GOE 623 AIRFOIL

Thickness: 12.0%
Camber: 3.9%
Trailing edge angle: 21.5o
Lower flatness: 22.6%
Leading edge radius: 3.0%
Efficiency: 40.6
Max CL: 1.465
Max CL angle: 11.0
Max L/D: 52.716
Max L/D angle: 4.5
Max L/D CL: 0.981
Stall angle: 6.5
Zero-lift angle: -3.5