NASA/AMES 63A108 MOD C AIRFOIL

Thickness: 7.7%
Camber: 0.6%
Trailing edge angle: 19.7o
Lower flatness: 9.7%
Leading edge radius: 2.1%
Efficiency: 31.4
Max CL: 0.853
Max CL angle: 15.0
Max L/D: 32.705
Max L/D angle: 5.5
Max L/D CL: 0.629
Stall angle: 5.5
Zero-lift angle: 0.5