Comparing Airfoils

GOE 423 AIRFOIL

AH 95-160

GOE 423 AIRFOIL AH 95-160
Thickness (%) 16.866 15.971
Camber (%) 5.017 5.495
Trailing Edge Angle (%) 26.667 15.107
Lower Surface Flatness 13.585 12.717
Leading Edge Radius (%) 4.093 3.003
Maximum Lift (CL) 1.615 1.860
Maximum Lift Angle-of-Attack (deg) 15.000 15.000
Maximum Lift-to-drag (L/D) 39.047 36.960
Lift at Maximum Lift-to-drag 1.103 0.639
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.500 -0.500