3D Swept Hybrid Wing Design Method for Icing Wind Tunnel Tests
Author:
Affiliation:
1. University of Illinois, Urbana-Champaign
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2616
Reference40 articles.
1. Iced-airfoil aerodynamics
2. Effects of ice accretions on aircraft aerodynamics
3. Airfoil Ice-Accretion Aerodynamic Simulation
4. Effect of High-Fidelity Ice-Accretion Simulations on Full-Scale Airfoil Performance
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