AG09

Drela AG09 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness: 4.9%
Camber: 1.9%
Trailing edge angle: 4.5o
Lower flatness: 94.5%
Leading edge radius: 0.6%
Max CL: 0.743
Max CL angle: 5.0
Max L/D: 24.928
Max L/D angle: 5.0
Max L/D CL: 0.743
Stall angle: 5.0
Zero-lift angle: -1.5