Comparing Experimental Ice Accretions on a Swept Wing with 3D Morphogenetic Simulations
Author:
Affiliation:
1. National Research Council, Ottawa, Ontario K1A 0R6, Canada
2. University of Alberta, Edmonton, Alberta T6G 2E3, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034879
Reference13 articles.
1. LWC and temperature effects on ice accretion formation on swept wings at glaze ice conditions
2. Ice accretion formations on a NACA 0012 swept wing tip in natural icing conditions
3. Current Experimental Basis for Modeling Ice Accretions on Swept Wings
4. BidwellC. S. “Icing Analysis of a Swept NACA 0012 Wing Using LEWICE3D Version 3.48,” AIAA Paper 2014-2200, 2014.
5. LEWICE Modeling of Swept Wing Ice Accretions
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