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5.2 Experimental data<br />
– 5.3 –<br />
5.2.1 Flow around a cylinder on a flat channel bed<br />
The measured data of flow around a cylinder on a flat channel bed are obtained from the<br />
previous work (Yulistiyanto, 1997). The data were produced from the measurements with<br />
and without the cylinder in place. Given below is a brief description of the data; details of<br />
the measurements and of the data can be found elsewhere (see Yulistiyanto, 1997).<br />
The measurements were conducted in a rectangular metal-bed (smooth) tilting flume of<br />
an effective length L = 38 [m] and width B = 2 [m]. The uniform approach flow was<br />
established by: discharge Q = 0.250 [m 3 /s] (Q B � 0.125 [m 2 s]), flow depth<br />
h ∞ = 18.5 [cm] (B h � � 10.8), cross-sectional-averaged velocity U ∞ = 0.67 [m/s]<br />
(Re = 123,950 and Fr = 0.5), and bed slope S o = 6.25 �10 -4 . An acoustic Doppler<br />
velocity profiler (ADVP), designed and conceived at LRH (see Lhermitte and Lemmin,<br />
1994), was used to measure the instantaneous velocity vector. This non-intrusive<br />
instrument measures instantaneously three-dimensional velocities at a number of layers<br />
(in 5 [mm] intervals) within a water column (flow depth) based on the Doppler shift of<br />
the backscattered acoustic signals. The ADVP was fixed at a compartment located below<br />
the metal bed, at the center line, x L = 16 [m] from the entrance. A Mylar film, permeable<br />
to acoustic waves, was used to separate the instrument compartment and the flow. A PVC<br />
circular cylinder of diameter D p = 22 [cm] (B D p � 9 ) was installed vertically with<br />
respect to the bed. The cylinder was attached to a movable carriage, allowing it to be<br />
positioned at predetermined measurement stations around the ADVP. Vertical<br />
distributions of 3D instantaneous velocities were obtained in five planes, � = 0°, 45°,<br />
90°, 157.5°, and 180°. The vertical distributions of the time-averaged velocities, (u,v,w),<br />
turbulence intensities, ( u �� u ��,<br />
v �� v ��,<br />
w �� w ��),<br />
and the Reynolds stresses, (��u ��w<br />
��,<br />
��v ��w<br />
��),<br />
were subsequently deduced.<br />
From the measurement in the uniform flow condition (the flow without the cylinder in<br />
place), an equivalent roughness of k s � 0.54 [mm] was reported (Yulistiyanto, 1997).<br />
This value was obtained by using the Colebroke-White equation. A reavaluation of the k s<br />
by imposing a logarithmic distribution to the measured u-velocity profile, u(z), shows an<br />
equivalent roughness of k s � 0.85 [mm]. Since the present mathematical model uses k s<br />
as the input parameter in the wall boundary treatment, its value shall be calibrated to get<br />
the suitable model value.<br />
5.2.2 Flow around a cylinder in a scoured channel bed<br />
Measured data of flow around a cylinder in a scoured channel bed are available from the<br />
laboratory measurement presented in the previous chapter (see Chapter 2). A brief<br />
description of the experimental work is recalled in the following paragraph.<br />
The experiment was conducted in a rectangular channel of length L = 29 [m] and width<br />
B = 2.45 [m]. The channel bed is made of uniform sand of mean diameter