CLARK V AIRFOIL

Thickness: 11.6%
Camber: 3.4%
Trailing edge angle: 22.2o
Lower flatness: 18.3%
Leading edge radius: 2.8%
Efficiency: 41.6
Max CL: 1.483
Max CL angle: 10.0
Max L/D: 62.075
Max L/D angle: 5.0
Max L/D CL: 1.084
Stall angle: 7.5
Zero-lift angle: -4.0