[1] 刘大响. 航空动力发展的历史性机遇[J]. 航空发动机, 2005, 13(2): 1-3.
[2] 邵卫卫. 风扇/轴流压气机最大负荷设计技术探索[D]. 北京:中国科学院研究生院(工程热物理研究所), 2008.
[3] Bmynes, Taylr, David J Peake,et al. Viscous Flow Control with Air-Jet Vortex Generators[R]. AIAA 99-3175.
[4] Lachmann G V. Boundary Layer and Flow Control[M]. Oxford:Pergamon Press, 1961.
[5] Pearcey H H. Shock-Induced Separation and Its Prevention. Boundary Layer and Flow Control-Its Principles and Application[M]. Oxford: Pergamon Press, 1961.
[6] Steven M Klausmeyer, Michael Papadakis, John C Lin. A Flow Physics Study of Vortex generators on a Multi-element Airfoil[R]. AIAA 96-0548.
[7] Ian Broadley, Kevin P Garry. Effectiveness of Vortex Generator Position and Orientation on Highly Swept Wings[R]. AIAA 97-2319.
[8] Ashill P R, Fulker J L, Hackett K C. Research at DERA on Sub Boundary Layer Vortex Generators(SBVGs)[R]. AIAA 2001-0887.
[9] Gammerdinger P M. The Effects of Low-Profile Vortex Generators on Flow in a Transonic Fan-Blade Cascade[D]. Monterey: Naval Postgraduate School, 1995.
[10] Law C H, Wennerstrom A J, Buzzell W A. The Use of Vortex Generators as Inexpensive Compressor Casing Treatment[R]. SAE Paper 1976-0925.
[11] 吴培根. 高负荷风扇流动失稳及流动控制方法研究[D]. 西安:空军工程大学, 2014.
[12] 胡加国, 王如根, 李坤, 等. 非设计条件下跨声速压气机失速机制分析[J]. 推进技术, 2016, 37(8): 1490-1499. (HU Jia-guo, WANG Ru-gen, LI Kun, et al. Instability Mechanism Analysis with Transonic Compressor at Off-Design Work Condition[J]. Journal of Propulsion Technology, 2016, 37(8): 1490-1499.)
[13] 何成, 王如根, 胡加国, 等. 不同转速下叶尖间隙流对跨声速压气机失速的影响[J]. 推进技术, 2016, 37(9): 1657-1663. (HE Cheng, WANG Ru-gen, HU Jia-guo, et al. The Effect of Tip Leakage Flow on Compressor Instability at Different Rotation Speed[J]. Journal of Propulsion Technology, 2016, 37(9): 1657-1663.)
[14] 吴培根, 王如根, 郭飞飞, 等. 涡流发生器对高负荷扩压叶栅性能影响的机理分析[J]. 推进技术, 2016, 37(1): 49-56. (WU Pei-gen, WANG Ru-gen, GUO Fei-fei, et al. Mechanism Analysis of Vortex Generator Effects on High-Load Compressor Cascade[J]. Journal of Propulsion Technology, 2016, 37(1): 49-56.)
[15] Kenneth L Suder. Blockage Development in a Transonic, Axial Compressor Rotor[R]. NASA TM-113115, 1997.
[16] Chunill Hah. Large Eddy Simulation of Transonic Flow Field in NASA Rotor 37[R]. NASA TM-215627, 2009. * 收稿日期:2016-09-10;修订日期:2016-11-08。作者简介:何成,男,硕士生,研究领域为推进系统气动热力理论与工程。E-mail: welcomehh@126.com(编辑:梅瑛)
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