NASA SC(2)-0403 AIRFOIL

Thickness: 3.0%
Camber: 0.4%
Trailing edge angle: 6.3o
Lower flatness: 26.9%
Leading edge radius: 1.3%
Efficiency: 9.5
Max CL: 0.408
Max CL angle: 5.0
Max L/D: 19.368
Max L/D angle: 0.5
Max L/D CL: 0.196
Stall angle: 5.0
Zero-lift angle: -1.5