NACA 2-H-15 AIRFOIL

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Thickness: 14.7%
Camber: 4.5%
Trailing edge angle: 18.3o
Lower flatness: 87.1%
Leading edge radius: 3.3%
Max CL: 0.975
Max CL angle: 15.0
Max L/D: 21.219
Max L/D angle: 8.5
Max L/D CL: 0.654
Stall angle: 2.5
Zero-lift angle: 1.0