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Experimental and Numerical Study of Swirling ... - Solid Mechanics

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<strong>Experimental</strong> <strong>and</strong> <strong>Numerical</strong> <strong>Study</strong> <strong>of</strong> <strong>Swirling</strong> Flow in Scavenging Process for 2-Stroke<br />

Marine Diesel Engines<br />

Figure 4.2:<br />

LDA Measurements<br />

along an arc behind the<br />

blades (a) mean radial<br />

velocity pr<strong>of</strong>ile (b) mean<br />

tangential velocity pr<strong>of</strong>ile<br />

(Schnipper, 2010).<br />

Chapter 4<br />

At downstream radial position <strong>of</strong> 180 mm, the relative variation in<br />

magnitudes <strong>of</strong> individual velocity components reduces significantly. A<br />

possible reason is that the flow at a radial position <strong>of</strong> 170 mm enters the<br />

contraction region which will have a damping effect to any variations/<br />

fluctuations in velocity <strong>and</strong> the flow at nearby upstream positions also feels<br />

the presence <strong>of</strong> the contraction section.<br />

(m/s)<br />

V r<br />

(m/s)<br />

V<br />

(a)<br />

(b)<br />

The measurements conducted along the two arcs behind the blades as<br />

mentioned in figure 3.18 are shown in figure 4.2. Where is the angular<br />

location <strong>of</strong> the measurement point on a given arc. The negative values <strong>of</strong> the<br />

velocity components are due to the orientation <strong>of</strong> LDA laser beams. Each<br />

half length <strong>of</strong> the error bar is one st<strong>and</strong>ard deviation. The results show that at<br />

a radial distance <strong>of</strong> 230 mm (the trailing end <strong>of</strong> the blade is approximately at<br />

51<br />

<strong>Swirling</strong> Flow in a Pipe

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