NASA/LANGLEY NLF 0414F AIRFOIL

Thickness: 14.2%
Camber: 2.4%
Trailing edge angle: 7.3o
Lower flatness: 6.7%
Leading edge radius: 2.4%
Efficiency: 34.6
Max CL: 1.236
Max CL angle: 15.0
Max L/D: 37.431
Max L/D angle: 7.5
Max L/D CL: 1.033
Stall angle: -0.5
Zero-lift angle: -2.5