Eulerian Modeling of Supercooled Large Droplet Splashing and Bouncing

Author:

Bilodeau David R.1,Habashi Wagdi G.1,Fossati Marco1,Baruzzi Guido S.2

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

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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