HQ 0/10 AIRFOIL

Thickness: 10.0%
Camber: 0.0%
Trailing edge angle: 7.2o
Lower flatness: 6.5%
Leading edge radius: 2.0%
Efficiency: 31.7
Max CL: 0.685
Max CL angle: 12.0
Max L/D: 36.777
Max L/D angle: 5.5
Max L/D CL: 0.641
Stall angle: 5.5
Zero-lift angle: 0.0