Anti-Icing System Simulation Using CANICE
Author:
Affiliation:
1. Ecole Polytechnique de Montreal, Montreal, Quebec, H3C 3A7, Canada
2. Bombardier Aerospace, Dorval, Quebec, H4S 1Y9, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2541
Reference23 articles.
1. Equilibrium Temperature of an Unheated Icing Surface as a Function of Air Speed
2. Numerical simulation of airfoil ice accretion
3. Ice accretion on aircraft wings with thermodynamic effects
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