NASA SC(2)-0710 AIRFOIL

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Thickness: 10.0%
Camber: 1.0%
Trailing edge angle: 13.6o
Lower flatness: 13.7%
Leading edge radius: 1.7%
Max CL: 1.139
Max CL angle: 12.0
Max L/D: 33.306
Max L/D angle: 2.0
Max L/D CL: 0.82
Stall angle: 2.0
Zero-lift angle: -4.5