Comparing Airfoils

AH 93-K-130/15

AH 80-129

AH 93-K-130/15 AH 80-129
Thickness (%) 13.034 12.862
Camber (%) 3.582 4.055
Trailing Edge Angle (%) 16.345 13.711
Lower Surface Flatness 9.645 12.701
Leading Edge Radius (%) 2.167 1.930
Maximum Lift (CL) 1.057 0.985
Maximum Lift Angle-of-Attack (deg) 9.500 10.500
Maximum Lift-to-drag (L/D) 38.592 39.259
Lift at Maximum Lift-to-drag 0.914 0.742
Angle-of-Attack for Maximum Lift-to-drag (L/D) 8.000 5.000