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FLOW AROUND A CYLINDER - istiarto

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– 5.29 –<br />

using a Joukowski transformation to construct the xy-grid, and by stretching this grid in<br />

the z direction to form the xyz control-volume grid. The grid sizes in the x and y<br />

directions vary between 0.11 to 12 [cm] and 0.5 to 8 [cm]; in the z direction, the grid<br />

sizes are 4% to 8% of the local flow-depth. To generate the bed level of the<br />

computational domain, the elevations of the bottom cell vertices were interpolated from a<br />

5 � 5-[mm 2 ] uniform bed-level grid. This grid was constructed based on the measured<br />

bed-level data obtained by point gauge measurements. Fig. 5.15 illustrates the xy and xz<br />

grids at an intermediate solution of the simulation.<br />

5.6.2 Boundary and initial conditions<br />

There are five boundary conditions in this run, i.e. inflow, outflow, symmetry, wall, and<br />

surface boundaries. These are all boundary-condition types that can be handled by the<br />

present model.<br />

� Upstream inflow, x = –2.5 [m]: Q 2 � 0.1[m 3 s] and u, v, w, k, � are available from<br />

the measurement in the approach flow region (see Chapter 2). The values of � are<br />

obtained by � � c � k 2 � t (see Eq. 5.1), where the eddy viscosity, � t , and the kinetic<br />

energy, k, are obtainable from the measured velocities (see also Eq. 5.2) such as<br />

�t � �u ��w<br />

�� �u �z and k � 1 2�u<br />

�� u ���<br />

v �� v ���<br />

w ��w<br />

���.<br />

� Downstream outflow, x = 2.5 [m]: constant surface elevation, which corresponds to<br />

the depth of the uniform approach flow, h � = 17.8 [cm].<br />

� Left (north) boundary, y = 0: wall boundary along the cylinder (persplex glass),<br />

BCC ��B<br />

��,<br />

(–0.75 ≤ x [m] ≤ 0.75) with ks = 0.22 [mm] and symmetry plane along the<br />

rest, ABB ��A<br />

��and<br />

CDD �� C ��.<br />

� Right (south) boundary, y = –1.225 [m]: wall boundary along the channel glass sidewall<br />

with k s = 0 [mm].<br />

� Bottom boundary: wall boundary along the channel uniform-sand bed with<br />

k s = 2d 50 = 4.2 [mm] (see Sect. 5.3.3).<br />

� Top boundary: water surface.<br />

The initial conditions of the simulation are horizontal flow depth corresponding to the<br />

known uniform flow depth (h∞ = 17.8 [cm]), hydrostatic pressure distribution,<br />

p � ��gz �zsurface � z�<br />

[Pa], velocity and k-� according to the known distributions at the<br />

inlet boundary. Within the initial stage, as in the simulation of the flat-bed case, the water<br />

surface was kept constant until the flow field was more or less constant. The simulation<br />

was then restarted and the water surface was let to move following the surface boundary<br />

treatment, except at the downstream boundary.

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