BOEING-VERTOL V23010-1.58 AIRFOIL

Thickness: 10.1%
Camber: 1.7%
Trailing edge angle: 10.8o
Lower flatness: 11.7%
Leading edge radius: 2.7%
Efficiency: 32.3
Max CL: 1.097
Max CL angle: 15.0
Max L/D: 45.001
Max L/D angle: 6.0
Max L/D CL: 0.774
Stall angle: 9.0
Zero-lift angle: -1.0