GOE 494 AIRFOIL

Thickness: 4.9%
Camber: 5.1%
Trailing edge angle: 5.5o
Lower flatness: 9.2%
Leading edge radius: 1.7%
Efficiency: 28.1
Max CL: 1.144
Max CL angle: 10.0
Max L/D: 76.749
Max L/D angle: 1.5
Max L/D CL: 0.74
Stall angle: -0.5
Zero-lift angle: -5.5