ARA-D 13% AIRFOIL

Thickness: 13.0%
Camber: 3.6%
Trailing edge angle: 46.5o
Lower flatness: 14.5%
Leading edge radius: 3.8%
Efficiency: 38.4
Max CL: 1.421
Max CL angle: 15.0
Max L/D: 28.423
Max L/D angle: 6.0
Max L/D CL: 1.098
Stall angle: -0.65
Zero-lift angle: -2.5