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Search results with tag "Naca 0015 airfoil"
LIFT, DRAG AND MOMENT OF A NACA 0015 AIRFOIL
smiller.sbyers.comThe NACA 0015 airfoil is relatively thin and symmetric. Because of this, thin airfoil theory was applied in order to determine the theoretical values of the lift, drag and moment coefficients. The following equation relates the coefficient of lift to the angle …
Numerical and Experimental Investigations of Lift …
www.ijmmm.orgenhancement of the air foil performance by using a plasma Abstract—In the present work, we studied numerical and experimentally analysis lift and drag performances of NACA 0015 airfoil at different attack angle at low Reynolds numbers