GOE 451 AIRFOIL

Thickness: 4.4%
Camber: 5.5%
Trailing edge angle: 6.1o
Lower flatness: 9.1%
Leading edge radius: 1.4%
Efficiency: 34.5
Max CL: 1.244
Max CL angle: 10.5
Max L/D: 338.184
Max L/D angle: -0.5
Max L/D CL: 0.6
Stall angle: -0.5
Zero-lift angle: -6.5