Eulerian Modeling of Supercooled Large Droplet Splashing and Bouncing-Reference-Cited by-同舟云学术

Eulerian Modeling of Supercooled Large Droplet Splashing and Bouncing

Published:2015-09 Issue:5 Volume:52 Page:1611-1624
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

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

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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