NASA SC(2)-0012 AIRFOIL

Thickness: 12.0%
Camber: 0.0%
Trailing edge angle: 27.3o
Lower flatness: 5.6%
Leading edge radius: 2.8%
Efficiency: 33.8
Max CL: 0.97
Max CL angle: 15.0
Max L/D: 24.003
Max L/D angle: 5.5
Max L/D CL: 0.659
Stall angle: 5.5
Zero-lift angle: 0.0