The two-dimensional characteristics of airfoil NACA 0018 have been measured for Reynolds numbers between 0.15×10⁶ and 1.0×10⁶ to establish the lift, drag and moment curves that serve as input to ...
A numerical study is presented for high-lift airfoils suitable for racecar applications. The study includes the effect of ground clearance (distance between the airfoil and the ground), angle of ...
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