GOE 523 AIRFOIL

Thickness: 16.4%
Camber: 9.7%
Trailing edge angle: 8.6o
Lower flatness: 6.6%
Leading edge radius: 4.8%
Efficiency: 52.2
Max CL: 2.712
Max CL angle: 15.0
Max L/D: 83.087
Max L/D angle: -0.5
Max L/D CL: 1.467
Stall angle: -4.0
Zero-lift angle: -12.0