Comparing Airfoils

CLARK V AIRFOIL

AH 63-K-127/24

CLARK V AIRFOIL AH 63-K-127/24
Thickness (%) 11.630 12.704
Camber (%) 3.402 3.761
Trailing Edge Angle (%) 22.173 11.288
Lower Surface Flatness 18.333 12.628
Leading Edge Radius (%) 2.818 1.990
Maximum Lift (CL) 1.483 1.198
Maximum Lift Angle-of-Attack (deg) 10.000 10.500
Maximum Lift-to-drag (L/D) 62.075 47.838
Lift at Maximum Lift-to-drag 1.084 1.036
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 5.500