AH 79-100 A AIRFOIL

Thickness: 10.0%
Camber: 3.6%
Trailing edge angle: 7.2o
Lower flatness: 17.0%
Leading edge radius: 2.1%
Efficiency: 33.4
Max CL: 1.227
Max CL angle: 6.5
Max L/D: 73.259
Max L/D angle: 4.5
Max L/D CL: 1.04
Stall angle: 6.5
Zero-lift angle: -4.0