GOE 511 AIRFOIL

Thickness: 16.6%
Camber: 8.0%
Trailing edge angle: 30.4o
Lower flatness: 34.2%
Leading edge radius: 5.2%
Efficiency: 49.4
Max CL: 2.072
Max CL angle: 15.0
Max L/D: 50.039
Max L/D angle: 4.5
Max L/D CL: 1.307
Stall angle: -0.5
Zero-lift angle: -7.0