USA 28 AIRFOIL

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Thickness: 13.2%
Camber: 3.8%
Trailing edge angle: 21.0o
Lower flatness: 81.6%
Leading edge radius: 3.4%
Max CL: 1.345
Max CL angle: 15.0
Max L/D: 62.786
Max L/D angle: 3.5
Max L/D CL: 0.882
Stall angle: 7.5
Zero-lift angle: -3.5