USA 46 AIRFOIL

Thickness: 6.5%
Camber: 2.2%
Trailing edge angle: 6.4o
Lower flatness: 39.3%
Leading edge radius: 2.0%
Efficiency: 29.8
Max CL: 0.92
Max CL angle: 6.0
Max L/D: 56.701
Max L/D angle: 4.0
Max L/D CL: 0.739
Stall angle: 6.0
Zero-lift angle: -2.5