CLARK Y AIRFOIL

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Thickness: 11.7%
Camber: 3.4%
Trailing edge angle: 18.6o
Lower flatness: 71.8%
Leading edge radius: 1.2%
Max CL: 1.294
Max CL angle: 8.5
Max L/D: 56.51
Max L/D angle: 4.0
Max L/D CL: 0.879
Stall angle: 8.5
Zero-lift angle: -3.5