ARA-D 10% AIRFOIL

Thickness: 10.0%
Camber: 4.0%
Trailing edge angle: 41.6o
Lower flatness: 41.6%
Leading edge radius: 3.0%
Efficiency: 39.4
Max CL: 1.432
Max CL angle: 15.0
Max L/D: 38.829
Max L/D angle: 5.0
Max L/D CL: 1.059
Stall angle: 9.5
Zero-lift angle: -3.5