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Unformatted text preview: Spring 2004 Uniﬁed Engineering
Fluids Problems F9 –F10 F9+F10. The circulation distribution on a wing is
�(� ) = 2bV� (A1 sin � + A2 sin 2�)
where A1 = 0.05, and A2 = 0.01. a) Determine and plot �i (y ). b) Determine the rolling moment on the entire wing. Mroll = b/2
−b/2 � V� � y dy ...
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- Fall '05