GOE 222 (MVA H.33) AIRFOIL

Thickness: 18.3%
Camber: 7.2%
Trailing edge angle: 21.8o
Lower flatness: 12.7%
Leading edge radius: 4.5%
Efficiency: 54.3
Max CL: 2.31
Max CL angle: 15.0
Max L/D: 55.237
Max L/D angle: 2.0
Max L/D CL: 1.362
Stall angle: -0.5
Zero-lift angle: -8.5