AH-6-40-7 AIRFOIL

Thickness: 6.8%
Camber: 5.5%
Trailing edge angle: 22.0o
Lower flatness: 9.5%
Leading edge radius: 2.1%
Efficiency: 43.3
Max CL: 1.749
Max CL angle: 9.0
Max L/D: 55.957
Max L/D angle: 6.0
Max L/D CL: 1.443
Stall angle: 9.0
Zero-lift angle: -6.5