GOE 587 AIRFOIL

Thickness: 5.8%
Camber: 3.0%
Trailing edge angle: 10.8o
Lower flatness: 50.0%
Leading edge radius: 1.6%
Efficiency: 26.7
Max CL: 0.844
Max CL angle: 11.0
Max L/D: 38.123
Max L/D angle: 2.0
Max L/D CL: 0.478
Stall angle: 2.0
Zero-lift angle: -2.0