Comparing Airfoils

GOE 115 (MVA MK.2) AIRFOIL

AH 79-100 A AIRFOIL

GOE 115 (MVA MK.2) AIRFOIL AH 79-100 A AIRFOIL
Thickness (%) 9.655 9.969
Camber (%) 3.727 3.644
Trailing Edge Angle (%) 10.443 7.194
Lower Surface Flatness 27.499 16.965
Leading Edge Radius (%) 2.113 2.107
Maximum Lift (CL) 1.103 1.227
Maximum Lift Angle-of-Attack (deg) 12.500 6.500
Maximum Lift-to-drag (L/D) 66.195 73.259
Lift at Maximum Lift-to-drag 0.717 1.040
Angle-of-Attack for Maximum Lift-to-drag (L/D) 2.500 4.500