[1] 唐狄毅. 叶轮机非定常流[M]. 北京:国防工业出版社, 1995.
[2] Moore F K, Greitzer E M. A Theory of Post-Stall Transients in Axial Compressors: Part I - Development of the Equations[J]. ASME Journal of Engineering for Gas Turbines and Power, 1986, 108: 68-76.
[3] Greitzer E M, Moore F K. A Theory of Post-Stall Transients in Axial Compressors, Part II: Application[J]. ASME Journal of Engineering for Gas Turbines and Power, 1986, 108: 231-239.
[4] McDougall N M, Cumpsty N A, Hynes T P. Stall Inception in Axial Compressors[J]. ASME Journal of Turbomachinery, 1990, 112: 116-125.
[5] Garnier V H, Epstein A H, Greitzer E M. Rotating Waves as a Stall Inception Indication in Axial Compressors[J]. ASME Journal of Turbomachinery, 1991, 113(2): 290-301.
[6] Day I J. Stall Inception in Axial Flow Compressors[J]. ASME Journal of Torbomachinery, 1993, 115: 1-9.
[7] Lei V M, Spakovszky Z S, Greitzer E M. A Criterion for Axial Compressor Hub-Corner Stall[J]. ASME Journal of Turbomachinery, 2008, 130.
[8] Gbadebo S A, Cumpsty N A, Hynes T P. Three-Dimensional Separation in Axial Compressors[R]. ASME GT2004-53617.
[9] Hoying D A, Tan C S, Greitzer E M. Role of Blade Passage Flow Structures in Axial Compressor Rotating Stall Inception[J]. ASME Journal of Turbomachinery, 1999, 121(4): 735-42.
[10] Vo H D, Tan C S, Greitzer E M. Criteria for Spike Initiated Rotating Stall[R]. ASME GT2005-68374.
[11] Saathoff H, Stark U.2. Tip Clearance Flow Induced Endwall Boundary Layer Separation in a Single-Stage Axial-Flow Low-Speed Compressor[R]. ASME 2000-GT-0501.
[12] Deppe A, Saathoff H, Stark U. Spike-Type Stall Inception in Axial Compressors[C]. Lille: 6th European Conference on Turbomachinery, 2005.
[13] Bennington M, Cameron J, Morris S, et al. Over Rotor Casing Surface Streak Measurements in a High Speed Axial Compressors[R]. ASME GT2007-28273.
[14] Bennington M, Cameron J, Morris S, et al. Investigation of Tip-Flow Based Stall Criteria Using Rotor Casing Visualization[R]. ASME GT2008-51319.
[15] Hah C, Bergner J, Schiffer H. Short Length-Scale Rotating Stall Inception in a Transonic Axial Compressor-Criteria and Mechanism[R]. ASME GT2006-90045.
[16] Chen J P, Michael D H, Gregory P H. Pre-Stall Behavior of Transonic Axial Compressor Stage Via Time-Accurate Numerical Simulation[R]. ASME GT2007-27926.
[17] Lin F, Zhang J X, Chen J Y, et al. Flow Structure of Short-Length Scale Disturbance in an Axial-Flow Compressor[J]. Journal of Propulsion and Power, 2008, 24(6): 1301-1308.
[18] Benningtong M A, Du J, Ross M H, et al. An Experiment and Computational Investigation of Tip Clearance Flow and Its Impact on Stall Inception[R]. ASME GT2010-23516.
[19] Farhan Ali Hashmi S. Numerical Investigation on Effect of Rotor Blade Lean Angel Variation on Stall Mechanism of Highly Loaded Low Speed Single Stage Fan[D]. Xi’an: Northwestern Polytechnical University, 2011.
[20] Farhan Ali Hashmi S, Qiao Weiyang, Chen Pingping.Prediction of Hub-Corner Stall Characteristics of a Highly Loaded Single Stage Fan[J]. Journal of Thermal Science, 2011, 20(2).
[21] Farhan Ali Hashmi S, Qiao Wei Yang, Chen Ping Ping. Numerical Investigation on Effect of Rotor Blade Lean Angle Variation on Single Stage Fan Stability[C]. Islamabad: 10th International Bhurban Conference on Applied Sciences & Technology, 2013. [21]时培杰. 基于叶尖区流动控制的压气机气动扩稳数值及实验研究[D]. 西安:西北工业大学, 2014.
[22] 陈萍萍. 轴流压气机角区分离流动损失机理及流动控制策略研究[D]. 西安:西北工业大学, 2015.
[23] Day I J, Freeman C. The Unstable Behavior of Low and High Speed Compressors[J]. ASME Journal of Turbomachinery, 1994, 116.
[24] Day I J, Breuer T, Escuret J, et al. Stall Inception and the Prospects for Active Control in Four High Speed Compressors[R]. ASME 1997-GT-281.
[25] Longley J P, Shin H W, Plumley R E, et al. Effects of Rotating Inlet Distortion on Multistage Compressor Stability[J]. ASME Journal of Turbomachinery, 1996, 118: 181-188.
[26] Camp T R, Day I J. A Study of Spike and Modal Stall Phenomena in a Low-Speed Axial Compressor[J]. ASME Journal of Turbomachinery, 1998, 120: 392-401.
[27] Inour M, Kuroumaru M, Yoshida S, et al. Short and Long Length-Scale Disturbances Leading to Rotating Stall in an Axial Compressor Stage with Different Rotor-Stator Gaps[J]. ASME Journal of Turbomachinery, 2001, 123: 24-32.
[28] 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): 432-437. (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): 432-437.)
[29] Inour M, Kuroumaru M, Yoshida S, et al. Short and Long Length-Scale Disturbances Leading to Rotating Stall in an Axial Compressor Stage with Different Rotor-Stator Gaps[J]. ASME Journal of Turbomachinery, 2001, 123: 24-32.
[30] Gannon A J, Hobson G V, Shreeve R P, et al. Experiment Investigation During Stall and Surge in a Transonic Fan Stage & Rotor-Only Configuration[R]. ASME GT2006-90925.
[31] Hoss B, Leinhos D C, Fottner L. Stall Inception in the Compressor System of a Turbofan Engine[J]. ASME Journal of Turbomachinery, 2000, 122: 32-44.
[32] Chen J P, Webster R S, Hathaway M D. Numerical Simulation of Stall and Stall Control in Axial and Radial Compressors[R]. AIAA 2006-418. 收稿日期:2015-10-19;修订日期:2016-01-27。作者简介:强冠杰,男,硕士生,研究领域为叶轮机械气动热力学。E-mail: qianggj@126.com(编辑:梅瑛)
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