AG19

Drela AG19 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness: 5.4%
Camber: 2.3%
Trailing edge angle: 3.7o
Lower flatness: 89.6%
Leading edge radius: 0.5%
Max CL: 0.941
Max CL angle: 6.0
Max L/D: 33.14
Max L/D angle: 6.0
Max L/D CL: 0.941
Stall angle: 6.0
Zero-lift angle: -2.0