BOEING VERTOL V43012-1.58 AIRFOIL

Thickness: 12.0%
Camber: 3.6%
Trailing edge angle: 16.3o
Lower flatness: 11.7%
Leading edge radius: 3.3%
Efficiency: 32.1
Max CL: 1.278
Max CL angle: 15.0
Max L/D: 46.997
Max L/D angle: 2.5
Max L/D CL: 0.537
Stall angle: 7.5
Zero-lift angle: -2.5