Aerodynamic Characterization of Low-Aspect-Ratio Swept Wings at Re=400
AIAA SciTech Forum and Exposition ; 2022 ; San Diego, Calif.; Online
Fluid dynamics ; Volume 4 of 7 ; 2515-2523
2022
Conference paper
English
Study of Low-Aspect Ratio Swept and Oblique Wings
AIAA | 1975
|Transonic Limit Cycle Flutter of High-Aspect-Ratio Swept Wings
Online Contents | 2008
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