NASA SC(2)-1006 AIRFOIL

Thickness: 6.0%
Camber: 0.0%
Trailing edge angle: 9.5o
Lower flatness: 19.5%
Leading edge radius: 1.6%
Efficiency: 17.5
Max CL: 0.93
Max CL angle: 5.0
Max L/D: 77.271
Max L/D angle: -0.5
Max L/D CL: 0.796
Stall angle: -0.5
Zero-lift angle: -7.5