AH 79-100 A

Althaus AH 79-100A airfoil

Thickness: 10.0%
Camber: 3.6%
Trailing edge angle: 7.1o
Lower flatness: 73.6%
Leading edge radius: 1.3%
Max CL: 1.228
Max CL angle: 6.5
Max L/D: 60.662
Max L/D angle: 4.5
Max L/D CL: 1.041
Stall angle: 6.5
Zero-lift angle: -4.0