Naca Airfoils: NACA_4412
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 | -10 | 0.016 | -0.6 | -37.5 | -0.07 | 6,000,000 |
| NACA_4412 | -8 | 0.012 | -0.38 | -31.7 | -0.075 | 6,000,000 |
| NACA_4412 | -6 | 0.009 | -0.15 | -16.7 | -0.08 | 6,000,000 |
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