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Numerical and Experimental Studies on the Aerodynamics of NACA64 and DU40 Airfoils at Low Reynolds Numbers

The aerodynamics of airfoils can be seen in a wide range of applications. To obtain the aerodynamic loads, geometrically-scaled airfoil sections are tested in wind tunnels. However, due to the limited space of the wind tunnel, the mismatch of Reynolds numbers may lead to different aerodynamic loads....

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Autors principals: Chieh-Hsun Wu, Jing-Zong Chen, Yuan-Lung Lo, Chung-Lin Fu
Format: Artigo
Idioma:Inglês
Publicat: MDPI AG 2023-01-01
Col·lecció:Applied Sciences
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Accés en línia:https://www.mdpi.com/2076-3417/13/3/1478
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