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Naca Airfoils: NACA 4412
15 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 4412 | 15 | 0.043 | 1.6 | 37.2 | -0.107 | 6,000,000 |
| NACA 4412 | 16 | 0.053 | 1.56 | 29.4 | -0.108 | 6,000,000 |
| NACA 4412 | 18 | 0.083 | 1.38 | 16.6 | -0.108 | 6,000,000 |
| NACA 4412 | 20 | 0.118 | 1.18 | 10 | -0.108 | 6,000,000 |
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