Comparing Airfoils

OAF102 AIRFOIL

AH 79-100 A AIRFOIL

OAF102 AIRFOIL AH 79-100 A AIRFOIL
Thickness (%) 10.135 9.969
Camber (%) 3.613 3.644
Trailing Edge Angle (%) 22.085 7.194
Lower Surface Flatness 14.165 16.965
Leading Edge Radius (%) 2.190 2.107
Maximum Lift (CL) 1.031 1.227
Maximum Lift Angle-of-Attack (deg) 15.000 6.500
Maximum Lift-to-drag (L/D) 39.153 73.259
Lift at Maximum Lift-to-drag 0.741 1.040
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 4.500