GOE 411 AIRFOIL

Thickness: 13.2%
Camber: 0.0%
Trailing edge angle: 20.4o
Lower flatness: 5.2%
Leading edge radius: 2.5%
Efficiency: 34.9
Max CL: 0.829
Max CL angle: 14.0
Max L/D: 38.549
Max L/D angle: 5.5
Max L/D CL: 0.656
Stall angle: 5.5
Zero-lift angle: 0.0