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Assume that the streamlines for the wingtip vortices from an airplane (see Fig. P4.26 an...

Assume that the streamlines for the wingtip vortices from an airplane (see Fig. P4.26 and Video V4.6) can be approximated by circles of radius r and that the speed is V = K/r, where K is a constant. Determine the streamline acceleration, as, and the normal acceleration, an, for this flow.

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Solutions For Problems in Chapter 4
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