Comparing Airfoils

MRC-16

AH 79-K-135/20 B

MRC-16 AH 79-K-135/20 B
Thickness (%) 13.900 13.486
Camber (%) 3.122 3.052
Trailing Edge Angle (%) 20.096 12.757
Lower Surface Flatness 8.366 8.532
Leading Edge Radius (%) 2.539 2.150
Maximum Lift (CL) 1.393 1.145
Maximum Lift Angle-of-Attack (deg) 11.500 12.500
Maximum Lift-to-drag (L/D) 50.490 38.690
Lift at Maximum Lift-to-drag 1.019 0.711
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 4.000