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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 />

Fi igure 4.28:<br />

No ormalized Reyno olds<br />

Str ress Component<br />

@ z3 L3=4D Chapter 4<br />

At z3 in<br />

figure 4.28 8, the maximum<br />

absolute values <strong>of</strong> u u´´ w decreasees,<br />

howeve er, in the near wall region itt<br />

grows radiallly<br />

inward towwards<br />

the vortex<br />

core an nd the concentrated<br />

uw ´´ rregion<br />

in the vortex core, spreads radiallly<br />

outward d.<br />

Further r downstream m at z5 in figuure<br />

4.29, the overall magnnitude<br />

<strong>of</strong> u´ w ´<br />

decrease es <strong>and</strong> is an order o <strong>of</strong> 10 smmaller<br />

than at z1. Comparinng<br />

contour ploots<br />

for ReA A <strong>and</strong> ReB in fi igure 4.28, u´ w ´ distributioon<br />

at ReA has small gradiennts<br />

in the flow f domain. In I other wordds,<br />

the flow at ReB is more reesistant<br />

towards<br />

a uniform<br />

spatial distribution<br />

<strong>of</strong> u u´´ w in the fllow<br />

domain. AAnother<br />

featuure<br />

79<br />

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

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