GOE 123 AIRFOIL

Thickness: 5.4%
Camber: 5.7%
Trailing edge angle: 12.5o
Lower flatness: 9.3%
Leading edge radius: 2.0%
Efficiency: 32.0
Max CL: 1.349
Max CL angle: 13.5
Max L/D: 71.843
Max L/D angle: 3.0
Max L/D CL: 0.947
Stall angle: 3.0
Zero-lift angle: -5.0