GOE 652 AIRFOIL

Thickness: 16.9%
Camber: 9.2%
Trailing edge angle: 4.0o
Lower flatness: 5.1%
Leading edge radius: 6.4%
Efficiency: 51.9
Max CL: 2.483
Max CL angle: 15.0
Max L/D: 61.298
Max L/D angle: 2.5
Max L/D CL: 1.44
Stall angle: -0.5
Zero-lift angle: -10.0