GOE 561 AIRFOIL

Thickness: 24.9%
Camber: 10.2%
Trailing edge angle: 42.7o
Lower flatness: 26.3%
Leading edge radius: 7.9%
Efficiency: 46.9
Max CL: 2.234
Max CL angle: 15.0
Max L/D: 40.466
Max L/D angle: -0.5
Max L/D CL: 1.09
Stall angle: -0.5
Zero-lift angle: -8.5