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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 4.32:<br />

Nor rmalized Reynold ds<br />

Stre ess Component<br />

@ z5 z L3=4D<br />

Chapter 4<br />

The dis stribution <strong>of</strong> Reynolds R sheaar<br />

stress components<br />

vv z <strong>and</strong> vv r z caan<br />

be unde erstood by considering<br />

the plots for bothh<br />

uw ´´ <strong>and</strong> v v´´ w . Since thhe<br />

axial ve elocity is sam me in both cooordinate<br />

systeems,<br />

the covaariance<br />

<strong>of</strong> axiial<br />

velocity y component with w tangentiial<br />

<strong>and</strong> radial velocities cann<br />

be understoood<br />

by cons sidering (Figu ure 4.14). As ddiscussed<br />

in ssection<br />

4.2.5, in the contouur<br />

plot <strong>of</strong> u the radial velocity v is obseerved<br />

along X-axis<br />

tangentiaal<br />

velocity alonng<br />

Y-axis. In I figure 4.27 7 for uw ´´ , thhe<br />

two small rregions<br />

along Y-axis <strong>and</strong> in<br />

figure 4.30 4 for vw ´´ , similar regionns<br />

along X-axis<br />

represent reggions<br />

with largge<br />

covarian nce between tangential a<strong>and</strong><br />

axial veloocity<br />

componnents<br />

i.e. vv vz .Similar rly, the near wall w regions inn<br />

figures 4.27 <strong>and</strong> 4.30 represent<br />

the largge<br />

83<br />

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

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