USA-35B AIRFOIL

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Thickness: 11.6%
Camber: 3.2%
Trailing edge angle: 14.1o
Lower flatness: 94.2%
Leading edge radius: 3.5%
Max CL: 1.508
Max CL angle: 15.0
Max L/D: 53.015
Max L/D angle: 0.5
Max L/D CL: 0.731
Stall angle: 8.0
Zero-lift angle: -5.5