Comparing Airfoils

AH 93-K-130/15

AH 79-K-132/20

AH 93-K-130/15 AH 79-K-132/20
Thickness (%) 13.034 13.198
Camber (%) 3.582 3.679
Trailing Edge Angle (%) 16.345 12.663
Lower Surface Flatness 9.645 10.496
Leading Edge Radius (%) 2.167 2.183
Maximum Lift (CL) 1.057 1.151
Maximum Lift Angle-of-Attack (deg) 9.500 11.500
Maximum Lift-to-drag (L/D) 38.592 45.390
Lift at Maximum Lift-to-drag 0.914 0.984
Angle-of-Attack for Maximum Lift-to-drag (L/D) 8.000 6.000