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FLOW AROUND A CYLINDER - istiarto

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– 6.3 –<br />

The spatial distributions of the turbulence intensities and the Reynolds stresses were also<br />

evaluated. The intensity of turbulence inside the scour hole is strong; an increasing<br />

turbulence was detected approaching the cylinder and moving around the cylinder<br />

towards the downstream (wake) region. In the wake region, where a separation evidenced<br />

by a flow reversal takes place, the turbulence attains its strongest intensity. The kinetic<br />

energy of the flow inside the scour hole, where a circulating flow is eminent, consists of<br />

high turbulent energy, ranging from 10% to 90% of the total kinetic energy. The profiles<br />

of the turbulent kinetic energy are characterized by distinguishable bulges along the<br />

presumed separation line. Approaching and moving around the cylinder, those bulges<br />

move downwards, increase, and enlarge.<br />

The longitudinal distribution of the bed shear-stresses along the plane of symmetry shows<br />

that the bed shear-stress is reduced upon entering the scour hole when compared to its<br />

value in the approach flow. The shear stress along the upstream scour bed has negative<br />

values, corresponding to the flow reversal in that region. These observations are<br />

supported by the numerical simulation.<br />

6.2.2 Numerical simulations<br />

The flow simulations were performed by using a 3D numerical model, which is<br />

developed based on the approximate solution of the Reynolds-averaged Navier-Stokes<br />

equations for incompressible flows by using finite-volume method. The model uses the k-<br />

� turbulence closure model to compute the turbulence stresses and the SIMPLE (Semi-<br />

Implicit Method for Pressure-Linked Equations) method of Patankar and Spalding<br />

(1972) 2 to link the velocity to the pressure. The water surface position is determined<br />

according to the pressure along the surface boundary. The model solves the transient flow<br />

equations, but is applicable only for steady flow problems.<br />

The core of the present model is relatively standard and can be found in classical<br />

textbooks. However, some detailed derivations and clarifications were elucidated about<br />

the boundary conditions and the pressure-velocity coupling. These are seldom presented<br />

in detail.<br />

Preliminary simulation tests were carried out to ascertain the methods and modeling<br />

techniques opted in the model; these serve as the calibration and verification of the<br />

model. A simple and well-known uniform flow was selected. The model value of the<br />

equivalent standard roughness of the bed was calibrated against the measurements.<br />

Verification of the model was done by simulating the flow under different boundary and<br />

initial conditions; the model could produce the uniform flow field and the agreement with<br />

the measured one was nearly perfect.<br />

2 Patankar, S.V., and Spalding, D.B. (1972). ―A calculation procedure for heat, mass and momentum<br />

transfer in three-dimensional parabolic flows.‖ Int. J. Heat Mass Transfer, 15, 1787-1806.

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