The Effect of Location and Shape of Vortex Generators on Aerodynamic Characteristics of a NACA 4415 Airfoil
This study examines the flow behavior and lift coefficient variations of a NACA 4415 airfoil using different vortex generator configurations.Experimental investigations are conducted in a subsonic wind tunnel at a Reynolds number of 1.8 mcclelland reclining sofa x 105.The airfoil is tested with two types of vortex generators, namely the dome vortex