AG08

Drela AG08 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness: 5.8%
Camber: 1.8%
Trailing edge angle: 5.7o
Lower flatness: 89.1%
Leading edge radius: 0.5%
Max CL: 0.817
Max CL angle: 5.5
Max L/D: 29.399
Max L/D angle: 5.5
Max L/D CL: 0.817
Stall angle: 5.5
Zero-lift angle: -1.5