Comparing Airfoils

NACA 8-H-12 AIRFOIL

AH 80-136

NACA 8-H-12 AIRFOIL AH 80-136
Thickness (%) 11.928 13.545
Camber (%) 3.509 3.397
Trailing Edge Angle (%) 8.554 8.297
Lower Surface Flatness 14.543 9.527
Leading Edge Radius (%) 2.681 2.211
Maximum Lift (CL) 1.056 1.015
Maximum Lift Angle-of-Attack (deg) 15.000 15.000
Maximum Lift-to-drag (L/D) 29.136 24.677
Lift at Maximum Lift-to-drag 0.765 0.783
Angle-of-Attack for Maximum Lift-to-drag (L/D) 7.500 8.500