Research Article

An Integrated Method for Designing Airfoils Shapes

Table 1

Coefficients for determining the NACA 64418 and S809 airfoils.

AirfoilsNACA 64418S809

0.894821.47486
0.049600.04733
−0.35665−0.55641
−0.35445−0.65773
−0.02444−0.07436
−0.01001−0.05212