[1] Pan T., Yan J., Yan Z., Sun D., Li Q., Experiment investigation on the effect of inlet circumferential non-uniformity on the stall behaviours in a transonic axial compressor with axisymmetric stall precursor. Aerospace Science and Technology, 2022, 128: 107781.
[2] Li J., Du J., Liu Y., Zhang H., Nie C., Effect of inlet radial distortion on aerodynamic stability in a multi-stage axial flow compressor. Aerospace Science and Technology, 2020, 105: 105886.
[3] Davis J.R.M., Parametric investigation into the combined effects of pressure and temperature distortion on compression system stability. 27th Joint Propulsion Conference, Sacramento, America, 1991, Paper No. AIAA-91-1895. DOI: 10.2514/6.1991-1895
[4] Gannon A.J., Hobson G.V., Hedges C.R., Descovich G.L., Investigation and prediction of steam-induced stall-margin reduction in two transonic rotor fans. Journal of Fluids Engineering, 2014, 136(11): 111101–111110.
[5] Mehalic C., Effect of spatial inlet temperature and pressure distortion on turbofan engine stability. 24th Joint Propulsion Conference, Boston, America, 1988, Paper No. AIAA-88-3016. DOI: 10.2514/6.1988-3016
[6] Das D.K., Trippi A., Peacock R.E., Unsteady response of an axial flow compressor to planar temperaturetransients. Journal of Aircraft, 1985, 22(1): 11–18.
[7] Moore F.K., Greitzer E., A theory of post-stall transients in axial compression systems: part II―application. Journal of Engineering for Gas Turbines and Power, 1986, 108(2): 231–239.
[8] Moore F.K., Greitzer E., A theory of post-stall transients in axial compression systems: part I―development of equations. Journal of Engineering for Gas Turbines and Power, 1986, 108(1): 68–76.
[9] Hynes T.P., Greitzer E.M., A method for assessing effects of circumferential flow distortion on compressor stability. Journal of Turbomachinery, 1987, 109(3): 371–379.
[10] Lin P., Wang C., Wang Y., A high-order model of rotating stall in axial compressors with inlet distortion. Chinese Journal of Aeronautics, 2017, 30(3): 898–906.
[11] Emmons H., Pearson C., Grant H., Compressor surge and stall propogation. Transaction of ASME, 1955, 77(4): 455–467.
[12] Nenni J.P., Ludwig G.R., A theory to predict the inception of rotating stall in axial flow compressors. AlAA 7th Fluid and Plasma Dynamics Conference, Palo Alto, America, 1974, Paper No.74-528. DOI: 10.2514/6.1974-528
[13] Bonnaure L.P., Modelling high speed multistage compressor stability. Massachusetts Institute of Technology, Cambridge, Massachusetts, 1991.
[14] Sun X.F., On the relation between the inception of rotating stall and casing treatment. 32nd Joint Propulsion Conference and Exhibit, Lake Buena Vista, Florida, 1996, Paper No. 96-2579. DOI: 10.2514/6.1996-2579
[15] Cheng F.J., Sun D.K., Xu D., Sun X.F., Prediction of stall inception in multi-stage compressors based on an eigenvalue approach. Science China Technological Sciences, 2017, 60(8): 1132–1143.
[16] Sun X., Sun D., Yu W., A model to predict stall inception of transonic axial flow fan/compressors. Chinese Journal of Aeronautics, 2011, 24(6): 687–700.
[17] Wang D., Huang X., Solution stabilization and convergence acceleration for the harmonic balance equation system. Journal of Engineering for Gas Turbines and Power, 2017, 139(9): 92503–92512.
[18] Sun D., Li J., Dong X., Xu R., Sun X., Foam-metal casing treatment on an axial flow compressor: stability improvement and noise reduction. Journal of Turbomachinery, 2022, 144(1): 11003–11015.
[19] Ning F., Map: a cfd package for turbomachinery flow simulation and aerodynamic design optimization. ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Düsseldorf, Germany, 2014, Paper No. GT2014-26515. DOI: 10.1115/GT2014-26515
[20] He C., Ma Y., Liu X., Sun D., Sun X., Aerodynamic instabilities of swept airfoil design in transonic axial-flow compressors. AIAA Journal, 2018, 56(5): 1878–1893.
[21] Ning W., He L., Computation of unsteady flows around oscillating blades using linear and nonlinear harmonic euler methods. Journal of Turbomachinery, 1998, 120(3): 508–514.
[22] He L., Ning W., Efficient approach for analysis of unsteady viscous flows in turbomachines. AIAA Journal, 1998, 36(11): 2005–2012.
[23] He L., Fourier modeling of steady and unsteady nonaxisymmetrical flows. Journal of Propulsion and Power, 2006, 22(1): 197–201.
[24] Sun H., Wang M., Wang Z., Magagnato F., Numerical investigation of surge prediction in a transonic axial compressor with a hybrid bdf/harmonic balance method. Aerospace Science and Technology, 2019, 90: 401–409.
[25] Du P., Ning F., Application of the harmonic balance method in simulating almost periodic turbomachinery flows. ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Düsseldorf, Germany, 2014, Paper No. GT2014-25457. DOI: 10.1115/GT2014-25457
[26] Schmid P.J., Dynamic mode decomposition of numerical and experimental data. Journal of Fluid Mechanics, 2010, 656: 5–28.
[27] Luong H.T., Wang Y., Han H.S., Sohn C.H., Combined applications of analytic methods for detection of combustion instability triggering. Aerospace Science and Technology, 2021, 118: 106994.
[28] Zhao M., Zhao Y., Liu Z., Dynamic mode decomposition analysis of flow characteristics of an airfoil with leading edge protuberances. Aerospace Science and Technology, 2020, 98: 105684.
[29] Taira K., Brunton S.L., Dawson S.T., Rowley C.W., Colonius T., McKeon B.J., Schmidt O.T., Gordeyev S., Theofilis V., Ukeiley L.S., Modal analysis of fluid flows: an overview. AIAA Journal, 2017, 55(12): 4013–4041.
[30] Hale A., Davis M., Dynamic turbine engine compressor code (dyntecc)-theory and capabilities. 28th Joint Propulsion Conference and Exhibit, Nashville, TN, 1992, Paper No. AIAA-92-3190. DOI: 10.2514/6.1992-3190
[31] Gorrell S.E., Yao J., Wadia A.R., High fidelity urans analysis of swirl generation and fan response to inlet distortion. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, 2008, Paper No. AIAA 2008-4985. DOI: 10.2514/6.2008-4985
