GOE 477 AIRFOIL

Thickness: 10.0%
Camber: 4.9%
Trailing edge angle: 12.4o
Lower flatness: 38.5%
Leading edge radius: 3.0%
Efficiency: 38.9
Max CL: 1.653
Max CL angle: 12.5
Max L/D: 76.264
Max L/D angle: 6.0
Max L/D CL: 1.278
Stall angle: -0.5
Zero-lift angle: -5.0