Naca Airfoils: NACA_0018
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_0018 | -10 | 0.0155 | -1.07 | -69 | 0 | 6,000,000 |
| NACA_0018 | -8 | 0.0115 | -0.89 | -77.4 | 0 | 6,000,000 |
| NACA_0018 | -6 | 0.0085 | -0.68 | -80 | 0 | 6,000,000 |
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