[1] Pantelidis K., Hall C., Reynolds number effects on the aerodynamics of compact axial compressors, Stockholm, Sweden, 2017.
[2] Horton H.P., A semi-empirical theory for the growth and bursting of laminar separation bubbles, Aeronautical Research Council, 1969.
[3] Arena A.V., Mueller T.J., Laminar separation, transition, and turbulent reattachment near the leading edge of airfoils. AIAA Journal, American Institute of Aeronautics and Astronautics, 1980, 18(7): 747–753.
[4] Tselepidakis D.P., Kim S., Modeling and prediction of the laminar leading-edge separation and transition in a blade-cascade flow. American Society of Mechanical Engineers Digital Collection, 1996.
[5] Li Z., Ju Y., Zhang C., Parallel large-eddy simulation of subsonic and transonic flows with transition in compressor cascade. Journal of Propulsion and Power, 2019, 35(6): 1163–1174.
[6] Li Z., Ju Y., Zhang C., Quasi-wall-resolved large eddy simulation of transitional flow in a transonic compressor rotor. Aerospace Science and Technology, 2022, 126: 107620.
[7] Zhang X., Hodson H., Combined effects of surface trips and unsteady wakes on the boundary layer development of an ultra-high-lift LP turbine blade. Journal of Turbomachinery, American Society of Mechanical Engineers Digital Collection, 2005, 127(3): 479–488.
[8] Zhou Y., Wang Z.J., Effects of surface roughness on separated and transitional flows over a wing. AIAA Journal, American Institute of Aeronautics and Astronautics, 2012, 50(3): 593–609.
[9] Satta F., Simoni D., Ubaldi M., Zunino P., Bertini F., Loading distribution effects on separated flow transition of ultra-high-lift turbine blades, Journal of Propulsion and Power. American Institute of Aeronautics and Astronautics, 2014, 30(3): 845–856.
[10] Wheeler A.P.S., Sofia A., Miller R.J., The effect of leading-edge geometry on wake interactions in compressors. Journal of Turbomachinery, 2009, 131(4): 041013.
[11] Zong H., Kotsonis M.F., Evolution and scaling of plasma synthetic jets. Journal of Fluid Mechanics, 2018, 837: 147–181.
[12] Thill C., Etches J., Bond I., Potter K., Weaver P., Morphing skins. The Aeronautical Journal, 2008, 112(1129): 117–139.
[13] Sudhi A., Elham A., Badrya C., Coupled boundary-layer suction and airfoil optimization for hybrid laminar flow control. AIAA Journal, American Institute of Aeronautics and Astronautics, 2021, 59(12): 5158–5173.
[14] Corsini A., Delibra G., Sheard A.G., The application of sinusoidal blade-leading edges in a fan-design methodology to improve stall resistance. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, IMECHE, 2014, 228(3): 255–271.
[15] Keerthi M.C., Rajeshwaran M.S., Kushari A., De A., Effect of leading-edge tubercles on compressor cascade performance. AIAA Journal, American Institute of Aeronautics and Astronautics, 2016, 54(3): 912–923.
[16] Keerthi M.C., Kushari A., De A., Kumar A., Experimental investigation of effects of leading-edge tubercles on compressor cascade performance. American Society of Mechanical Engineers Digital Collection, 2014.
https://doi.org/10.1115/GT2014-26242
[17] Wang Z., Zhuang M., Leading-edge serrations for performance improvement on a vertical-axis wind turbine at low tip-speed-ratios. Applied Energy, 2017, 208: 1184–1197.
[18] ANSYS CFX, Version 19.2, ANSYS CFX-solver theory guide, ANSYS, Inc., Canonsburg, PA, 2018.
[19] Nicoud F., Ducros F., Subgrid-scale stress modelling based on the square of the velocity gradient tensor. Flow. Turbulence and Combustion, 1999, 62(3): 183–200.
[20] Vanna F.D., Picano F., Benini E., A sharp-interface immersed boundary method for moving objects in compressible viscous flows. Computers & Fluids, 2020, 201: 104415.
[21] Celik I.B., Cehreli Z.N., Yavuz I., Index of resolution quality for large eddy simulations. Journal of Fluids Engineering, 2005, 127(5): 949–958.
[22] Boese M., Fottner L., Effects of riblets on the loss behavior of a highly loaded compressor cascade. American Society of Mechanical Engineers Digital Collection, 2009, pp. 743–750.
[23] Choudhry A., Arjomandi M., Kelso R., A study of long separation bubble on thick airfoils and its consequent effects. International Journal of Heat and Fluid Flow, 2015, 52: 84–96.
[24] Boiko A.V., Grek G.R., Dovgal A.V., Koslov V.V., The origin of turbulance in near-wall flows. Springer, Berlin Heidelberg New York, 2002.
[25] Lang M., Rist U., Wagner S., Investigations on controlled transition development in a laminar separation bubble by means of LDA and PIV. Experiments in Fluids, 2004, 36(1): 43–52.
[26] Walker G.J., Transitional flow on axial turbomachine blading. AIAA Journal, American Institute of Aeronautics and Astronautics, 1989, 27(5): 595–602.
[27] Joshua R.B., Numerical investigations of instability and transition in attached and separated shear layers. Carleton University, 2014.
[28] Yang Z., Voke P.R., Large-eddy simulation of boundary-layer separation and transition at a change of surface curvature. Journal of Fluid Mechanics, 2001, 439: 305–333.
[29] Sajadmanesh S.M., Mojaddam M., Mohseni A., Nikparto A., Numerical identification of separation bubble in an ultra-high-lift turbine cascade using URANS simulation and proper orthogonal decomposition. Aerospace Science and Technology, 2019, 93: 105329.
[30] Chen L., Liu C., Numerical study on mechanisms of second sweep and positive spikes in transitional flow on a flat plate. Computers & Fluids, 2011, 40(1): 28–41.
[31] Liu C., Wang Y., Yang Y., Duan Z., New omega vortex identification method. Science China Physics, Mechanics & Astronomy, 2016, 59(8): 684711.
[32] Dubief Y., Delcayre F., On coherent-vortex identification in turbulence. Journal of Turbulence, 2000, 1(1): 011.
[33] Dong X., Wang Y., Chen X., Dong Y., Zhang Y., Liu C., Determination of epsilon for Omega vortex identification method. Journal of Hydrodynamics, 2018, 30(4): 541–548.
[34] Wang M., Li Z., Yang C., Zhao S., Zhang Y., Lu X., Large eddy simulation of the separated flow transition on the suction surface of a high subsonic compressor airfoil. Physics of Fluids, American Institute of Physics, 2020, 32(3): 034110.
[35] Yarusevych S., Sullivan P.E., Kawall J.G., On vortex shedding from an airfoil in low-Reynolds-number flows. Journal of Fluid Mechanics, Cambridge University Press, 2009, 632: 245–271.
[36] Moser R.D., Rogers M.M., The three-dimensional evolution of a plane mixing layer: pairing and transition to turbulence. Journal of Fluid Mechanics, Cambridge University Press, 1993, 247: 275–320.
[37] Liu C., Chen L., Study of mechanism of ring-like vortex formation in late flow transition. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2010-1456
[38] Moore J., Shaffer D.M., Moore J.G., Reynolds stresses and dissipation mechanisms downstream of a turbine cascade. Journal of Turbomachinery, 1987, 109(2): 258–267.