Research Article
An Integrated Method for Designing Airfoils Shapes
Table 1
Coefficients for determining the NACA 64418 and S809 airfoils.
| Airfoils | NACA 64418 | S809 |
| | 0.89482 | 1.47486 | | 0.04960 | 0.04733 | | −0.35665 | −0.55641 | | −0.35445 | −0.65773 | | −0.02444 | −0.07436 | | −0.01001 | −0.05212 |
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