BOEING-VERTOL VR-7 AIRFOIL WITH TAB

Thickness: 12.0%
Camber: 3.1%
Trailing edge angle: 11.3o
Lower flatness: 12.8%
Leading edge radius: 2.5%
Efficiency: 33.2
Max CL: 1.178
Max CL angle: 15.0
Max L/D: 35.182
Max L/D angle: 6.5
Max L/D CL: 0.845
Stall angle: 8.5
Zero-lift angle: -1.5