Effects of Wing-Cuff on NACA 23015 Aerodynamic Performances
The main subject of this work is the numerical study control of flow separation on a NACA 23015 airfoil by using wing cuff.This last is a leading edge modification done to the wing.The modification consists of a slight extension of the chord on the outboard section of the wings.Different numerical veste a frange sandro cases are considered for the