GOE 417A (GEW. PLATTE) AIRFOIL

Thickness: 3.1%
Camber: 5.9%
Trailing edge angle: 14.4o
Lower flatness: 6.1%
Leading edge radius: 1.8%
Efficiency: 29.5
Max CL: 1.23
Max CL angle: 13.0
Max L/D: 76.843
Max L/D angle: 1.5
Max L/D CL: 0.715
Stall angle: 2.5
Zero-lift angle: -5.0