HQ 2.5/8 AIRFOIL

Thickness: 8.0%
Camber: 2.5%
Trailing edge angle: 6.0o
Lower flatness: 23.9%
Leading edge radius: 1.7%
Efficiency: 26.1
Max CL: 1.001
Max CL angle: 5.5
Max L/D: 62.294
Max L/D angle: 3.0
Max L/D CL: 0.724
Stall angle: 5.5
Zero-lift angle: -3.0