共 26 条
- [1] VIJAYRAJ K,, GOVARDHAN M., Aerodynamics of contra-rotating fans with swept blades, (2015)
- [2] HAN Shaobing, ZHANG Wenqi, ZHONG Jingjun, Research on design of blade tip winglet for transonicfan rotor and mechanism of stability enhancement, Journal of Propulsion Technology, 41, 7, pp. 1484-1492, (2020)
- [3] CHEN Y,, YANG L, ZHONG J., Numerical study on endwall fence with varying geometrical parameters in a highly-loaded compressor cascade[J], Aerospace Science and Technology, 94, pp. 1053901-10539010, (2019)
- [4] MA S,, CHU W,, ZHANG H,, Et al., Impact of a combination of micro-vortex generator and boundary layer suction on performance in a high-load compressor cascade, (2018)
- [5] SHI L, LIU B, Et al., Experimental investigation of a counter-rotating compressor with boundary layer suction, Chinese Journal of Aeronautics, 28, 4, pp. 1044-1054, (2015)
- [6] KHALEGHI H., Parametric study of injector radial penetration on stalling characteristics of a transonic fan, Aerospace Science and Technology, 66, pp. 112-118, (2017)
- [7] LI J., Self-adaptive stability-enhancing technology with tip air injection in an axial flow compressor, Journal of Turbomachinery, 139, 1, pp. 81-89, (2017)
- [8] CHU Wuli, LU Xingen, WU Yanhui, Numerical and experimental investigations of the flow in a compressor with circumferential grooves, Journal of Aerospace Power, 21, 1, pp. 100-105, (2006)
- [9] DAY I J., Stall, surge, and 75 years of research, Journal of Turbomachinery, 138, 1, pp. 1-16, (2016)
- [10] CHEN H, KOLEY S S, LI Y, Et al., Systematic experimental evaluations aimed at optimizing the geometry of axial casing groove in a compressor, (2019)