Frossling Number Assessment for Airfoil Under Fully Turbulent Flow Conditions
Author:
Affiliation:
1. University of Quebec in Chicoutimi, Chicoutimi, Quebec G7H 2B1, Canada
2. École de Technologie Supérieure, Montreal, Quebec H3C 1K3, Canada
Funder
Natural Sciences and Engineering Research Council of Canada
Consortium de Recherche et d'innovation en Aérospatiale au Québec
Bell Textron Canada Ltd
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.T6389
Reference30 articles.
1. GuffondD.BrunetL. “Validation du Programme Bidimensionnel de Capitation //Oce National D’Etudes et de Recherches Aerospatiales of Work,” ONERA RP, 1988.
2. FENSAP-ICE's Three-Dimensional In-Flight Ice Accretion Module: ICE3D
3. Anti-Icing System Simulation Using CANICE
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