AG38

Drela AG38 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness: 7.0%
Camber: 3.5%
Trailing edge angle: 8.8o
Lower flatness: 88.2%
Leading edge radius: 0.7%
Max CL: 0.997
Max CL angle: 5.5
Max L/D: 27.955
Max L/D angle: 5.5
Max L/D CL: 0.997
Stall angle: 5.5
Zero-lift angle: -3.0