Comparing Airfoils

NASA SC(2)-0706 AIRFOIL

EPPLER EA 8(-1)-006 AIRFOIL

NASA SC(2)-0706 AIRFOIL EPPLER EA 8(-1)-006 AIRFOIL
Thickness (%) 6.000 5.996
Camber (%) 0.376 0.000
Trailing Edge Angle (%) 9.383 8.236
Lower Surface Flatness 15.506 12.504
Leading Edge Radius (%) 1.618 1.797
Maximum Lift (CL) 0.819 0.695
Maximum Lift Angle-of-Attack (deg) 7.500 12.500
Maximum Lift-to-drag (L/D) 30.318 21.711
Lift at Maximum Lift-to-drag 0.469 0.230
Angle-of-Attack for Maximum Lift-to-drag (L/D) -0.500 2.000