Comparing Airfoils

AH 80-129

AH 79-K-132/20

AH 80-129 AH 79-K-132/20
Thickness (%) 12.862 13.198
Camber (%) 4.055 3.679
Trailing Edge Angle (%) 13.711 12.663
Lower Surface Flatness 12.701 10.496
Leading Edge Radius (%) 1.930 2.183
Maximum Lift (CL) 0.985 1.151
Maximum Lift Angle-of-Attack (deg) 10.500 11.500
Maximum Lift-to-drag (L/D) 39.259 45.390
Lift at Maximum Lift-to-drag 0.742 0.984
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 6.000