FENSAP-ICE-Unsteady: Unified In-Flight Icing Simulation Methodology for Aircraft, Rotorcraft, and Jet Engines
Author:
Affiliation:
1. Newmerical Technologies International, Montreal, Quebec H3A 2M7, Canada
2. McGill University, Montreal, Quebec H3A 2S6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C000327
Reference21 articles.
1. ONERA three-dimensional icing model
2. Development of a Shallow-Water Icing Model in FENSAP-ICE
3. Validation Results of FENSAP-ICE at MHI
4. Beaugendre, H. "A PDE-Based 3D Approach to In-Flight Ice Accretion," Ph.D. Thesis,McGill Univ., Montreal, June 2003.
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