NASA/LANGLEY LS(1)-0013 AIRFOIL

Thickness: 12.8%
Camber: 0.0%
Trailing edge angle: 20.9o
Lower flatness: 5.6%
Leading edge radius: 2.8%
Efficiency: 34.2
Max CL: 0.977
Max CL angle: 15.0
Max L/D: 27.866
Max L/D angle: 7.0
Max L/D CL: 0.738
Stall angle: 7.0
Zero-lift angle: 0.0