NPL 9510 AIRFOIL

Thickness: 11.1%
Camber: 1.6%
Trailing edge angle: 17.8o
Lower flatness: 5.6%
Leading edge radius: 2.5%
Efficiency: 33.0
Max CL: 1.004
Max CL angle: 15.0
Max L/D: 15.837
Max L/D angle: 3.5
Max L/D CL: 0.48
Stall angle: 0.5
Zero-lift angle: -2.0