GOE 610-B MOD. AIRFOIL

Thickness: 7.6%
Camber: 5.7%
Trailing edge angle: 24.8o
Lower flatness: 12.0%
Leading edge radius: 2.1%
Efficiency: 33.5
Max CL: 1.657
Max CL angle: 9.0
Max L/D: 54.709
Max L/D angle: 6.5
Max L/D CL: 1.39
Stall angle: 9.0
Zero-lift angle: -5.5