Comparing Airfoils

EPPLER 682 AIRFOIL

AH 82-150 A

EPPLER 682 AIRFOIL AH 82-150 A
Thickness (%) 15.293 14.995
Camber (%) 3.024 3.278
Trailing Edge Angle (%) 10.772 10.121
Lower Surface Flatness 6.705 7.777
Leading Edge Radius (%) 2.386 2.244
Maximum Lift (CL) 1.310 1.265
Maximum Lift Angle-of-Attack (deg) 10.000 12.000
Maximum Lift-to-drag (L/D) 46.162 45.550
Lift at Maximum Lift-to-drag 1.062 0.929
Angle-of-Attack for Maximum Lift-to-drag (L/D) 7.000 4.500