ARA-D 6% AIRFOIL

Thickness: 6.0%
Camber: 5.0%
Trailing edge angle: 32.6o
Lower flatness: 12.1%
Leading edge radius: 2.0%
Efficiency: 32.8
Max CL: 1.588
Max CL angle: 8.5
Max L/D: 44.454
Max L/D angle: 8.0
Max L/D CL: 1.544
Stall angle: 8.5
Zero-lift angle: -5.5