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Naca Airfoils: NACA 2412
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 2412 | 15 | 0.04 | 1.43 | 35.8 | -0.058 | 6,000,000 |
| NACA 2412 | 16 | 0.05 | 1.4 | 28 | -0.059 | 6,000,000 |
| NACA 2412 | 18 | 0.078 | 1.22 | 15.6 | -0.06 | 6,000,000 |
| NACA 2412 | 20 | 0.112 | 1.05 | 9.4 | -0.06 | 6,000,000 |
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