New Roughness Computation Method and Geometric Accretion Model for Airfoil Icing

Recent developments are presented in wet and dry ice accretion simulation at the Anti-Icing Materials International Laboratory in a joint project with the Italian Aerospace Research Center. An analytical model is introduced to calculate the surface roughness and the remaining, runback, and shedding...

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Veröffentlicht in:Journal of aircraft 2004-01, Vol.41 (1), p.119-127
Hauptverfasser: Fortin, Guy, Ilinca, Adrian, Laforte, Jean-Louis, Brandi, Vincenzo
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Sprache:eng
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