HQ 2.0/8 AIRFOIL

Thickness: 8.0%
Camber: 2.0%
Trailing edge angle: 6.0o
Lower flatness: 18.0%
Leading edge radius: 1.8%
Efficiency: 27.4
Max CL: 0.981
Max CL angle: 6.0
Max L/D: 58.869
Max L/D angle: 3.0
Max L/D CL: 0.649
Stall angle: 6.0
Zero-lift angle: -2.5