BOEING-VERTOL VR-11X AIRFOIL

Thickness: 11.0%
Camber: 2.4%
Trailing edge angle: 22.2o
Lower flatness: 10.1%
Leading edge radius: 2.4%
Efficiency: 32.1
Max CL: 1.112
Max CL angle: 15.0
Max L/D: 35.303
Max L/D angle: 7.5
Max L/D CL: 0.898
Stall angle: 0.0
Zero-lift angle: -0.5