Effect of Geometric Fidelity on the Aerodynamics of a Swept Wing with Scalloped Ice Accretion
Author:
Affiliation:
1. Vantage Partners, LLC
2. NASA Glenn Research Center
3. University of Illinois, Urbana-Champaign
4. University of Washington, Seattle
Publisher
American Institute of Aeronautics and Astronautics
Reference28 articles.
1. Aerodynamic scaling experiments with simulated ice accretions
2. A Wind Tunnel Study of Icing Effects on a Business Jet Airfoil
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2. Investigating Iced Swept-Wing Flowfields Using a Swept Flat Plate and a Discontinuous Backward-Facing Step;AIAA AVIATION 2021 FORUM;2021-07-28
3. Comparison of Ice Shapes on Full-Chord and Truncated Swept Wing Models;AIAA AVIATION 2021 FORUM;2021-07-28
4. Effect of Geometric Fidelity on the Aerodynamics of a Swept Wing with Glaze Ice Accretion;AIAA AVIATION 2020 FORUM;2020-06-08
5. Effect of Spanwise Discontinuities on the Aerodynamics of a Swept Wing with Scalloped Ice Accretion;AIAA AVIATION 2020 FORUM;2020-06-08
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