Experimental and Numerical Study of Swirling ... - Solid Mechanics
Experimental and Numerical Study of Swirling ... - Solid Mechanics Experimental and Numerical Study of Swirling ... - Solid Mechanics
Experi imental and Numerical N Stud dy of Swirling g Flow in Scaveenging Processs for 2-Stroke Marin ne Diesel Engin nes Figure F 4.23: : Normalized N Reyn nolds Stress S Component t @ z5 L3= =4D Chapter 4 At furth her downstrea am position zz5 in figure 4.23, the decayy in the largeest ww is half the larg gest value at zz3. The flow att high Reynollds number ReA has stro onger tendenc cy towards axiaal disturbancee w ´ . The higgh ww regioon in the vortex v core an nd the near wwall region groow in size in radial directioon and few w regions wit th patches off very low w variance are remained. In general, with the swirl decay, the sspatial distribuution of www , however loow in magn nitude, becom mes more unifoorm. 74 Swirling Flow in a Pipe
Experi imental and Numerical N Stud dy of Swirling g Flow in Scaveenging Processs for 2-Stroke Marin ne Diesel Engin nes Figure F 4.24: Normalized N Reyn nolds Stress S Component @ z1 L3=4D 4.2.6 Reynolds Shear Streesses Chapter 4 The she ear stress components of Reeynolds stressees, statisticallyy, are a measuure of the covariance c betw ween differennt velocity commponents. Thee distribution of Reynold ds shear stress s components are defined hhere in Cartessian coordinattes as descr ribed in sectio on 4.2.5 and a possible intterpretation foor their countter parts in n polar coordin nates is also diiscussed. The u´ v ´ contour plots p are showwn in figure 44.24 for z1 at both Reynoldds number rs. The uv ´´ has h large valuees near the cyllinder axis andd at large radiial 75 Swirling Flow in a Pipe
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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 4.23: :<br />
Normalized N Reyn nolds<br />
Stress S Component t<br />
@ z5 L3= =4D<br />
Chapter 4<br />
At furth her downstrea am position zz5<br />
in figure 4.23,<br />
the decayy<br />
in the largeest<br />
ww is<br />
half the larg gest value at zz3.<br />
The flow att<br />
high Reynollds<br />
number ReA<br />
has stro onger tendenc cy towards axiaal<br />
disturbancee<br />
w ´ . The higgh<br />
ww regioon<br />
in the vortex v core an nd the near wwall<br />
region groow<br />
in size in radial directioon<br />
<strong>and</strong> few w regions wit th patches <strong>of</strong>f<br />
very low w variance are<br />
remained. In<br />
general,<br />
with the swirl<br />
decay, the sspatial<br />
distribuution<br />
<strong>of</strong> www , however loow<br />
in magn nitude, becom mes more unifoorm.<br />
74<br />
<strong>Swirling</strong> Flow in a Pipe