BOEING 103 AIRFOIL

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Thickness: 12.7%
Camber: 3.6%
Trailing edge angle: 17.4o
Lower flatness: 88.3%
Leading edge radius: 3.1%
Max CL: 1.485
Max CL angle: 14.5
Max L/D: 59.803
Max L/D angle: 4.5
Max L/D CL: 1.02
Stall angle: 7.0
Zero-lift angle: -4.0