HQ 0/9 AIRFOIL

Thickness: 8.1%
Camber: 0.0%
Trailing edge angle: 5.8o
Lower flatness: 8.0%
Leading edge radius: 1.8%
Efficiency: 26.3
Max CL: 0.552
Max CL angle: 9.5
Max L/D: 33.995
Max L/D angle: 4.0
Max L/D CL: 0.462
Stall angle: 4.0
Zero-lift angle: 0.0