GOE 359 AIRFOIL

Thickness: 7.8%
Camber: 5.9%
Trailing edge angle: 15.1o
Lower flatness: 12.2%
Leading edge radius: 2.2%
Efficiency: 33.3
Max CL: 1.521
Max CL angle: 7.5
Max L/D: 71.486
Max L/D angle: 6.0
Max L/D CL: 1.35
Stall angle: 7.5
Zero-lift angle: -5.5