Comparing Airfoils

BOEING 106 AIRFOIL

AH 79-K-132/20

BOEING 106 AIRFOIL AH 79-K-132/20
Thickness (%) 13.030 13.198
Camber (%) 3.316 3.679
Trailing Edge Angle (%) 17.663 12.663
Lower Surface Flatness 13.315 10.496
Leading Edge Radius (%) 3.206 2.183
Maximum Lift (CL) 1.413 1.151
Maximum Lift Angle-of-Attack (deg) 12.000 11.500
Maximum Lift-to-drag (L/D) 61.001 45.390
Lift at Maximum Lift-to-drag 0.733 0.984
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.000 6.000