DYNAMIC STALL INVESTIGATION OF NACA4412 AIRFOIL - A VERTICAL AXIS WINDMILL WING

Energy vitalization is an important role in modern life, Vertical windmill is an engrossed field of design in modern renewable energy generation but due to limitation and scant knowledge in understanding the behavior of wing in dynamic stall condition selection of wing is not proposed yet. The present investigation aims to propose the behavior of NACA 4412 Airfoil in a dynamic stall condition. The creation of lift and drag coefficient on the wing is a dependent feature of the respective angle of inclination and its variable. This case study presented on NACA 4412 Airfoil is aimed of Scientists and Engineers to understand the correlation on pressure-CL & CD for the optimization and selection of wing.