NACA 64-108 AIRFOIL

Thickness: 8.0%
Camber: 0.6%
Trailing edge angle: 4.7o
Lower flatness: 10.6%
Leading edge radius: 1.7%
Efficiency: 28.4
Max CL: 0.678
Max CL angle: 10.5
Max L/D: 21.702
Max L/D angle: 1.5
Max L/D CL: 0.269
Stall angle: 1.5
Zero-lift angle: -0.5