NASA SC(2)-0503 AIRFOIL

Thickness: 3.0%
Camber: 0.2%
Trailing edge angle: 6.5o
Lower flatness: 30.1%
Leading edge radius: 1.3%
Efficiency: 9.2
Max CL: 0.435
Max CL angle: 4.5
Max L/D: 23.855
Max L/D angle: 0.0
Max L/D CL: 0.217
Stall angle: 4.5
Zero-lift angle: -2.0