Comparing Airfoils

MRC-20

AH 82-150 A

MRC-20 AH 82-150 A
Thickness (%) 15.559 14.995
Camber (%) 2.928 3.278
Trailing Edge Angle (%) 23.039 10.121
Lower Surface Flatness 7.160 7.777
Leading Edge Radius (%) 2.513 2.244
Maximum Lift (CL) 1.541 1.265
Maximum Lift Angle-of-Attack (deg) 12.000 12.000
Maximum Lift-to-drag (L/D) 52.672 45.550
Lift at Maximum Lift-to-drag 1.146 0.929
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.500 4.500