Comparing Airfoils

GOE 239 (MVA H.31) AIRFOIL

AH 79-100 B AIRFOIL

GOE 239 (MVA H.31) AIRFOIL AH 79-100 B AIRFOIL
Thickness (%) 11.201 10.026
Camber (%) 5.998 6.419
Trailing Edge Angle (%) 20.060 6.522
Lower Surface Flatness 13.998 10.985
Leading Edge Radius (%) 3.046 2.094
Maximum Lift (CL) 1.748 1.706
Maximum Lift Angle-of-Attack (deg) 10.500 7.000
Maximum Lift-to-drag (L/D) 69.764 79.930
Lift at Maximum Lift-to-drag 1.489 1.424
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 4.000