[1]
Denton J.D., Loss mechanism in turbomachines. Journal of Turbomachinery, 1993, 115(04): 621–656.
DOI: 10.1115/93-GT-435.
[2]
Han S.B., Numerical simulation of using blade tip winglet in plane compressor cascade. Dalian Maritime University, Dalian, China, 2009. (in Chinese)
[3]
Han S.B., Experimental and numerical investigation of compressor tip clearance flow control using blade tip winglet. Dalian Maritime University, Dalian, China, 2013. (in Chinese)
[4]
Zhong J.J., Wu W.Y., Han S.B., Research progress of tip winglet technology in compressor. Journal of Thermal Science, 2021, 30(01): 18–31.
DOI: 10.1007/s11630-020-1402-3.
[5]
Wu W.Y., Zhong J.J., Han S.B., Effects of pressure side winglet on aerodynamic performance of high subsonic compressor cascade with different incidences. Journal of Propulsion Technology, 2018, 39(01): 76–85.
DOI: 10.13675/j.cnki.tjjs.2018.01.008. (in Chinese)
[6]
Wu W.Y., Zhong J.J., Experimental investigation of the influence on compressor cascade characteristics at high subsonic speed with pressure surface tip winglets. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, February 2021. DOI: 10.1177/0957650921990198.
[7]
Han S.B., Zhong J.J., Lu H.W., Experimental investigation of compressor cascade tip leakage flow control using suction-side winglet with different widths. Journal of Propulsion Technology, 2016, 37(03): 471–478. DOI: 0.13675/j.cnki.tjjs.2016.03.009. (in Chinese)
[8]
Wu W.Y., Zhong J.J., Wang H.S., Control effect of suction side winglet on tip clearance leakage at different inlet Mach number of high subsonic. Journal of Engineering Thermophysics, 2019, 40(10): 2266–2276. DOI: CNKI:SUN:GCRB.0.2019-10-011. (in Chinese)
[9]
Han S.B., Zhong J.J., Yang L., Wei M., Numerical study of tip-clearance effect of a compressor rotor with pressure-side winglet. Journal of Engineering Thermophysics, 2014, 35(09): 1739–1743. (in Chinese)
DOI: CNKI: SUN: GCRB.0.2014-09-013.
[10]
Zhong J.J., Han S.B., Effects of blended tip winglet on aerodynamic performance of a low speed compressor rotor. Journal of Propulsion Technology, 2014, 35(06): 749–757. (in Chinese)
DOI: 10.13675/j.cnki.tjjs.2014.06.005.
[11]
Han S.B., Zhong J.J., Influence of blade tip winglet on the off-design performance of a transonic compressor rotor. Journal of Aerospace Power, 2016, 31(03): 647–658. (in Chinese)
DOI: 10.13224/j.cnki.jasp.2016.03.016.
[12]
Han S.B., Guo Y.C., Zhong J.J., Influence of tip winglet combined with tip groove on the leakage flow of compressor cascade. Journal of Engineering Thermophysics, 2019, 40(06): 1268–1274. (in Chinese)
DOI: CNKI:SUN:GCRB.0.2019-06-010.
[13]
Sang Z.L., Experimental study on influence of blade tip geometries on the tip clearance flow of compressor cascade. Dalian Maritime University, Dalian, China, 2017. (in Chinese)
[14]
Wu W.Y., Zhong J.J., Han S.B., Numerical simulation of blade tip winglet on the aerodynamic performance of high subsonic compressor cascade. Journal of Dalian Maritime University, 2017, 43(02): 97–102. (in Chinese) DOI: 10.16411/j.cnki.issn1006-7736.2017.02.015.
[15]
Wbitcomb R.T., A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets. NASA TN D-8260.
[16]
Zhao Y., The influence of aerodynamic performance by using tip winglet with different width in rectangular compressor cascade. Dalian Maritime University, Dalian, China, 2013. (in Chinese)
[17]
Inoue M., Kuroumaru M., Furukawa M., Behaviour of tip leakage flow behind and axial compressor rotor. Journal of Engineering for Gas Turbines and Power, 1986, 108(01): 7–14. DOI: 10.1115/1.3239889.
[18]
Inoue M., Furukawa M., Saiki K., Yamada K., Physical excaseations of tip leakage flow field in an axial compressor rotor. In Proceedings of the ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition, Stockholm, Sweden, 2–5 June 1998; V001T001A027, DOI: 10.1115/98-gt-091.
[19]
Lakshiminarayana B., Zaccaria M., Marathe B., The structure of tip clearance flow in axial flow compressors. Journal of Turbomachinery, 1995, 117(03): 336–347. DOI: 10.1115/1.2835667.
