GOE 122 (MVA H.2) AIRFOIL

Thickness: 7.3%
Camber: 4.1%
Trailing edge angle: 13.4o
Lower flatness: 30.7%
Leading edge radius: 2.0%
Efficiency: 30.7
Max CL: 1.18
Max CL angle: 14.0
Max L/D: 53.711
Max L/D angle: 2.5
Max L/D CL: 0.675
Stall angle: 3.5
Zero-lift angle: -3.5