Comparing Airfoils

MRC-20

AH 82-150 F

MRC-20 AH 82-150 F
Thickness (%) 15.559 14.991
Camber (%) 2.928 3.633
Trailing Edge Angle (%) 23.039 12.352
Lower Surface Flatness 7.160 7.815
Leading Edge Radius (%) 2.513 2.118
Maximum Lift (CL) 1.541 1.189
Maximum Lift Angle-of-Attack (deg) 12.000 11.000
Maximum Lift-to-drag (L/D) 52.672 39.119
Lift at Maximum Lift-to-drag 1.146 0.936
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.500 4.500