AG04

Drela AG04 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness: 6.4%
Camber: 1.8%
Trailing edge angle: 5.7o
Lower flatness: 84.5%
Leading edge radius: 0.5%
Max CL: 0.866
Max CL angle: 6.0
Max L/D: 32.1
Max L/D angle: 6.0
Max L/D CL: 0.866
Stall angle: 6.0
Zero-lift angle: -1.5