NASA SC(2)-0404 AIRFOIL

Thickness: 4.0%
Camber: 0.5%
Trailing edge angle: 7.4o
Lower flatness: 19.8%
Leading edge radius: 1.4%
Efficiency: 15.7
Max CL: 0.495
Max CL angle: 6.0
Max L/D: 18.529
Max L/D angle: 1.0
Max L/D CL: 0.242
Stall angle: 6.0
Zero-lift angle: -1.5