GOE 55 AIRFOIL

Thickness: 6.1%
Camber: 2.0%
Trailing edge angle: 19.3o
Lower flatness: 53.5%
Leading edge radius: 2.4%
Efficiency: 29.5
Max CL: 1.042
Max CL angle: 15.0
Max L/D: 26.951
Max L/D angle: 3.0
Max L/D CL: 0.525
Stall angle: 3.0
Zero-lift angle: -1.5