ONERA OA213 AIRFOIL

Thickness: 12.5%
Camber: 3.3%
Trailing edge angle: 9.5o
Lower flatness: 9.9%
Leading edge radius: 2.6%
Efficiency: 37.5
Max CL: 1.167
Max CL angle: 15.0
Max L/D: 30.269
Max L/D angle: 8.0
Max L/D CL: 0.914
Stall angle: 12.0
Zero-lift angle: -1.0