GOE 239 (MVA H.31) AIRFOIL

Thickness: 11.2%
Camber: 6.0%
Trailing edge angle: 20.1o
Lower flatness: 14.0%
Leading edge radius: 3.0%
Efficiency: 52.2
Max CL: 1.748
Max CL angle: 10.5
Max L/D: 69.764
Max L/D angle: 6.0
Max L/D CL: 1.489
Stall angle: 6.0
Zero-lift angle: -6.5