ONERA OA206 AIRFOIL

Thickness: 6.0%
Camber: 0.8%
Trailing edge angle: 7.1o
Lower flatness: 13.3%
Leading edge radius: 1.6%
Efficiency: 27.4
Max CL: 0.643
Max CL angle: 11.0
Max L/D: 31.192
Max L/D angle: 4.5
Max L/D CL: 0.543
Stall angle: 4.5
Zero-lift angle: 0.0