GOE 124 (MVA H.4) AIRFOIL

Thickness: 7.9%
Camber: 5.5%
Trailing edge angle: 16.9o
Lower flatness: 12.3%
Leading edge radius: 2.4%
Efficiency: 38.3
Max CL: 1.532
Max CL angle: 10.5
Max L/D: 63.804
Max L/D angle: 5.0
Max L/D CL: 1.187
Stall angle: 10.5
Zero-lift angle: -5.0