GOE 564 AIRFOIL

Thickness: 8.2%
Camber: 2.7%
Trailing edge angle: 13.6o
Lower flatness: 37.6%
Leading edge radius: 2.4%
Efficiency: 32.2
Max CL: 1.119
Max CL angle: 14.0
Max L/D: 64.244
Max L/D angle: 5.5
Max L/D CL: 0.989
Stall angle: 5.5
Zero-lift angle: -3.0