NACA 64-008A AIRFOIL

Thickness: 8.0%
Camber: 0.0%
Trailing edge angle: 10.4o
Lower flatness: 8.7%
Leading edge radius: 1.7%
Efficiency: 28.2
Max CL: 0.599
Max CL angle: 11.0
Max L/D: 13.686
Max L/D angle: 1.5
Max L/D CL: 0.173
Stall angle: 1.5
Zero-lift angle: 0.0