BOEING-VERTOL V23010-1.58 AIRFOIL

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Thickness: 10.2%
Camber: 1.8%
Trailing edge angle: 10.9o
Lower flatness: 74.5%
Leading edge radius: 2.5%
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