GOE 602 MOD. AIRFOIL

Thickness: 9.5%
Camber: 3.8%
Trailing edge angle: 11.8o
Lower flatness: 34.9%
Leading edge radius: 2.3%
Efficiency: 32.9
Max CL: 1.38
Max CL angle: 7.5
Max L/D: 71.727
Max L/D angle: 5.5
Max L/D CL: 1.164
Stall angle: 7.5
Zero-lift angle: -4.5