GOE 559 AIRFOIL

Thickness: 11.1%
Camber: 3.4%
Trailing edge angle: 14.2o
Lower flatness: 16.1%
Leading edge radius: 1.5%
Efficiency: 25.9
Max CL: 0.883
Max CL angle: 9.0
Max L/D: 59.86
Max L/D angle: 3.5
Max L/D CL: 0.756
Stall angle: 3.5
Zero-lift angle: -3.0