Comparing Airfoils

GOE 633 AIRFOIL

AH 80-140

GOE 633 AIRFOIL AH 80-140
Thickness (%) 13.749 13.949
Camber (%) 3.932 4.349
Trailing Edge Angle (%) 15.893 13.195
Lower Surface Flatness 16.475 13.298
Leading Edge Radius (%) 4.005 2.925
Maximum Lift (CL) 1.459 1.433
Maximum Lift Angle-of-Attack (deg) 15.000 14.000
Maximum Lift-to-drag (L/D) 35.703 28.169
Lift at Maximum Lift-to-drag 0.805 0.962
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 8.000