Comparing Airfoils

MH 38 9.68%

AH 79-100 A AIRFOIL

MH 38 9.68% AH 79-100 A AIRFOIL
Thickness (%) 9.674 9.969
Camber (%) 3.913 3.644
Trailing Edge Angle (%) 5.698 7.194
Lower Surface Flatness 23.291 16.965
Leading Edge Radius (%) 1.935 2.107
Maximum Lift (CL) 1.100 1.227
Maximum Lift Angle-of-Attack (deg) 5.500 6.500
Maximum Lift-to-drag (L/D) 105.392 73.259
Lift at Maximum Lift-to-drag 1.046 1.040
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 4.500