GOE 113 AIRFOIL

Thickness: 6.6%
Camber: 3.1%
Trailing edge angle: 15.5o
Lower flatness: 163.2%
Leading edge radius: 1.7%
Efficiency: 29.9
Max CL: 1.133
Max CL angle: 7.0
Max L/D: 50.071
Max L/D angle: 6.0
Max L/D CL: 1.027
Stall angle: 7.0
Zero-lift angle: -3.0