[1] Messinger, B. L. (1953). Equilibrium Temperature of an Unheated Icing Surface as a Function of Air Speed. J. Aeronaut. Sci., 1, 29–42.
[2] Anderson, D. N., & Tsao, J.-C. (2003). Evaluation and Validation of the Messinger Freezing Fraction.
Am. Inst. Aeronaut. Astronaut., 1218. doi: https://doi.org/10.2514/6.2003-1218
[3] Morency, F., Brahimi, M. T., Tezok, F., & Paraschivoiu, I. (1998). Hot Air Anti-Icing System Modelization in the Ice Prediction Code CANICE.
Am. Inst. Aeronaut. Astronaut., 192. doi:
https://doi.org/10.2514/6.1998-192
[4] Morency, F., Tezok, F., & Paraschivoiu, I. (2000). Heat and Mass Transfer in the Case of Anti-Icing System Simulation. J. Aircr., 37, 245–251.
[5] Hasanzadeh, K., Mosahebi, A., Laurendeau, E., & Paraschivoiu, I. (2013). Validation and Verification of Multi-Steps Icing Calculation Using CANICE2D-NS Code.
Am. Inst. Aeronaut. Astronaut., 2671. doi: https://doi.org/10.2514/6.2013-2671
[6] Fregeau, M., Saeed, F., & Paraschivoiu, I. (2004). Surface Heat Transfer Study for Ice Accretion and Anti-Icing Prediction in Three Dimension.
Am. Inst. Aeronaut. Astronaut., 2004–2063. doi: https://doi.org/10.2514/6.2004-63
[7] Silva, G. A. L., Silvares, O., & Jesus, E. J. G. (2007). Numerical Simulation of Airfoil Thermal Anti-Ice Operation Part 1: Mathematical Modeling. J. Aircr., 44, 627–634.
[8] Mingione, G., Brandi, V., & Esposito, B. (1997). Ice accretion prediction on multi-element airfoils.
Am. Inst. Aeronaut. Astronaut., 0177. doi:
https://doi.org/10.2514/6.1997-177
[9] Wright, B. W., Al-Khalil, K., & Miller, D. (1997). Validation of NASA thermal ice protection computer codes part2- lewice/thermal.
Am. Inst. Aeronaut. Astronaut., 0050. doi:
https://doi.org/10.2514/6.1997-50
[10] Trajice, R. W. G. (1994). A combined water droplet and ice accretion prediction code for aerofoils.
[11] Henry, R. (1992). Development of an electrothermal de-icing/anti-icing model.
Am. Inst. Aeronaut. Astronaut., 526. doi: https://doi.org/10.2514/6.1992-526
[12] AerTex. (n.d.). Aircraft Icing Analysis Codes. Retrieved from
http://www.aerotex.co.uk/analysis_codes/analysis_codes.htm [Accessed: 27 May 2026]
[13] BAE Systems. (n.d.). 3D Ice Prediction Tool - ICECREMO2. Retrieved from
http://www.baesystems.com/ProductsServices/ss_tes_atc_icecremo.html [Accessed: 27 May 2026]
[14] Newmerical Technologies International. (2009). Fensap-ice in flight icing simulation system.
[15] Mingione, G., Barocco, M., Denti, E., & Francesco Bindi, G. (n.d.). (1997). FLIGHT IN ICING CONDITIONS SUMMARY.
[16] Gelder, T. F., Lewis, J. P., & Koutz, S. L. (1953). Icing Protection for a Turbojet Transport Airplane: Heating Requirements, Methods of Protection, and Performance Penalties.
[17] Gray, V. H. (1952). Simple Graphical Solution on Heat-Transfer and Evaporation from Surface Heated to prevent Icing.
[18] Society of Automotive Engineers. (1969). SAE Aerospace Applied Thermodynamics Manual (2nd ed.). New York: Society of Automotive Engineers.
[19] Bergman, T. L., Lavine, A. S., Incropera, F. P., & Dewitt, D. P. (2011). Fundamentals of Heat and Mass Transfer (7th ed.). JOHN WILEY & SONS, INC.
[20] Hardy, J. K. (1945). Kinetic Temperature of Wet Surfaces. A Method of Calculating the Amount of Alcohol Required to Prevent Ice, and the Derivation of the Psychrometric Equation.
[21] Boelter, L. M. K., Martinelli, R. C., Romie, F. E., & Morrin, E. H. (1945). An Investigation of Aircraft Heaters. XVIII.- A Design Manual for Exhaust Gas and Air Heat Exchangers.