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Question 1 (10 points) Rotational Flow and Vorticity The velocity components for a two-dimensional flow are u = ln hie) v = c
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for ination War & Co. - 2 y = 0 TOY ca V Cy yen² tn 2 av = Cyx. (4+ xº) x-1 x 25 dx - 2ny C (x² + y)² au - cnx (4 + x²) x 1Adding this the equation substitute to -zny Xc I (-2ny Xc - ((n + y)2 + zres ac -rayx -IN The show is irrotational

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