BOEING 103 AIRFOIL

Thickness: 12.7%
Camber: 3.6%
Trailing edge angle: 20.7o
Lower flatness: 16.4%
Leading edge radius: 3.4%
Efficiency: 41.2
Max CL: 1.485
Max CL angle: 14.5
Max L/D: 59.803
Max L/D angle: 4.5
Max L/D CL: 1.02
Stall angle: 7.0
Zero-lift angle: -4.0