Comparing Airfoils

MH 115 11.06%

AH 79-100 C AIRFOIL

MH 115 11.06% AH 79-100 C AIRFOIL
Thickness (%) 11.065 9.934
Camber (%) 5.558 6.699
Trailing Edge Angle (%) 8.359 11.524
Lower Surface Flatness 19.174 12.226
Leading Edge Radius (%) 2.340 2.185
Maximum Lift (CL) 1.725 1.650
Maximum Lift Angle-of-Attack (deg) 10.000 11.500
Maximum Lift-to-drag (L/D) 107.008 79.298
Lift at Maximum Lift-to-drag 1.366 1.435
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.500 4.000