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AG37

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Drela AG37 airfoil. See also Drela airfoil links http://www.charlesriverrc.org/articles.htm and http://www.monkeytumble.com/hlg/supergee.htm

Thickness:	7.7%
Camber:	3.9%
Trailing edge angle:	9.2^o
Lower flatness:	83.3%
Leading edge radius:	0.8%

Max C_L:	1.069
Max C_L angle:	6.0
Max L/D:	35.349
Max L/D angle:	6.0
Max L/D C_L:	1.069
Stall angle:	6.0
Zero-lift angle:	-3.0