GOE 410 AIRFOIL

Thickness: 15.9%
Camber: 0.0%
Trailing edge angle: 10.3o
Lower flatness: 5.4%
Leading edge radius: 4.5%
Efficiency: 37.9
Max CL: 1.039
Max CL angle: 15.0
Max L/D: 30.941
Max L/D angle: 6.5
Max L/D CL: 0.666
Stall angle: 9.0
Zero-lift angle: 0.0