BOEING 106 AIRFOIL

Thickness: 13.0%
Camber: 3.3%
Trailing edge angle: 17.7o
Lower flatness: 13.3%
Leading edge radius: 3.2%
Efficiency: 41.1
Max CL: 1.413
Max CL angle: 12.0
Max L/D: 61.001
Max L/D angle: 3.0
Max L/D CL: 0.733
Stall angle: 12.0
Zero-lift angle: -3.0