GOE 444 AIRFOIL

Thickness: 5.6%
Camber: 0.0%
Trailing edge angle: 10.3o
Lower flatness: 12.3%
Leading edge radius: 1.5%
Efficiency: 24.6
Max CL: 0.515
Max CL angle: 10.5
Max L/D: 31.627
Max L/D angle: 3.5
Max L/D CL: 0.375
Stall angle: 3.5
Zero-lift angle: 0.0