USA 32 AIRFOIL

No description available

Thickness: 14.7%
Camber: 9.3%
Trailing edge angle: 27.9o
Lower flatness: 77.4%
Leading edge radius: 4.5%
Max CL: 2.313
Max CL angle: 14.0
Max L/D: 61.341
Max L/D angle: 0.5
Max L/D CL: 1.004
Stall angle: -0.5
Zero-lift angle: -8.5