Naca Airfoils: NACA_4415
NACA airfoil aerodynamic data — lift coefficient, drag coefficient, moment coefficient, and lift-to-drag ratio as functions of angle of attack for standard NACA airfoil profiles
| airfoil id | angle of attack deg | Cd (dimensionless) | Cl (dimensionless) | Cl Cd (dimensionless) | Cm c4 (dimensionless) | reynolds number (dimensionless) |
|---|---|---|---|---|---|---|
| NACA_4415 | -10 | 0.017 | -0.57 | -33.5 | -0.072 | 6,000,000 |
| NACA_4415 | -8 | 0.0128 | -0.35 | -27.3 | -0.077 | 6,000,000 |
| NACA_4415 | -6 | 0.0095 | -0.12 | -12.6 | -0.082 | 6,000,000 |
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