NACA M25 AIRFOIL

Thickness: 6.3%
Camber: 8.2%
Trailing edge angle: 18.6o
Lower flatness: 6.7%
Leading edge radius: 1.8%
Efficiency: 29.2
Max CL: 1.26
Max CL angle: 14.0
Max L/D: 32.791
Max L/D angle: 5.5
Max L/D CL: 0.818
Stall angle: -0.5
Zero-lift angle: -4.0