NACA M2 AIRFOIL

Thickness: 8.0%
Camber: 0.0%
Trailing edge angle: 18.1o
Lower flatness: 9.9%
Leading edge radius: 2.2%
Efficiency: 31.0
Max CL: 0.759
Max CL angle: 14.5
Max L/D: 13.926
Max L/D angle: 2.0
Max L/D CL: 0.227
Stall angle: 2.0
Zero-lift angle: 0.0