DSMA-523A AIRFOIL

Thickness: 11.0%
Camber: 2.3%
Trailing edge angle: 3.2o
Lower flatness: 6.1%
Leading edge radius: 2.9%
Efficiency: 32.4
Max CL: 1.282
Max CL angle: 15.0
Max L/D: 39.679
Max L/D angle: 1.5
Max L/D CL: 0.686
Stall angle: 1.5
Zero-lift angle: -4.0