Eulerian Modeling of Supercooled Large Droplet Splashing and Bouncing
Author:
Affiliation:
1. CFD Laboratory, Department of Mechanical Engineering, McGill University, Montreal, Quebec H3A 2S6, Canada
2. R&D, 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.C033023
Reference24 articles.
1. Aircraft icing
2. NTSB, “In-Flight Icing Encounter and Loss of Control,” National Transportation Safety Board AAR-96/01, Vol. 2, Washington, D.C. Oct. 1994.
3. HonsekR. “Development of a Three-Dimensional Eulerian Model of Droplet–Wall Interaction Mechanisms,” M.E. Thesis, Mechanical Engineering Dept., McGill Univ., Montreal, QC, 2005.
4. Development of a Shallow-Water Icing Model in FENSAP-ICE
5. Further Refinement of the LEWICE SLD Model
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