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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Bibliographic Details

Published in:	Applied Sciences
Main Authors:	Chieh-Hsun Wu, Jing-Zong Chen, Yuan-Lung Lo, Chung-Lin Fu
Format:	Article
Language:	English
Published:	MDPI AG 2023-01-01
Subjects:	aerodynamics airfoils Reynolds number Vortex Particle Method wind tunnel experiments wind energy
Online Access:	https://www.mdpi.com/2076-3417/13/3/1478