Immersed Boundary Methodology for Multistep Ice Accretion Using a Level Set
Author:
Affiliation:
1. Polytechnique Montreal, Montreal, Quebec H3T 1J4, Canada
2. ONERA/Multi-Physics Department for Energy, University of Toulouse, F-31055 Toulouse, France
Funder
ONERA, the French Aerospace Lab
Natural Sciences and Engineering Research Council of Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036492
Reference37 articles.
1. WrightW. B. “User Manual for the NASA Glenn Ice Accretion Code LEWICE Version 2.2.2,” NASA CR 2002-211793, 2002, https://ntrs.nasa.gov/citations/20020080990.
2. Development of a Second Generation In-Flight Icing Simulation Code
3. Validation Methods and Results for a Two-Dimensional Ice Accretion Code
4. Ice Accretion Model on Multi-Element Airfoil
5. PoliMIce: A simulation framework for three-dimensional ice accretion
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