GOE 386 AIRFOIL

Thickness: 20.1%
Camber: 5.4%
Trailing edge angle: 29.7o
Lower flatness: 11.4%
Leading edge radius: 6.8%
Efficiency: 38.6
Max CL: 1.924
Max CL angle: 15.0
Max L/D: 38.384
Max L/D angle: 4.5
Max L/D CL: 1.081
Stall angle: -0.5
Zero-lift angle: -5.0