NASA SC(2)-0402 AIRFOIL

Thickness: 2.0%
Camber: 0.2%
Trailing edge angle: 5.1o
Lower flatness: 45.4%
Leading edge radius: 1.3%
Efficiency: 4.5
Max CL: 0.328
Max CL angle: 3.5
Max L/D: 20.159
Max L/D angle: 0.0
Max L/D CL: 0.155
Stall angle: 3.5
Zero-lift angle: -1.5