[1]
Liang T., Liu B., Spence S., et al., Numerical investigation into the effects of tip clearance on the performance of a counter-rotating axial flow compressor. Journal of Applied Fluid Mechanics, 2020, 13(5): 1587–1599.
[2]
Mailach R., Lehmann I., Vogeler K., Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex. Journal of Turbomachinery, 2000, 123(3): 453–460.
[3]
Shen X., Zhang D., Xu B., et al., Comparative study of tip leakage vortex trajectory and cavitation in an axial flow pump with various tip clearances. Journal of Mechanical Science and Technology, 2022, 36(3): 1289–1302.
[4]
Du J., Lin F., Zhang H., et al., Numerical investigation on the self-induced unsteadiness in tip leakage flow for a transonic fan rotor. Journal of Turbomachinery, 2010, 132(2): 021017.
[5]
Kan X., Wu W., Zhong J., Effects of vortex dynamics mechanism of blade-end treatment on the flow losses in a compressor cascade at critical condition. Aerospace Science and Technology, 2020, 102: 105857.
[6]
Tian Q., Simpson R., Experimental study of tip leakage flow in the linear compressor cascade: Part i-stationary wall. 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, United States, 2007.
[7]
Fukano T., Jang C., Tip clearance noise of axial flow fans operating at design and off-design condition. Journal of Sound and Vibration, 2004, 275(3): 1027–1050.
[8]
Kameier F., Neise W., Experimental study of tip clearance losses and noise in axial turbomachines and their reduction. Journal of Turbomachinery, 1997, 119(3): 460–471.
[9]
Qiao W., Wang L., Duan W., et al., Theory, model and method of aero-engine aeroacoustic design. Journal of Propulsion Technology, 2021, 42(1): 10–38.
[10]
Cyrus V., Rehak K., Polansky J., Unsteady flows in the last stator rows of axial compressor of gas turbine working in coal gasification combined cycle. Turbo Expo: Power for Land, Sea, and Air, New York, United States, 2006.
[11]
Hellmich B., Acoustic resonance in a high-speed axial compressor. Leibniz Universitat Hannover, Germany, 2008.
[12]
Hong Z., Zhao G., Yang M., et al., Development of flow-induced acoustic resonance in aeroengine compressors. Acta Aeronautica et Aerodynamica Sinica, 2019, 40(11): 023139.
[13]
Chen G.T., Greitzer E.M., Tan C.S., et al., Similarity analysis of compressor tip clearance flow structure. Journal of Turbomachinery, 1991, 113(2): 260–269.
[14]
Gao Y., Liu Y., A flow model for tip leakage flow in turbomachinery using a square duct with a longitudinal slit. Aerospace Science and Technology, 2019, 95: 105460.
[15]
Wheeler A.P., Sandberg R.D., Direct numerical simulations of a transonic tip flow with free-stream disturbances. ASME Turbine Blade Tip Symposium, Hamburg, Gemany, 2013.
[16]
Maynard J.M., Wheeler A.P.S., Taylor J.V., et al., Unsteady structure of compressor tip leakage flows. Journal of Turbomachinery, 2022, 145(5): 051005.
[17]
Shang W., Li D., Luo K., et al., Effects of tip clearance size on vortical structures and turbulence statistics in tip-leakage flows: A direct numerical simulation study. Physics of Fluids, 2021, 33(8): 085127.
[18]
Yang D.G., Li J.Q., Liang J.M., Sound generation induced by self-sustained oscillations inside cavities based on CFD and aeroacoustic theory. ACTA Aerodynamica Sinica, 2010, 28(6): 724–730.
[19]
Boudet J., Caro J., Li B., et al., Zonal large-eddy simulation of a tip leakage flow. International Journal of Aeroacoustics, 2016, 15(6–7): 646–661.
[20]
Bai X., Cheng H., Ji B., LES investigation of the noise characteristics of sheet and tip leakage vortex cavitating flow. International Journal of Multiphase Flow, 2022, 146: 103880.
[21]
Decaix J., Balarac G., Dreyer M., et al., RANS and LES computations of the tip-leakage vortex for different gap widths. Journal of Turbulence, 2015, 16(4): 309–341.
[22]
Gao Y., Liu Y., Lu L., Modification of realizable k-e model for tip-leakage flow in an axial compressor rotor. Journal of Engineering Thermophysics, 2019, 40(3): 505–512.
[23]
Sun W., Assessment of advanced rans turbulence models for prediction of complex flows in compressors. Chinese Journal of Aeronautics, 2023, 36(9): 162–177.
[24]
Cao T., Kanzaka T., Xu L., et al., Tip leakage flow instability in a centrifugal compressor. Journal of Engineering for Gas Turbines and Power, 2019, 143(4): V02BT44A003.
[25]
Zeinali M., Abbasi S., Aghdam A.H., Commencement and development processes of flow unsteadiness at tip clearance region of a low speed axial compressor rotor blade row. Periodica Polytechnica Mechanical Engineering, 2017, 61(4): 288–295.
[26]
Su W.T., Li X.B., Li F.C., et al., Comparisons of LES and RANS computations with piv experiments on a cylindrical cavity flow. Advances in Mechanical Engineering, 2013, 5: 592940.
[27]
Emmanuel S.O., Large-eddy simulation of flow in a compressor cascade with tip clearance using ansys cfx code. University College London, London, 2009.
[28]
Chen X., Björn K., Martin L., et al., Comparison of turbulence modeling for a compressor rotor at different tip clearances. AIAA Journal, 2021, 60(2): 1–13.
[29]
Zhao L., Wu D., Yuan Y., et al., Numerical simulation and noise analysis of a flow over an open cavity. Journal of Engineering Thermophysics, 2009, 30(11): 1859–1862.
[30]
Liu X., Willeke T., Herbst F., et al., A theory on the onset of acoustic resonance in a multistage compressor. Journal of Turbomachinery, 2018, 140(8): 0081003.
[31]
Pardowitz B., Tapken U., Sorge R., et al., Rotating instability in an annular cascade: Detailed analysis of the instationary flow phenomena. ASME Turbo Expo: Turbine Technical Conference and Exposition, San Antonio, United States, 2013.
[32]
Wu Z., An investigation on the onset mechanism of acoustic resonance in a multistage compressor. Shanghai Jiao Tong University, Shanghai, China, 2022.
