FX 63-120 AIRFOIL

Thickness: 12.0%
Camber: 5.2%
Trailing edge angle: 4.7o
Lower flatness: 14.8%
Leading edge radius: 2.9%
Efficiency: 52.6
Max CL: 1.963
Max CL angle: 9.0
Max L/D: 87.427
Max L/D angle: 2.0
Max L/D CL: 1.165
Stall angle: 9.0
Zero-lift angle: -7.5