Eulerian Modeling of In-Flight Icing Due to Supercooled Large Droplets
Author:
Affiliation:
1. McGill University, Montreal, Quebec H3A 2S6, Canada
2. Newmerical Technologies International, Montreal, Quebec H3A 2M7, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34541
Reference25 articles.
1. A finite element method study of Eulerian droplets impingement models
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