BOEING-VERTOL VR-14 AIRFOIL

Thickness: 8.0%
Camber: 1.7%
Trailing edge angle: 16.5o
Lower flatness: 12.8%
Leading edge radius: 2.0%
Efficiency: 29.4
Max CL: 0.961
Max CL angle: 9.0
Max L/D: 43.583
Max L/D angle: 6.0
Max L/D CL: 0.747
Stall angle: 9.0
Zero-lift angle: -0.5