[1]
Willems F., De Jager B., Modeling and control of rotating stall and surge: An overview. Proceedings of the 1998 IEEE International Conference on Control Applications, 1998. DOI: 10.1109/CCA.1998.728438.
[2]
Kirn K.H., Fleeter S., Compressor unsteady aerodynamic response to rotating stall and surge excitations. Journal of Propulsion and Power, 1994, 10(5): 698–708.
[3]
Langston L.S., Stall and surge are endemic scourges of jet engine and gas turbine operation. Mechanical Engineering, 2017, 139(4): 36–41.
[4]
Huang W., Huang X.H., Development of aero-engine surge active control. Aeronautical Science & Technology, 2013, 1: 68–73.
[5]
Ucer A.S., Stow P., Hirsch C., et al., Thermodynamics and fluid mechanics of turbomachinery. Journal of Turbomachinery, 1987, 109(3): 453–453.
[6]
Tavakoli S., Griffin I., Fleming P., An overview of compressor instabilities: basic concepts and control. IFAC Proceedings Volumes, Journal of Engineering for Gas Turbines and Power, 2004, 37(6): 523–528.
[7]
Mazzawy R.S., Surge-induced structural loads in gas turbines. Journal of Engineering for Gas Turbines and Power, 1980, 102(1): 162–168.
[8]
Munari E., Morini M., Pinelli M., Brun K., Simons S., Kurz R., A new index to evaluate the potential damage of a surge event: the surge severity coefficient. Journal of Engineering for Gas Turbines and Power, 2019, 141: 031017. DOI: 10.1115/GT2018-76185.
[9]
Zhao F., Dodds J., Vahdati M., Flow physics during surge and recovery of a multi-stage high-speed compressor. Journal of Turbomachinery, 2021, 143(6): 1–29.
[10]
Marshall F.L., Prediction of inlet duct overpressures resulting from engine surge. Journal of Aircraft, 1973, 10(5): 274–278.
[11]
Greitzer E.M., Surge and rotating stall in axial flow compressors—Part I: Theoretical compression system model. Journal of Engineering for Power, 1976, 98(2): 190–198.
[12]
Greitzer E.M., Surge and rotating stall in axial flow compressors—Part II: experimental results and comparison with theory. Journal of engineering for power, 1976, 98(2): 199–211.
[13]
Moore F.K., Greitzer E.M., 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.
[14]
Greitzer E.M., Moore F.K., 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.
[15]
Shahriyari M., Khaleghi H., Heinrich M., A model for predicting post-stall behavior of axial compressors. Journal of Applied Fluid Mechanics, 2020, 14(3): 897–908.
[16]
Tucci L., Ferlauto M., Analysis and simulation of instabilities in axial compressors: engine model integration. Politecnico di Torino, Italia, 2020.
[17]
Drummond C., Davison C.R., Improved compressor maps using approximate solutions to the moore-greitzer model. Proceedings of the ASME Turbo Expo, 2009. DOI: 10.1115/GT2009-60148.
[18]
Bitikofer C., Schoen M.P., Li J.C., Lin F., Characteristic Moore-Greitzer model parameter identification for a one stage axial compressor system. American Control Conference, IEEE, 2017, pp. 164–169.
DOI: 10.23919/ACC.2017.7962948
[19]
Teramoto S.J.C.f.T.R., Annual Research Briefs., Analysis of the entire surge cycle of a multi-stage high-speed compressor. Stanford University, Stanford, CA, 2008.
[20]
Backi, C.J., Gravdahl J.T., Grøtli E.I., Nonlinear observer design for a Greitzer compressor model. 21st Mediterranean Conference on Control and Automation, IEEE, 2013, pp. 1457–1463.
DOI: 10.1109/MED.2013.6608913
[21]
Sari G., Akhrif O., Saydy L., Qualitative analysis of an axial compressor model with non-constant speed. ASME Power Conference, 2011, 1(1): 515–524.
[22]
Liu X., Zhou Y., Sun X., Sun D., Calculation of flow instability inception in high speed axial compressors based on an eigenvalue theory. Journal of Turbomachinery, 2015, 137(6): 061007.
[23]
Xu J., Chen Z., Effects of delay on surge in axial compressors. Scientia Sinica Physica, Mechanica & Astronomica, 2013, 43(4): 380.
[24]
Hu J., Fottner L., A new simplified model of post stall transients in axial compression systems. Journal of Thermal Science, 1999, 8(3): 176–189.
[25]
Davis Jr M.W., O'Brien W.F., Stage-by-stage poststall compression system modeling technique. Journal of Propulsion and Power, 1991, 7(6): 997–1005.
[26]
Sugiyama Y., Tabakoff W., Hamed A., J85 surge transient simulation. Journal of Propulsion and Power, 1989, 5(3): 375–381.
[27]
Nisitani H., Chen D.H., Body force method and its applications to numerical and theoretical problems in fracture and damage. Computational Mechanics, 1997, 19(6): 470–480.
[28]
Marble F.E., Hawthorne W.R., Three-dimensional flow in turbomachines. High Speed Aerodynamics and Jet Propulsion, 1964, 10(10): 83–166.
[29]
Xu L., Assessing viscous body forces for unsteady calculations. Journal of Turbomachinery, 2003, 125(3): 425–432.
[30]
Xu L., Hynes T.P., Denton J.D., Towards long length scale unsteady modelling in turbomachines. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 2003, 217(1): 75–82.
[31]
Longley J.P., Calculating stall and surge transients. Turbo Expo: Power for Land, Sea, and Air, 2007, 47950: 125–136. DOI: 10.1115/GT2007-27378.
[32]
Righi M., Pachidis V., Könözsy L., Pawsey L.J.A.S., Three-dimensional through-flow modelling of axial flow compressor rotating stall and surge. Aerospace Science and Technology, 2018, 78: 271–279.
[33]
Righi M., Pachidis V., Könözsy L., Zhao F., Vahdati M., Three-dimensional low-order surge model for high-speed axial compressors. Journal of the Global Power and Propulsion Society, 2020, 4: 274–284.
[34]
Day I.J., Axial compressor performance during surge. Journal of Propulsion and Power, 1994, 10(3): 329–336.
[35]
Dodds J., Vahdati M., Rotating stall observations in a high speed compressor—Part I: Experimental study. Journal of Turbomachinery, 2015, 137(5): 051002.
[36]
Wang M., Sun H., Wang Z., Wang Y., Magagnato F., Luan Y., Numerical investigation of the effects of system volume and average mass flow on the surge characteristics of an axial compressor. Aerospace Science and Technology, 2020, 106: 106172.
[37]
Greitzer E.M., Some aerodynamic problems of aircraft engines: fifty years after-the 2007 IGTI scholar lecture. Journal of Turbomachinery, 2009, 131(3): 031101.
[38]
Hale A., O’Brien W., A three-dimensional Turbine Engine Analysis Compressor Code (TEACC) for steady-state inlet distortion. Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 1997, 78712: V004T16A005.
[39]
Chima R.V., A three-dimensional unsteady CFD model of compressor stability. Engineering, 2013.
[40]
Guo J., Hu J., Wang X., Xu R., A three-dimensional unsteady through-flow model for rotating stall in axial compressors. American Society of Mechanical Engineers, 2020. DOI: 10.1115/GT2020-16186.
[41]
Outa E., Kato D., Chiba K., An NS simulation of stall cell behavior in a 2-D compressor rotor-stator system at various loads. Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 1994, 78835: V001T01A093.
[42]
Crevel F., Gourdain N., Ottavy X.J.J.o.T., Numerical simulation of aerodynamic instabilities in a multistage high-speed high-pressure compressor on Its Test Rig—part II: deep surge. Journal of Turbomachinery, 2014, 136(10): 101004.
[43]
Lee K.-B., Wilson M., Vahdati M.J., Validation of a numerical model for predicting stalled flows in a low-speed fan—part I: Modification of Spalart-Allmaras turbulence model. Journal of Turbomachinery, 2018, 140(5): 051008.
[44]
Lee K.-B., Dodds J., Wilson M., Vahdati M., Validation of a numerical model for predicting stalled flows in a low-speed fan—Part II: Unsteady analysis. Journal of Turbomachinery, 2018, 140(5): 051009.
[45]
Giersch T., Numerical models for the vibration response of high pressure compressor rotors with validation for forced response and surge. 2018.
[46]
Niazi S., Numerical simulation of rotating stall and surge alleviation in axial compressors. Georgia Institute of Technology, Atlanta, America, 2000.
[47]
Dumas M., Vo H.D., Yu H., Post-surge load prediction for multi-stage compressors via CFD simulations. Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2015.
DOI: 10.1115/GT2015-42748.
[48]
Bonnaure L.P., Modelling high speed multistage compressor stability. Massachusetts Institute of Technology, 1991.
[49]
Vahdati M., Simpson G., Imregun M., Unsteady flow and aeroelasticity behavior of aeroengine core compressors during rotating stall and surge. Journal of Turbomachinery, 2008, 130(3): 031017.
[50]
Schoenenborn H., Breuer T., Aeroelasticity at reversed flow conditions—part II: application to compressor surge. Journal of Turbomachinery, 2012 134(6): 061031.
[51]
Schoenenborn H., de Vries M., Aeroelasticity at reversed flow conditions—Part III: reduction of surge loads by means of intentional mistuning. Journal of Turbomachinery, 2013, 135(4): 041009.
[52]
Crevel F., Gourdain N., Ottavy X., Numerical simulation of aerodynamic instabilities in a multistage high-speed high-pressure compressor on Its Test Rig—part II: deep surge. Journal of Turbomachinery, 2014, 136(10): 101004.
[53]
Courtiade N., Ottavy X., Experimental study of surge precursors in a high-speed multistage compressor. Journal of Turbomachinery, 2018. DOI: 10.1115/GT2018-75283.
[54]
Zhao F., Dodds J., Vahdati M., Post-stall behaviour of a multi-stage high speed compressor at off-design conditions. Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2018, 50992: V02AT45A005.
[55]
Moreno J., Dodds J., Sheaf C., Zhao F., Vahdati M., Aerodynamic loading considerations of three-shaft engine compression system during surge. Journal of Turbomachinery, 2018. DOI: 10.1115/GT2018-75052.
[56]
Huang P.X., Mazzawy R.S., Shock tube simulation of the transient surge phase inside an axial compressor. turbo expo: power for land, sea, and air. American Society of Mechanical Engineers, 2018, 50992: V02AT45A003.
[57]
de Laborderie J., Duchaine F., Gicque, L., Analysis of a high-pressure multistage axial compressor at off-design conditions with coarse large eddy simulations. 12th European Conference on Turbomachinery Fluid dynamics & Thermodynamics. European Turbomachinery Society, 2017.
[58]
Yamada K., Furukawa M., Tamura Y., Saito S., Matsuoka A., Nakayama K., Large-scale DES analysis of stall inception process in a multi-stage axial flow compressor. Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2016, 49729: V02DT44A021.
[59]
Arroyo C.P., Dombard J., Duchaine F., Gicquel L., Martin B., Odier N., Staffelbach G.J.J.o.t.G.P., Society P., Towards the large-eddy simulation of a full engine: integration of a 360 azimuthal degrees fan, compressor and combustion chamber. Part I: Methodology and initialisation. Journal of the Global Power and Propulsion Society, 2021, pp. 1–16. DOI: 10.33737/jgpps/133115.
[60]
Anand M., Medic G., Paliath U., Suder K.L., Malik M.R., Laskowski G.M., Vision 2030 Aircraft propulsion grand challenge problem: Full-engine CFD simulations with high geometric fidelity and physics accuracy. AIAA Scitech 2021 Forum, 2021, pp. 0956.
