NASA SC(2)-0706 AIRFOIL

Thickness: 6.0%
Camber: 0.4%
Trailing edge angle: 9.4o
Lower flatness: 15.5%
Leading edge radius: 1.6%
Efficiency: 23.3
Max CL: 0.819
Max CL angle: 7.5
Max L/D: 30.318
Max L/D angle: -0.5
Max L/D CL: 0.469
Stall angle: 0.5
Zero-lift angle: -4.5