GOE 518 AIRFOIL

Thickness: 17.9%
Camber: 7.3%
Trailing edge angle: 28.8o
Lower flatness: 28.4%
Leading edge radius: 5.4%
Efficiency: 49.4
Max CL: 2.096
Max CL angle: 15.0
Max L/D: 49.042
Max L/D angle: 4.0
Max L/D CL: 1.246
Stall angle: -0.5
Zero-lift angle: -7.0