BOEING VERTOL V13006-.7 AIRFOIL

Thickness: 6.0%
Camber: 0.9%
Trailing edge angle: 10.5o
Lower flatness: 16.4%
Leading edge radius: 1.7%
Efficiency: 28.3
Max CL: 0.734
Max CL angle: 12.5
Max L/D: 18.423
Max L/D angle: 1.5
Max L/D CL: 0.245
Stall angle: 1.5
Zero-lift angle: -0.5