GOE 391 AIRFOIL

Thickness: 5.1%
Camber: 3.2%
Trailing edge angle: 11.3o
Lower flatness: 35.1%
Leading edge radius: 1.6%
Efficiency: 27.5
Max CL: 0.983
Max CL angle: 11.5
Max L/D: 55.958
Max L/D angle: 0.5
Max L/D CL: 0.409
Stall angle: 2.0
Zero-lift angle: -3.5