GOE 456 AIRFOIL

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Thickness: 7.2%
Camber: 5.2%
Trailing edge angle: 9.8o
Lower flatness: 89.6%
Leading edge radius: 2.5%
Max CL: 1.35
Max CL angle: 6.5
Max L/D: 75.443
Max L/D angle: 4.5
Max L/D CL: 1.133
Stall angle: 6.5
Zero-lift angle: -5.5