AG12

Drela AG12 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness: 6.2%
Camber: 1.8%
Trailing edge angle: 4.0o
Lower flatness: 85.7%
Leading edge radius: 0.5%
Max CL: 0.901
Max CL angle: 6.0
Max L/D: 33.108
Max L/D angle: 6.0
Max L/D CL: 0.901
Stall angle: 6.0
Zero-lift angle: -2.0