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FLOW AROUND A CYLINDER - istiarto

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– 5.37 –<br />

than the measured one. The strong vorticity peaks (positive and negative ones) in the<br />

bottom corner of the cylinder are missed by the simulation. This is due, as has been<br />

mentioned in the preceding section, to the inability of the simulation to reproduce the<br />

strong reversed flow at this location, which is caused by the limited spatial resolution<br />

of the grid.<br />

� In the plane � = 90° (Fig. 5.19c,d), the vorticity fields show small activity since the<br />

velocity components on this plane are very small as shown in the preceding section.<br />

Nevertheless, the contour plot near the bed indicates a reasonable agreement between<br />

the simulation and the measurement.<br />

� In the plane � = 180° (Fig. 5.19e,f), the simulation and the measurement exhibit<br />

surprisingly a good agreement. The vorticity, being rather small, is distributed more<br />

or less evenly over the plane and there is no region of concentrated vorticity.<br />

Turbulent kinetic energy around the cylinder<br />

Discussed in this section is the turbulent kinetic energy computed by the model. The<br />

computed turbulent kinetic energy is presented as an equivalent height (energy per unit<br />

weight), k g [mm], as shown in Fig. 5.20. For the sake of comparison, plotted also in the<br />

same figure are the values obtained from the experimental data; here the turbulent kinetic<br />

energy is obtained by k � 1 2 u �� u ���<br />

v �� v ���<br />

w ��w<br />

��<br />

following remarks:<br />

� � (see Chapter 3). The figures allow the<br />

� The plots show that the comparison of the computed and measured turbulent kinetic<br />

energy can be considered good. The simulation results in a lower energy than the<br />

measurement, but the tendency of the overall distributions is rather well predicted.<br />

� In the plane � = 0° (Fig. 5.20a,b), both simulation and measurement show high<br />

energy concentrations in the bottom corner of the cylinder. The computed maximum<br />

value shown at the corner vicinity of the cylinder, however, is considerably lower<br />

than the measured one. This is consistent with the difference observed between the<br />

computed and the measured velocities (and vorticities) at this particular location as<br />

discussed in the preceding sections. From the simulation, the high energy is also<br />

observed almost along the entire depth at close vicinity of the cylinder. Unfortunately,<br />

measurements in this region are not available along the entire depth.<br />

� In the plane � = 90° (Fig. 5.20c,d) similar observations as in the plane � = 0° can be<br />

made, but the simulation at the bottom corner of the cylinder is better, showing a<br />

close comparison to the measured data.<br />

� In the plane � = 180° (Fig. 5.20e,f) the simulation and the measurement show a<br />

similar pattern, but the under-estimation of the kinetic energy is also considerable as<br />

in the plane � = 0°.

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