NACA M23 AIRFOIL

Thickness: 8.1%
Camber: 6.3%
Trailing edge angle: 22.1o
Lower flatness: 13.2%
Leading edge radius: 2.1%
Efficiency: 33.9
Max CL: 1.197
Max CL angle: 15.0
Max L/D: 27.68
Max L/D angle: 4.5
Max L/D CL: 0.616
Stall angle: -0.5
Zero-lift angle: -2.5