[1]
Mason J.G., Strapp W., Chow P., The ice particle threat to engines in flight. 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA, 2006.
[2]
Lynch F.T., Khodadoust A., Effects of ice accretions on aircraft aerodynamics. Progress in Aerospace Sciences, 2001, 37(1): 669–767.
[3]
Zilio C., Patricelli L., Aircraft anti-ice system: Evaluation of system performance with a new time dependent mathematical model. Applied Thermal Engineering, 2014, 63(1): 40–51.
[4]
Cao Y., Wu Z., Yuan S., et al., Aircraft flight characteristics in icing conditions. Progress in Aerospace Sciences, 2014, 74(1183): 963–979.
[5]
Jin W., Taghavi R., Computational study of the effects of ice accretions on the flowfields in the M2129 S-Duct inlets. 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA, 2008.
[6]
Oliver M.J., Validation ice crystal icing engine test in the propulsion systems laboratory at NASA Glenn Research Center. 6th AIAA Atmospheric and Space Environments Conference, Atlanta, USA, 2014.
[7]
Lian W., Zhao L., Xuan Y., et al., A modified spongy icing model considering the effect of droplets retention on the ice accretion process. Applied Thermal Engineering, 2018, 134: 54–61.
[8]
Özgen S., Uğur N., Görgϋlϋ I., et al., Ice accretion simulations on airfoils. Progress in Flight Physics, 2017, 9: 107–126.
[9]
Peng K., Xing T., Yi L., et al., Effects of turbulent dispersion on water droplet impingement based on statistics method. International Journal of Aeronautical and Space Sciences, 2018, 19(2): 330–339.
[10]
Isobe K., Suzuki M., Yamamoto M. Numerical investigation on super-cooled large droplet icing of fan rotor blade in jet engine. Journal of Thermal Science, 2014, 23: 432–437.
[11]
Potapczuk M.G., LEWICE/E - An Euler based ice accretion code. 30th Aerospace Sciences Meeting and Exhibit, Cleveland, USA, 1992.
[12]
Ruff G.A., Berkowitz B.M., Users manual for the NASA Lewis Ice Accretion Prediction Code (LEWICE). NASA Contractor Report 185129, 1990.
[13]
Morency F., Beaugendre H., Habashi W.G., FENSAP-ICE: a study of the effect of ice shapes on droplet impingement. 41st Aerospace Sciences Meeting and Exhibit, Reno, USA, 2003.
[14]
Hedde T., Guffond D., ONERA three-dimensional icing model. AIAA Journal, 1995, 33(6): 1038–1045.
[15]
Hedde T., Guffond D., Improvement of the ONERA 3D icing code, comparison with 3D experimental shapes. 31st Aerospace Sciences Meeting, Reno, USA, 1993.
[16]
Mingione G., Brandi V., Ice accretion prediction on multielement airfoils. Journal of Aircraft, 1998, 35(2): 240–246.
[17]
Potapczuk M.G., Gerhart P.M., Progress in development of a Navier-Stokes solver for evaluation of iced airfoil performance. 23rd Aerospace Sciences Meeting, Reno, USA, 1985.
[18]
Chi X., Li Y., Chen H., et al., A comparative study using CFD to predict iced airfoil aerodynamics. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA, 2005.
[19]
Anderson D.N., Hentschel D.B., Ruff G.A., Measurement and correlation of ice accretion roughness. 36th AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA, 1998.
[20]
Fortin G., Ilinca A., Laforte J.-L., et al., New roughness computation method and geometric accretion model for airfoil icing. Journal of Aircraft, 2012, 41(1): 119–127.
[21]
Maltezos D.G., Osonitsch C., Shaw R.J., et al., Particle trajectory computer program for icing analysis of axisymmetric bodies - A progress report. 25th AIAA Aerospace Sciences Meeting, Reno, USA, 1987.
[22]
Tong X., Luke E.A., Eulerian simulations of icing collection efficiency using a singularity diffusion model. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA, 2005.
[23]
Bourgault Y., Boutanios Z., Habashi W.G., Three-dimensional Eulerian approach to droplet impingement simulation using FENSAP-ICE. Part 1: Model, algorithm, and validation. Journal of Aircraft, 2000, 37(1): 95–103.
[24]
Honsek R., Habashi W.G., Aubé M.S., Eulerian modeling of in-flight icing due to supercooled large droplets. Journal of Aircraft, 2008, 45(4): 1290–1296.
[25]
Messinger B.L., Equilibrium temperature of an unheated icing surface as a function of air speed. Journal of the Aeronautical Sciences, 1953, 20(1): 29–42.
[26]
Li Y., Chen W., Yu X., Numerical simulation of aircraft icing based on the Szilder Random-Walk model. CSAA/IET International Conference on Aircraft Utility Systems, Guiyang, China, 2018.
[27]
Al-Khalil K.M., Keith T.G., DeWitt K.J., et al., Thermal analysis of engine inlet anti-icing systems. Journal of Propulsion and Power, 1990, 6(5): 628–634.
[28]
Tatar V., Aras H., An investigation on an anti-ice static vane of a gas turbine engine. Applied Thermal Engineering, 2017, 110: 1039–1050.
[29]
Yeoman K., Efficiency of a bleed air powered inlet icing protective system. 32nd Aerospace Sciences Meeting and Exhibit, Reno, USA, 1994.
[30]
Pellissier M., Habashi W.G., Pueyo A., Design optimization of hot-air anti-icing systems by FENSAP-ICE. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, USA, 2010.
[31]
Dong W., Zhu J., Zhou Z., et al., Heat transfer and temperature analysis of an aeroengine strut under icing conditions. Journal of Aircraft, 2015, 52(1): 216–225.
[32]
Ma H., Chen W., Zhang D., Numerical investigation of engine inlet vane hot-air anti-icing system with surface air film. International Journal of Modern Physics: Conference Series, 2012, 19: 331–340.
[33]
Lian W., Xuan Y., Experimental investigation on a novel aero-engine nose cone anti-icing system. Applied Thermal Engineering, 2017, 121: 1011–1021.
[34]
Beaugendre H., Morency F., Habashi W.G., FENSAP-ICE’s three-dimensional in-flight ice accretion module: ICE3D. Journal of Aircraft, 2003, 40(2): 239–247.
[35]
Farag K.A., Bragg M.B., Three dimensional droplet trajectory code for propellers of arbitrary geometry. 36th AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA, 1998.
[36]
Chu W., Li X., Ma T., et al., Study on hydraulic and thermal performance of printed circuit heat transfer surface with distributed airfoil fins. Applied Thermal Engineering, 2017, 114: 1309–1318.
[37]
Menter F.R., Two-equation eddy-viscosity turbulence models for engineering applications. AIAA Journal, 1994, 32(8): 1598–1605.
[38]
Heinrich A., Ross R., Zumwalt G., Aircraft icing handbook. Gates Learjet Corp., Wichita, KS, 1991.
[39]
Kind R.J., Potapczuk M.G., Feo A., et al., Experimental and computational simulation of in-flight icing phenomena. Progress in Aerospace Sciences, 1998, 34(2): 257–345.
[40]
Murilo D.M., Innocentini V.R., Salvinia A.M., Prediction of ceramic foams permeability using Ergun’s equation. Materials Research, 1999, 2(4): 283–289.
[41]
Shin J., Bond T.H., Results of an icing test on a NACA 0012 airfoil in the NASA Lewis Icing Research Tunnel. 30th Aerospace Sciences Meeting and Exhibit, Reno, USA, 1992.
[42]
Dong W., Zheng M., Zhu J., et al., Experimental investigation on anti-icing performance of an engine inlet strut. Journal of Propulsion and Power, 2017, 33(2): 379–386.
