NASA SC(2)-0606 AIRFOIL

Thickness: 6.0%
Camber: 0.4%
Trailing edge angle: 10.3o
Lower flatness: 14.8%
Leading edge radius: 1.6%
Efficiency: 24.7
Max CL: 0.766
Max CL angle: 8.0
Max L/D: 25.958
Max L/D angle: 0.0
Max L/D CL: 0.41
Stall angle: 1.0
Zero-lift angle: -5.5