HQ 2.0/9 AIRFOIL

Thickness: 9.0%
Camber: 2.0%
Trailing edge angle: 6.8o
Lower flatness: 14.3%
Leading edge radius: 1.9%
Efficiency: 30.4
Max CL: 1.092
Max CL angle: 7.0
Max L/D: 57.587
Max L/D angle: 3.0
Max L/D CL: 0.654
Stall angle: 6.0
Zero-lift angle: -2.5