Coefficient of pressure distribution around airfoil at 50% of the wingspan, in one-phase flow: (a) AoA = 0 • ; (b) AoA = 16 • .

Coefficient of pressure distribution around airfoil at 50% of the wingspan, in one-phase flow: (a) AoA = 0 • ; (b) AoA = 16 • .

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The correlation between computational fluid dynamics (CFD) and experimental fluid dynamics (EFD) is crucial for the behavior prediction of aerodynamic bodies. This paper’s objective is twofold: (1) to develop a method that approaches commercial CFD codes and their link with EFD in a more efficient way, using a downscaled model, and (2) to investiga...

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