Comparing Airfoils

EPPLER 654 AIRFOIL

AH 95-160

EPPLER 654 AIRFOIL AH 95-160
Thickness (%) 17.160 15.971
Camber (%) 4.825 5.495
Trailing Edge Angle (%) 9.170 15.107
Lower Surface Flatness 8.415 12.717
Leading Edge Radius (%) 2.902 3.003
Maximum Lift (CL) 1.838 1.860
Maximum Lift Angle-of-Attack (deg) 14.500 15.000
Maximum Lift-to-drag (L/D) 45.637 36.960
Lift at Maximum Lift-to-drag 0.694 0.639
Angle-of-Attack for Maximum Lift-to-drag (L/D) -0.500 -0.500