Development of a Second Generation In-Flight Icing Simulation Code
Author:
Affiliation:
1. Computational Fluid Dynamics Laboratory, Department of Mechanical Engineering, McGill University, 688 Sherbrooke Street West, 7th Floor, Montréal, Québec H3A 2S6 Canada
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/128/2/378/5645781/378_1.pdf
Reference30 articles.
1. Equilibrium Temperature of an Unheated Icing Surface as a Function of Air Speed;Messinger;J. Aeronaut. Sci.
2. MacArthur, C. D. , 1983, “Numerical Simulation of Airfoils Ice Accretion,” AIAA Paper No. 83-0112.
3. Ruff, G. A., and Berkowitz, M., 1990, “Users Manual for the NASA Lewis Ice Accretion Prediction Code (LEWICE),” NASA Contractor Report No. 185129.
4. ONERA Three-Dimensional Icing Model;Hedde;AIAA J.
5. Gent, R. W. , 1990, “TRAJICE2, A Combined Water Droplet and Ice Accretion Prediction Program for Aerofoil,” DRA Technical Report No. TR90054.
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