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Space Grant Consortium - University of Wisconsin - Green Bay

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frames in the upper left corner, which lack transecting lines, were identified by hand so as<br />

to seed the automated vortex ring tracking code. The horizontal dotted line indicates the<br />

position <strong>of</strong> the fluid density interface. Notable in Fig. 3 is a slight change in the trajectory<br />

and orientation <strong>of</strong> the vortex ring just after penetrating the fluid density interface. These<br />

changes are accompanied by a slight change in its velocity and diameter.<br />

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Figure 3: A montage depicting the position, and orientation, <strong>of</strong> a vortex ring launched from the<br />

upper left corner <strong>of</strong> the image at an angle <strong>of</strong> 45 degrees with respect to a normal to the horizontal<br />

density interface (dotted line).<br />

Results and Discussion<br />

Vortex ring refraction. In the right column <strong>of</strong> Fig. 4 are shown nine representative<br />

trajectories <strong>of</strong> vortex rings when launched at incidence angles θi = 35 (row a), 45 (row b),<br />

and 60 degrees (row c). In each row, three separate launches are shown, represented from<br />

right to left by triangles, squares and circles. The precise value <strong>of</strong> θi for each launch is<br />

determined by fitting a line to the data which lies above the interface (the horizontal axis).<br />

It is then measured with respect to a normal to the fluid density interface.<br />

In the left column <strong>of</strong> Fig. 4 is shown the depth dependence <strong>of</strong> A/F for each launch. A<br />

logarithmic scale has been used on the abscissa to facilitate depiction <strong>of</strong> a wide range <strong>of</strong><br />

data. Notice that in each row, the rightmost vortex strikes the interface with the smallest<br />

velocity, and hence the largest value <strong>of</strong> A/F . In such cases, once below the interface, the<br />

vortex begins to curve upward. This suggests that for small Froude numbers, the buoyancy,<br />

rather than inertia, determines its trajectory. Proceeding leftward in each row, the vortices<br />

strike the interface with diminishing values <strong>of</strong> A/F . In particular, notice that the leftmost<br />

trajectory (circles) exhibits a distinct downward deflection, as emphasized by a broken line<br />

fit to the data beneath the interface. Such refraction occurs at relatively large values <strong>of</strong> the<br />

Froude number, when A/F � 0.004.<br />

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