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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 />

Fig gure 4.34:<br />

Norm malized Turbulen nt<br />

Kine etic Energy @ z3<br />

L3=4 4D<br />

Chapter 4<br />

With th he enlargemen nt <strong>of</strong> vortex coore<br />

at z3, the mmaximum<br />

vallue<br />

<strong>of</strong> turbulent<br />

kinetic energy decreases<br />

(Figure 44.34).<br />

The forrced<br />

vortex reegion,<br />

howeveer,<br />

still has s largest value e <strong>of</strong> k . For ReeB,<br />

the region surrounding the vortex coore<br />

with minimum m value es <strong>of</strong> k , is obbserved<br />

only in<br />

a small regiion<br />

<strong>of</strong> the crooss<br />

sectiona al plane at z3.<br />

Turbulent kkinetic<br />

energyy<br />

is very low along Y-axis at<br />

radial position p Y/R= = ±0.35 from cylinder axis <strong>and</strong> along XX-axis,<br />

turbulent<br />

kinetic energy has co omparatively inncreased.<br />

For both axes, thee<br />

values <strong>of</strong> k at<br />

large ra adial distance from f cylinder axis indicate an increase inn<br />

the turbulence<br />

level at t larger dista ance from thhe<br />

cylinder wwall.<br />

This demonstrates<br />

thhe<br />

existenc ce <strong>of</strong> asymmet tric distributioon<br />

<strong>of</strong> k also ooutside<br />

the forcced<br />

vortex.<br />

86<br />

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

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