[1] Zhang C., Research on the performance prediction model and aerodynamic design method of centrifugal compressors. University of Chinese Academy of Sciences (Institute of Engineering Thermophysics, Chinese Academy of Sciences), Beijing, China, 2020.
[2] Hu C., Yang C., Shi X., et al., Investigation of rotating stall in radial vaneless diffusers with asymmetric inflow. Aerospace Science and Technology, 2020, 96: 105546.
[3] Jenny P., Bidaut Y., Experimental determination of mechanical stress induced by rotating stall in unshrouded impellers of centrifugal compressors. Journal of Turbomachinery, 2017, 139(3): 031011.
[4] Kulak M., Grapow F., Liśkiewicz G., Recirculation zones during the centrifugal compressor surge cycle: CFD simulation. ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, 2020, 84089: V02CT35A044.
[5] Zhang C., Dong X., Liu X., et al., A method to select loss correlations for centrifugal compressor performance prediction. Aerospace Science and Technology, 2019, 93: 105335.
[6] Wu C.H., A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial, radial, and mixed-flow types. Transactions of the American Society of Mechanical Engineers, 1952, 74(8): 1363–1380.
[7] Shen Y., Investigation of compressor blade design based on the S2 flow field theory and performance analysis. Nanjing University of Aeronautics and Astronautics, 2016, Nanjing, China.
[8] Kim S.G., Lee J., Ahn Y., et al., CFD investigation of a centrifugal compressor derived from pump technology for supercritical carbon dioxide as a working fluid. The Journal of Supercritical Fluids, 2014, 86: 160–171.
[9] Wang M., Zhao X., Gao S., et al., Visualizing and understanding corrosion evolution beneath a condensed droplet using the multi-electrode array. Colloids and Surfaces A: Physicochemical and Engineering Aspects, 2024, 684: 133252.
[10] Zhang L., Yang Z., Sun E., et al., Numerical simulation study on influence of equation of state on internal flow field and performance of s-CO2 compressor. Journal of Thermal Science, 2024, 33(3): 888–898.
[11] Guo Z., Chen Y., Lu Y., et al., Application of the fast 3D simplified simulation method for the large CAP1400 nuclear island evaporator based on the coupled source term method. Energy, 2024, 299: 131465.
[12] Coppage J.E., Dallenbach F., Eichenberger H.P., Study of supersonic radial compressors for refrigeration and pressurization systems. WADC Technical Report 55-257, ASITA Document No. AD 110467, 1957.
[13] Dean R.C., Senoo Y., Rotating wakes in vaneless diffusers. Journal of Fluids Engineering, 1960, 82(3): 563–570.
[14] Japikse D., Centrifugal compressor design and performance, Concepts ETI, Wilder, VT, 1996.
[15] Liang Q., Zuo Z., Zhu Y., et al., Modification and validation of two zone modelin centrifugal compressor. Journal of Aerospace Power, 2017, 32(10): 2544–2552.
[16] Oh H.W., Yoon E.S., Chung M.K., An optimum set of loss models for performance prediction of centrifugal compressors. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 1997, 211: 331–338.
[17] VELáSQUEZ Elkin I.G., Determination of a suitable set of loss models for centrifugal compressor performance prediction. Chinese Journal of Aeronautics, 2017, 30(5): 1644–1650.
[18] Aungier R.H., Centrifugal compressors: a strategy for aerodynamic design and analysis, ASME Press, New York, 2000.
[19] Jansen W., A method for calculating the flow in a centrifugal impeller when entropy gradients are present. Royal Society Conference on Internal Aerodynamics (Turbomachinery), University of Cambridge, UK, July, 1967, pp. 133–146.
[20] Conrad O., Raif K., Wessels M., The calculation of performance maps for centrifugal compressors with vane-island diffusers. ASME Twenty-fifth Annual International Gas Turbine Conference and Twenty-Second Annual Fluids Engineering Conference on Performance Prediction of Centrifugal Pumps and Compressors, New Orleans, LA, 1997, pp. 135–147.
[21] Stanitz J.D., One-dimensional compressible flow in vaneless diffusers of radial-and mixed-flow centrifugal compressors, including effects of friction. NASA Technical Paper 2610, 1952.
[22] Sundström E., Kerres B., Sanz S., et al., On the assessment of centrifugal compressor performance parameters by theoretical and computational models. ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, Charlotte, North Carolina, USA, 2017, Article ID: V02CT44A029.
[23] Zhang L., Yang F., An G., et al., Investigation of a rotating stall in a supercritical CO2 centrifugal compressor. Physics of Fluids, 2024, 36(5): 054102.
[24] Khoshkalam N., Mojaddam M., Pullen K.R., Characterization of the performance of a turbocharger centrifugal compressor by component loss contributions. Energies, 2019, 12(14): 2711.
[25] Hu C., Geng K., Yang C., et al., Thermodynamics investigation and spike-stall identification based on energy loss of centrifugal compressor. International Journal of Heat and Mass Transfer, 2021, 166: 120693.
[26] Du Y., Yang C., Wang H., et al., One-dimensional optimization design and off-design operation strategy of centrifugal compressor for supercritical carbon dioxide Brayton cycle. Applied Thermal Engineering, 2021, 196: 117318.
[27] Zhang L., An G., Lang J., et al., Investigation of the unsteady flow mechanism in a centrifugal compressor adopted in the compressed carbon dioxide energy storage system. Journal of Energy Storage, 2024, 104: 114488.
[28] Chen H., Zhuge W., Zhang Y., et al., Effect of compressor inlet condition on supercritical carbon dioxide compressor performance. ASME Turbo Expo 2019, Turbomachinery Technical Conference and Exposition, Phoenix, Arizona, USA, 2019, Article ID: V009T38A012.
[29] Cho S.Y., Ahn K.Y., Lee Y.D., et al., Optimal design of a centrifugal compressor impeller using evolutionary algorithms. Mathematical Problems in Engineering, 2012, pp: 752931.
[30] Kim J.H., Choi J.H., Husain A., et al., Design optimization of a centrifugal compressor impeller by multi-objective genetic algorithm. ASME 2009 Fluids Engineering Division Summer Meeting, Vail, Colorado, USA, 2009, pp: 185–191.
[31] Shi L., Mao R., Wang B., et al., Vortex dynamics and associated turbulence production in the separated transitional flow and the wake at a moderate Reynolds number. Experimental Thermal and Fluid Science, 2023, 144(6): 110871.
[32] Shi L., Mao R., Ma H., et al., Flow structure and vortex dynamics of blade surface transitional flow in the near-tip region of a compressor cascade. Physics of Fluids, 2023, 35(9): 094102.
[33] Li J., Teng J., Zhu M., et al., Loss prediction of axial compressors using genetic algorithm-back propagation neural network in throughflow method. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2022, 236(8): 1577–1589.
[34] Wang W., Mo R., Zhang Y., Multi-objective aerodynamic optimization design method of compressor rotor based on Isight. Procedia Engineering, 2011, 15: 3699–3703.
[35] Xia W., Zhang Y., Yu H., et al., Aerodynamic design and multi-dimensional performance optimization of supercritical CO2 centrifugal compressor. Energy Conversion and Management, 2021, 248: 114810.
[36] Hathaway M.D., Chriss R.M., Strazisar A.J., et al., Laser anemometer measurements of the three-dimensional rotor flow field in the NASA low-speed centrifugal compressor. NASA Technical Paper 3527, 1995.
[37] Qi D., Principle of centrifugal compressor. Beijing Mechanical Industry Press, Beijing, 2018. (in Chinese)
[38] Benedict R.P., Carlucci N.A., Swetz S.D., Flow losses in abrupt enlargements and contractions. Journal of Engineering for Gas Turbines and Power, 1966, 88(1): 73–81.
[39] Wiesner F.J., A review of slip factors for centrifugal impellers. Journal of Engineering for Gas Turbines and Power, 1967, 89(4): 558–566.
[40] Johnston J.P., Dean Jr R.C., Losses in vaneless diffusers of centrifugal compressors and pumps: analysis, experiment, and design. Journal of Engineering for Gas Turbines and Power, 1966; 88(1): 49–60.
