USA 50 AIRFOIL

Thickness: 7.0%
Camber: 1.9%
Trailing edge angle: 14.4o
Lower flatness: 27.1%
Leading edge radius: 1.8%
Efficiency: 28.8
Max CL: 0.922
Max CL angle: 6.0
Max L/D: 63.987
Max L/D angle: 3.5
Max L/D CL: 0.653
Stall angle: 6.0
Zero-lift angle: -2.0