NASA/LANGLEY RC08-64C AIRFOIL

Thickness: 8.0%
Camber: 1.0%
Trailing edge angle: 17.6o
Lower flatness: 10.8%
Leading edge radius: 1.8%
Efficiency: 27.5
Max CL: 0.711
Max CL angle: 12.0
Max L/D: 18.841
Max L/D angle: 1.5
Max L/D CL: 0.273
Stall angle: 1.5
Zero-lift angle: -0.5