AG16

Drela AG16 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness: 7.1%
Camber: 1.9%
Trailing edge angle: 4.5o
Lower flatness: 77.8%
Leading edge radius: 0.5%
Max CL: 0.921
Max CL angle: 6.0
Max L/D: 34.003
Max L/D angle: 6.0
Max L/D CL: 0.921
Stall angle: 6.0
Zero-lift angle: -2.0