AG13

Drela AG13 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness: 5.8%
Camber: 2.0%
Trailing edge angle: 3.9o
Lower flatness: 88.7%
Leading edge radius: 0.5%
Max CL: 0.861
Max CL angle: 5.5
Max L/D: 30.031
Max L/D angle: 5.5
Max L/D CL: 0.861
Stall angle: 5.5
Zero-lift angle: -2.0