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USA 35 A AIRFOIL

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Thickness:	18.2%
Camber:	6.4%
Trailing edge angle:	21.6^o
Lower flatness:	86.3%
Leading edge radius:	5.6%

Max C_L:	2.018
Max C_L angle:	15.0
Max L/D:	40.964
Max L/D angle:	4.0
Max L/D C_L:	1.149
Stall angle:	-0.5
Zero-lift angle:	-6.0