Comparing Airfoils

GOE 572 AIRFOIL

GOE 571 AIRFOIL

GOE 572 AIRFOIL GOE 571 AIRFOIL
Thickness (%) 18.463 24.783
Camber (%) 8.285 9.796
Trailing Edge Angle (%) 32.273 38.642
Lower Surface Flatness 48.737 25.771
Leading Edge Radius (%) 4.130 7.622
Maximum Lift (CL) 1.938 2.248
Maximum Lift Angle-of-Attack (deg) 15.000 15.000
Maximum Lift-to-drag (L/D) 41.616 40.025
Lift at Maximum Lift-to-drag 0.786 1.105
Angle-of-Attack for Maximum Lift-to-drag (L/D) -0.500 -0.500