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

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Experi imental <strong>and</strong> <strong>Numerical</strong> N Stud dy <strong>of</strong> <strong>Swirling</strong> g Flow in Scaveenging<br />

Processs<br />

for 2-Stroke<br />

Marin ne Diesel Engin nes<br />

Figure F 4.22:<br />

Normalized N Reyn nolds<br />

Stress S Component<br />

@ z3 L3= =4D<br />

Chapter 4<br />

minimu um variance or in other wwords<br />

comparratively<br />

steadyy<br />

axial velociity<br />

distribu ution is betwe een the core a<strong>and</strong><br />

the wall region where high values <strong>of</strong><br />

axial ve elocity are obs served (Figuree<br />

4.10). ww is<br />

also large in<br />

the near waall<br />

region. The relatively y smaller size o<strong>of</strong><br />

large w vaariance<br />

region at ReB is due to<br />

smaller vortex core co ompared to onne<br />

at ReA.<br />

The largest<br />

w varian nce at z3 is neearly<br />

half the vvalue<br />

at z1 (Fiigure<br />

4.22). Thhe<br />

forced vortex v region has large ww<br />

value except<br />

vortex cennter<br />

where it is<br />

low. Ne ear wall region n also demonsstrate<br />

large axxial<br />

w ´ disturbbances<br />

with thhe<br />

swirl de ecaying downs stream the floww.<br />

73<br />

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

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