OAF102 AIRFOIL

Thickness: 10.1%
Camber: 3.6%
Trailing edge angle: 22.1o
Lower flatness: 14.2%
Leading edge radius: 2.2%
Efficiency: 23.2
Max CL: 1.031
Max CL angle: 15.0
Max L/D: 39.153
Max L/D angle: 6.0
Max L/D CL: 0.741
Stall angle: 6.0
Zero-lift angle: -3.5