Naca Airfoils: NACA_2412
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 | -10 | 0.0148 | -0.82 | -55.4 | -0.025 | 6,000,000 |
| NACA_2412 | -8 | 0.0108 | -0.61 | -56.5 | -0.03 | 6,000,000 |
| NACA_2412 | -6 | 0.008 | -0.4 | -50 | -0.035 | 6,000,000 |
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