Unsteady Thermodynamic Computational Fluid Dynamics Simulations of Aircraft Wing Anti-Icing Operation
Author:
Affiliation:
1. University of Toronto, Toronto, Ontario M3H 5T6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.24122
Reference8 articles.
1. Three-Dimensional Eulerian Approach to Droplet Impingement Simulation Using FENSAP-ICE, Part 1: Model, Algorithm, and Validation
2. FENSAP-ICE's Three-Dimensional In-Flight Ice Accretion Module: ICE3D
3. Ice accretion calculations for a commercial transport using the LEWICE3D, ICEGRID3D and CMARC programs
4. Heat and Mass Transfer in the Case of Anti-Icing System Simulation
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