RG 12A-1.8/9.0 AIRFOIL

Thickness: 9.0%
Camber: 1.8%
Trailing edge angle: 9.1o
Lower flatness: 12.6%
Leading edge radius: 1.9%
Efficiency: 31.3
Max CL: 0.998
Max CL angle: 6.0
Max L/D: 49.099
Max L/D angle: 5.0
Max L/D CL: 0.89
Stall angle: 6.0
Zero-lift angle: -2.5