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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 />

Figu ure 6.8:<br />

Comp parison <strong>of</strong><br />

Norm malized Tangentia al<br />

Veloci ity Pr<strong>of</strong>ile at z . 6<br />

Figu ure 6.9:<br />

Comp parison <strong>of</strong><br />

Norm malized Axial<br />

Veloc city Pr<strong>of</strong>ile at z . 1<br />

6.2.2<br />

Axial Ve elocity<br />

Chapter 6<br />

For nor rmalized axial l velocity pr<strong>of</strong>files,<br />

at z , all the simulatioon<br />

cases resultt<br />

a<br />

1<br />

wake-lik ke pr<strong>of</strong>ile but<br />

with a recirrculation<br />

zonne<br />

in the vorttex<br />

core regioon<br />

(Figure 6.9). This see ems to be a mmajor<br />

differencce<br />

between thhe<br />

experimenttal<br />

<strong>and</strong> num merical results s because the experimental data, at z doees<br />

not show anny<br />

1<br />

recircul lation. Since no n measuremeents<br />

have beenn<br />

carried out at<br />

cross sectionnal<br />

position ns before z , it t is however unnknown<br />

whetther<br />

or not in the experiment<br />

1<br />

setup th here exists an ny recirculation<br />

prior to z . The vortex ccore<br />

size is also<br />

1<br />

predicte ed to be larg ger than the experimentaal<br />

data. This shows a pooor<br />

agreement<br />

with the experimentall<br />

data. RNG k modell<br />

with T.I 100%<br />

predicts s a comparativ vely lower peaak<br />

axial velociity<br />

magnitudee<br />

than the othher<br />

simulat tion cases. All<br />

the modells<br />

show reasoonable<br />

agreemment<br />

with thhe<br />

experim mental axial ve elocity pr<strong>of</strong>ile in the region close to the wwall<br />

i.e X/R =00.6<br />

to 0.8.<br />

154<br />

<strong>Numerical</strong> Modeling

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