[1] RAINS D A. Tip clearance flows in axial compressors and pumps[D]. Pasadena: California Institute of Technolo-gy,1954.
[2] ADAMCZYK J J, CELESTINA M L, GREITZER E M. The role of tip clearance in high-speed fan stall[J]. Journal of Turbomachinery,1993,115(1):28-39.
[3] COPENHAVER W W, MAYHEW E, HAH C, et al. The effect of tip clearance on a swept transonic compressor rotor[C]. ASME paper 94-GT-363.
[4] SAKULKAEW S, TAN C S, DONAHOO E, et al. Com-pressor efficiency variation with rotor tip gap from van-ishing to large clearance[J]. ASME Journal of Tur-bomachinery,2013,135(3):35-48.
[5] YAMADA K, KIKUTA H, FURUKAWA M, et al. Effects of tip clearance on the stall inception process in an axial compressor rotor[C]. ASME Paper 2013-GT-95479.
[6] HOYING D A, TAN C S, VO H D, et al. Role of blade passage flow structures in axial compressor rotating in-ception[J]. Journal of Turbomachinery,1999,121(4):735-742.
[7] HAH C, BERGNER J, SCHIFFER H. Short length-scale rotating stall inception in a transonic axial compressor cri-teria and mechanisms[R]. ASME Paper 2006-GT-90045,2006
[8] VO H D, TAN C S, GREITZER E M. Criteria for spike initiated rotating stall[J]. Journal of Turbomachin-ery,2008,130(1):1-9.
[9] DU J, LIN F, ZHANG H W, et al. Numerical investigation on the originating mechanism of unsteadiness in tip leakage flow for a transonic fan rotor[R]. ASME Paper 2008GT-51463,2008.
[10] 刘东健,李军,李建伟,等.转子叶顶间隙泄漏流轨迹前移的动力学机制[J].航空动力学报,2014,29(7):1680-1687.
LIU D J, LI J, LI J W, et al. Dynamics mechanism of tip leakage flow trajectory movement in rotor[J]. Journal of Aerospace Power,2014,29(7):1680-1687.(in Chinese)
[11] 张晨凯,胡骏,王志强,等.轴流压气机转子叶尖间隙流动结构的数值研究[J].航空学报,2014,35(5):1236-1245.
ZHANG C K, HU J, WANG Z Q, et al. Numerical study on tip clearance flow structure of an axial flow compres-sor rotor[J]. Acta Aeronautica et Astronautica Sini-ca,2014,35(5):1236-1245.(in Chinese)
[12] 谢芳,楚武利,李相君,等.叶尖间隙对跨声速轴流压气机近失速的影响[J].航空动力学报,2014,29(10):2417-2423.
XIE F, CHU W L, LI X J, et al. Influence of blade tip clearance at near-stall condition on transonic axial-flow compressor[J]. Journal of Aerospace Pow-er,2014,29(10):2417-2423.(in Chinese)
[13] 付磊,宋西镇,袁巍,等.跨声速压气机转子叶尖非定常流场数值研究[J].航空动力学报,2013,28(12):2821-2828.
FU L, SONG X Z, YUAN W, et al. Numerical investiga-tions on unsteady flow field at tip region in transonic compressor rotor[J]. Journal of Aerospace Pow-er,2013,28(12):2821-2828.(in Chinese)
[14] 刘宝杰,张志博,于贤君.轴流压气机转子叶尖泄漏堵塞特性的试验研究[J].航空学报,2013,34(12):2682-2691.
LIU B J, ZHANG Z B, YU X J. Experimental investiga-tion on characteristics of tip leakage blockage in an axial compressor[J]. Acta Aeronautica et Astronautica Sini-ca,2013,34(12):2682-2691.(in Chinese)
[15] Yu Y, Liu Q Y, Shen B Y, et al. Radial clearance analysis on high pressure compressor[J].推进技术,2013,34(3):339-346.
[16] GRAF M B, WONG T S, GREITZER E M, et al. Effects of nonaxisymmetric tip clearance on axial compressor performance and stability[J]. Journal of Turbomachin-ery,1998,120(4):648-661.
[17] GORDON K A. Three-dimensional rotating stall inception and effects of rotating tip clearance asymmetry in axial compressor[D]. Massachusetts : Massachusetts Insitute of Technology,1999.
[18] CAMERON J D, BENNINGTON M A, ROSS M H, et al. Effects of steady tip clearance asymmetry and rotor whirl on stall inception in an axial compressor[R]. ASME Paper GT2007-28278,2007.
[19] MARE L D, IMREGUN M, GREEN J S. Effect of real geometry on compressor performance predictions[R]. ASME Paper GT2009-59824,2009.
[20] KANG Y S, KANG S H. Prediction of the nonuniform tip clearance effect on the axial compressor flow field[J]. Journal of Fluids Engineering,2010,132(5):0511101-9.
[21] SONG S J, CHO S H. Nonuniform flow in a compressor due to asymmetric tip clearance[J]. Journal of tur-bomachinery,2000,122(4):751-760.
[22] 梁武昌,楚武利,朱俊强,等.非轴对称尖部间隙对轴流压气机性能影响的实验研究[J].航空动力学报,2004,19(2):233-236.
LIANG W C, CHU W L, ZHU J Q, et al. Effects of asymmetric tip clearance on axial flow compressor per-formance[J]. Journal of Aerospace Pow-er,2004,19(2):233-236.(in Chinese)
[23] 陈颖秀,侯安平,张明明,等.轴流压气机机匣变形对多排转子流场特性的影响[J].航空学报,2016,37(11):3284-3295.
CHEN Y X, HOU A P, ZHANG M M, et al. Effects of casing deformation on blade rows flow field characteris-tics in an axial-flow compressor[J]. Acta Aeronautica et Astronautica Sinica,2016,37(11):3284-3295.(in Chinese)
[24] 桂幸民,王同庆,于清,等.跨音压气机转子叶尖流场试验与分析[J].工程热物理学报,1998,19(5):553-558.
GUI X M, WANG T Q, YU Q, et al. Investigation on the tip clearance flow field in a transonic compressor rotor[J]. Journal of Engineering Thermophysics,1998,19(5):553-558.(in Chinese)
CJA