03.2 - Experimental Aerodynamics
EXPERIMENTAL INVESTIGATION OF WISHBONE VORTEX GENERATOR EFFECTS ON THE NACA 4412 AIRFOIL AT LOW REYNOLDS NUMBERS
D. Domínguez¹, F. Parra¹, D. López¹, A. García-Gutiérrez¹; ¹Universidad de León, Spain
This work focuses on the experimental characterization of the NACA 4412 airfoil in the low Reynolds number regime, as well as on assessing the impact of Vortex Generators (VG) on its aerodynamic performance. The data obtained in this experimental campaign will be incorporated into an open repository and the aim is to use the concept to design more efficient propellers.
DOI: 10.71945/icas2026_0232