AG17

Drela AG17 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness: 6.5%
Camber: 2.0%
Trailing edge angle: 4.2o
Lower flatness: 84.7%
Leading edge radius: 0.5%
Max CL: 0.878
Max CL angle: 5.5
Max L/D: 31.669
Max L/D angle: 5.5
Max L/D CL: 0.878
Stall angle: 5.5
Zero-lift angle: -2.0