GOE 571 AIRFOIL

Thickness: 24.8%
Camber: 9.8%
Trailing edge angle: 38.6o
Lower flatness: 25.8%
Leading edge radius: 7.6%
Efficiency: 45.6
Max CL: 2.248
Max CL angle: 15.0
Max L/D: 40.025
Max L/D angle: -0.5
Max L/D CL: 1.105
Stall angle: -0.5
Zero-lift angle: -8.5