ListarICMF - Artículos por tema "Wingtip Vortex"
Mostrando ítems 1-1 de 1
-
Comparison of the Aerodynamic Characteristics of the NACA0012 Airfoil at Low-to-Moderate Reynolds Numbers for any Aspect Ratio
(Scientific & Academic Publishing, 2016)This experimental work deais with the influence of the angle of attack (AoA) and the chord based Reynolds number (Rec) on the lift and drag coefficients for a low-aspect-ratio NACA0012 airfoil. In addition, we provide novel ...