NACA 8-H-12 AIRFOIL

Thickness: 11.9%
Camber: 3.5%
Trailing edge angle: 8.6o
Lower flatness: 14.5%
Leading edge radius: 2.7%
Efficiency: 33.3
Max CL: 1.056
Max CL angle: 15.0
Max L/D: 29.136
Max L/D angle: 7.5
Max L/D CL: 0.765
Stall angle: 8.5
Zero-lift angle: -0.5