USA 49 AIRFOIL

Thickness: 7.2%
Camber: 1.7%
Trailing edge angle: 14.0o
Lower flatness: 20.0%
Leading edge radius: 1.9%
Efficiency: 29.2
Max CL: 0.886
Max CL angle: 13.0
Max L/D: 38.652
Max L/D angle: 3.5
Max L/D CL: 0.557
Stall angle: 3.5
Zero-lift angle: -1.0