RAF 26 AIRFOIL

Thickness: 6.6%
Camber: 2.1%
Trailing edge angle: 13.2o
Lower flatness: 35.8%
Leading edge radius: 1.8%
Efficiency: 28.8
Max CL: 0.878
Max CL angle: 11.0
Max L/D: 53.078
Max L/D angle: 4.5
Max L/D CL: 0.803
Stall angle: 2.5
Zero-lift angle: -2.5