Numerical Simulation of Rotorcraft In-Flight Icing and Shedding via a High-Fidelity Method

Author:

Morelli M.,Rausa A.,Bellosta T.,Guardone A.

Publisher

Springer International Publishing

Reference54 articles.

1. Anthony J, Habashi WG (2021) Helicopter rotor ice shedding and trajectory analyses in forward flight. J Aircr 58(5):1–17. https://doi.org/10.2514/1.C036043

2. Bain J, Sankar L, Egolf T, Flemming R, Kreeger R (2009) Progress towards modelling the effects of ice accretion on rotorcraft performance in hover and forward flight. In: 35th European Rotorcraft Forum, Hamburg, September 2009

3. Bain J, Deresz R, Sankar L, Egolf TA, Flemming R, Kreeger E (2011) Effects of icing on rotary wing loads and surface heat transfer. In: 49th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition, Orlando, January 2011, p 1100

4. Bellosta T, Parma G, Guardone A (2019) A robust 3D particle tracking solver for in-fight ice accretion using arbitrary precision arithmetic. In: VIII international conference on computational methods for coupled problems in science and engineering

5. Belte D (1981) Helicopter Icing Spray System (HISS) nozzle improvement evaluation. U.S. Army Aviation Engineering Flight Activity, Edwards Air Force Base, Los Angeles

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