Computational Investigation of Simulated Large-Droplet Ice Shapes on Airfoil Aerodynamics
Author:
Affiliation:
1. University of Illinois at Urbana – Champaign, Urbana, Illinois 61801
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2517
Reference23 articles.
1. Aircraft aerodynamic effects due to large droplet ice accretions
2. An experimental and computational investigation of spanwise-step-ice shapes on airfoil aerodynamics
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