AG10

Drela A109 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness: 4.7%
Camber: 1.7%
Trailing edge angle: 4.2o
Lower flatness: 93.8%
Leading edge radius: 0.8%
Max CL: 0.772
Max CL angle: 11.5
Max L/D: 20.839
Max L/D angle: 5.0
Max L/D CL: 0.726
Stall angle: 5.0
Zero-lift angle: -1.0