HQ 0/7 AIRFOIL

Thickness: 7.0%
Camber: 0.0%
Trailing edge angle: 5.0o
Lower flatness: 9.3%
Leading edge radius: 1.6%
Efficiency: 21.5
Max CL: 0.475
Max CL angle: 8.5
Max L/D: 29.51
Max L/D angle: 2.5
Max L/D CL: 0.288
Stall angle: 3.0
Zero-lift angle: 0.0