Comparing Airfoils

Eiffel 10 (Wright) - 1903 Wright Flyer airfoil

EPPLER 377 (MODIFIED) AIRFOIL

Eiffel 10 (Wright) - 1903 Wright Flyer airfoil EPPLER 377 (MODIFIED) AIRFOIL
Thickness (%) 2.730 3.706
Camber (%) 6.225 9.095
Trailing Edge Angle (%) 16.160 3.264
Lower Surface Flatness 5.986 3.694
Leading Edge Radius (%) 1.675 1.815
Maximum Lift (CL) 0.760 1.453
Maximum Lift Angle-of-Attack (deg) 10.000 9.500
Maximum Lift-to-drag (L/D) 36.558 103.649
Lift at Maximum Lift-to-drag 0.442 1.085
Angle-of-Attack for Maximum Lift-to-drag (L/D) -0.500 3.500