International Journal of Rotating Machinery / 2015 / Article / Fig 1

Research Article

Effect of Reynolds Number on Aerodynamics of Airfoil with Gurney Flap

Figure 1

(a) Entire domain of the grid used. (b) Near surface grid and blocking near the airfoil surfaces. (c) Boundary layer elements near the leading and trailing edges of the airfoil.
(a)
(b)
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