional flow in cascade;part I—Topological rules for skin-friction lines and section streamlines. Applied Mathematics and Mechanics, 1990, 11(5): 457-462.[16] Zhang Y J, Wang H S, Xu J Z, et al. Research on topology and vortex structure in diffuser cascades. Science Chinese, Series E: Technological Science, 2009, 39(5): 1016-1025. (in Chinese) 张永军, 王会社, 徐建中, 等. 扩压叶栅中拓扑和漩涡结构的研究. 中国科学, E辑: 技术科学, 2009, 39(5): 1016-1025.[17] Zhao X H, Li Y H, Yue T P, et al. Experimental investigation of flow separation control on highly loaded compressor cascade by plasma aerodynamic actuation. High Voltage Engineering, 2011, 37(6): 1521-1527. (in Chinese) 赵小虎, 李应红, 岳太鹏, 等. 等离子体气动激励抑制高负荷压气机叶栅流动分离的实验研究. 高电压技术, 2011, 37(6): 1521-1527.[18] Han W J, Yang Q H. Topology and vortex structures of turbine cascade with different tip clearance. Chinese Journal of Aeronautics, 2002, 15(1): 18-26.[19] Zhang H X, Deng X G. A nalytic studies for three-dimensional steady separated flows and vortex motion. Acta Aerodynamic Sinica, 1992, 10(1): 8-12. (in Chinese) 张涵信, 邓小刚. 三维定常分离流和涡运动的定性分析研. 空气动力学报, 1992, 10(1): 8-12.[20] Seraudie A, Aubert E, Naude N, et al. Effect of plasma actuators on a flat plate laminar boundary layer in subsonic condition. AIAA-2006-3350, 2006. |