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UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT

Click plot for plotting control

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Thickness:	8.6%
Camber:	2.3%
Trailing edge angle:	13.3^o
Lower flatness:	96.8%
Leading edge radius:	3.7%

Max C_L:	0.667
Max C_L angle:	15.0
Max L/D:	22.123
Max L/D angle:	10.5
Max L/D C_L:	0.516
Stall angle:	-0.5
Zero-lift angle:	-5.5