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Naca Airfoils: NACA 4415
10 to 20
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 | 0.0165 | 1.48 | 89.7 | -0.107 | 6,000,000 |
| NACA 4415 | 12 | 0.0235 | 1.61 | 68.5 | -0.108 | 6,000,000 |
| NACA 4415 | 14 | 0.036 | 1.68 | 46.7 | -0.109 | 6,000,000 |
| NACA 4415 | 16 | 0.055 | 1.65 | 30 | -0.109 | 6,000,000 |
| NACA 4415 | 18 | 0.086 | 1.48 | 17.2 | -0.109 | 6,000,000 |
| NACA 4415 | 20 | 0.122 | 1.27 | 10.4 | -0.109 | 6,000,000 |
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