BOEING VERTOL V(1.95)3009-1.25 AIRFOIL

Thickness: 9.0%
Camber: 1.3%
Trailing edge angle: 14.0o
Lower flatness: 11.4%
Leading edge radius: 2.4%
Efficiency: 33.0
Max CL: 1.026
Max CL angle: 15.0
Max L/D: 47.971
Max L/D angle: 5.5
Max L/D CL: 0.756
Stall angle: 7.5
Zero-lift angle: -0.5