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NACA 63-415 AIRFOIL

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Thickness:	15.0%
Camber:	2.2%
Trailing edge angle:	9.7^o
Lower flatness:	42.1%
Leading edge radius:	2.0%

Max C_L:	1.3
Max C_L angle:	15.0
Max L/D:	49.417
Max L/D angle:	5.0
Max L/D C_L:	0.901
Stall angle:	8.0
Zero-lift angle:	-3.0