NACA M10 AIRFOIL

Thickness: 6.2%
Camber: 1.9%
Trailing edge angle: 17.2o
Lower flatness: 40.2%
Leading edge radius: 1.8%
Efficiency: 28.7
Max CL: 0.81
Max CL angle: 12.5
Max L/D: 30.065
Max L/D angle: 3.0
Max L/D CL: 0.483
Stall angle: 3.0
Zero-lift angle: -1.0