Revisited Model for Supercooled Large Droplet Impact onto a Solid Surface
Author:
Affiliation:
1. ONERA—The French Aerospace Lab, F-31055 Toulouse, France
Funder
French Civil Aviation Authority
Seventh Framework Programme
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034092
Reference22 articles.
1. Validation Results for LEWICE 3.0
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3. HonsekR.HabashiW. G. “Fensap-Ice: Eulerian Modeling of Droplet Impingement in the SLD Regime of Aircraft Icing,” AIAA Paper 2006-0465, 2006.
4. Eulerian Modeling of In-Flight Icing Due to Supercooled Large Droplets
5. HospersJ.HoeijmakersH. W. M. “Numerical Simulation of SLD Ice Accretions,” SAE Technical Paper, Technical Rept. 2011.
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