Comparing Airfoils

MH 115 11.06%

AH 79-100 B AIRFOIL

MH 115 11.06% AH 79-100 B AIRFOIL
Thickness (%) 11.065 10.026
Camber (%) 5.558 6.419
Trailing Edge Angle (%) 8.359 6.522
Lower Surface Flatness 19.174 10.985
Leading Edge Radius (%) 2.340 2.094
Maximum Lift (CL) 1.725 1.706
Maximum Lift Angle-of-Attack (deg) 10.000 7.000
Maximum Lift-to-drag (L/D) 107.008 79.930
Lift at Maximum Lift-to-drag 1.366 1.424
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.500 4.000