NACA 64-012A AIRFOIL

Thickness: 12.0%
Camber: 0.0%
Trailing edge angle: 15.2o
Lower flatness: 5.8%
Leading edge radius: 2.2%
Efficiency: 33.9
Max CL: 0.852
Max CL angle: 14.5
Max L/D: 33.309
Max L/D angle: 4.5
Max L/D CL: 0.534
Stall angle: 4.5
Zero-lift angle: 0.0