GOE 522 AIRFOIL

Thickness: 21.7%
Camber: 5.2%
Trailing edge angle: 21.0o
Lower flatness: 9.0%
Leading edge radius: 6.7%
Efficiency: 41.7
Max CL: 2.06
Max CL angle: 15.0
Max L/D: 47.147
Max L/D angle: 4.5
Max L/D CL: 1.203
Stall angle: -0.5
Zero-lift angle: -6.0