This paper presents the results of an experimental and computational study of low-Reynolds number swept wing aerodynamics. This work has been conducted in preparation for icing effects on a swept wing. A complete abstract will be written for the final paper.
Low-Reynolds Number Aerodynamics of an 8.9 Percent Scale Semispan Swept Wing for Assessment of Icing Effects
AIAA Atmospheric and Space Environments Conference 2017 ; 2017 ; Denver, CO, United States
2017-06-05
Miscellaneous
No indication
English
Computations of Swept Wing Icing Aerodynamics
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