USA 45 AIRFOIL

Thickness: 14.4%
Camber: 4.1%
Trailing edge angle: 16.4o
Lower flatness: 13.5%
Leading edge radius: 3.6%
Efficiency: 35.6
Max CL: 1.477
Max CL angle: 15.0
Max L/D: 47.916
Max L/D angle: 2.0
Max L/D CL: 0.64
Stall angle: -0.606
Zero-lift angle: -3.0