GOE 382 AIRFOIL

Thickness: 19.9%
Camber: 6.0%
Trailing edge angle: 25.7o
Lower flatness: 12.5%
Leading edge radius: 5.6%
Efficiency: 39.2
Max CL: 1.954
Max CL angle: 15.0
Max L/D: 36.373
Max L/D angle: 4.0
Max L/D CL: 0.996
Stall angle: -0.5
Zero-lift angle: -5.5