Effect of Spanwise Discontinuities on the Aerodynamics of a Swept Wing with Scalloped Ice Accretion
Author:
Affiliation:
1. University of Illinois, Urbana-Champaign
2. University of Washington, Seattle
Publisher
American Institute of Aeronautics and Astronautics
Reference43 articles.
1. Iced-airfoil aerodynamics
2. Computational and Experimental Ice Accretions of Large Swept Wings in the Icing Research Tunnel
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2. Aerodynamic Simulation of Artificial Scallop Ice Shapes on NACA 23012 Airfoil;AIAA SCITECH 2022 Forum;2022-01-03
3. Investigating Iced Swept-Wing Flowfields Using a Swept Flat Plate and a Discontinuous Backward-Facing Step;AIAA AVIATION 2021 FORUM;2021-07-28
4. Comparison of Ice Shapes on Full-Chord and Truncated Swept Wing Models;AIAA AVIATION 2021 FORUM;2021-07-28
5. Effect of Geometric Fidelity on the Aerodynamics of a Swept Wing with Glaze Ice Accretion;AIAA AVIATION 2020 FORUM;2020-06-08
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