GOE 622 AIRFOIL

Thickness: 8.0%
Camber: 2.4%
Trailing edge angle: 15.4o
Lower flatness: 30.4%
Leading edge radius: 2.1%
Efficiency: 31.7
Max CL: 1.174
Max CL angle: 8.0
Max L/D: 58.441
Max L/D angle: 6.5
Max L/D CL: 1.021
Stall angle: 8.0
Zero-lift angle: -2.5