AH 79-100 C

Althaus AH 79-100C airfoil

Thickness: 9.9%
Camber: 6.7%
Trailing edge angle: 11.7o
Lower flatness: 59.3%
Leading edge radius: 1.3%
Max CL: 1.65
Max CL angle: 11.5
Max L/D: 73.887
Max L/D angle: 4.0
Max L/D CL: 1.435
Stall angle: 5.5
Zero-lift angle: -8.5