GOE 427 AIRFOIL

Thickness: 4.6%
Camber: 5.7%
Trailing edge angle: 9.5o
Lower flatness: 9.5%
Leading edge radius: 1.7%
Efficiency: 29.0
Max CL: 1.206
Max CL angle: 11.0
Max L/D: 59.987
Max L/D angle: -0.5
Max L/D CL: 0.586
Stall angle: 1.5
Zero-lift angle: -6.0