NACA 64-110 AIRFOIL

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Thickness: 10.0%
Camber: 0.6%
Trailing edge angle: 7.7o
Lower flatness: 56.4%
Leading edge radius: 1.2%
Max CL: 0.805
Max CL angle: 12.5
Max L/D: 35.908
Max L/D angle: 3.5
Max L/D CL: 0.506
Stall angle: 3.5
Zero-lift angle: -0.5