USA 27 mod. AIRFOIL

No description available

Thickness: 13.3%
Camber: 5.1%
Trailing edge angle: 24.0o
Lower flatness: 92.7%
Leading edge radius: 3.8%
Max CL: 1.667
Max CL angle: 14.5
Max L/D: 67.502
Max L/D angle: 1.5
Max L/D CL: 0.752
Stall angle: 6.0
Zero-lift angle: -4.5