NASA SC(2)-0406 AIRFOIL

Thickness: 6.0%
Camber: 0.3%
Trailing edge angle: 10.4o
Lower flatness: 12.8%
Leading edge radius: 1.6%
Efficiency: 26.5
Max CL: 0.664
Max CL angle: 9.5
Max L/D: 21.619
Max L/D angle: 2.0
Max L/D CL: 0.411
Stall angle: 2.0
Zero-lift angle: -1.5