Experimental and Numerical Study of Swirling ... - Solid Mechanics
Experimental and Numerical Study of Swirling ... - Solid Mechanics Experimental and Numerical Study of Swirling ... - Solid Mechanics
Experimental and Numerical Study of Swirling Flow in Scavenging Process for 2-Stroke Marine Diesel Engines Chapter 4 Based on the average angle of 28.6° at the radial position of 200 mm, using the conservation of angular momentum, the design swirl parameter for current experimental setup is 0.34 (Equation 2.8). 4.2 PIV Experimental Results (L3) The PIV experimental results are discussed here by describing the mean data for each flow characteristic. In order to present the results in a comprehensive and more understandable manner, at first, the results for the base case of cylinder length L3 are discussed and then the effect of change in cylinder length is discussed by comparing the results for L1, L2 and L3 at selected positions. The results for the remaining positions are presented in appendix A. 4.2.1 Mean Velocity Field The mean velocity field at z1 is presented for both the Reynolds numbers in figure 4.6. Each velocity component is non-dimensionalized with bulk flow velocity Vb. It can be seen that the resulting in-cylinder swirling flow is comprised of a concentrated vortex with a small core surrounded by a high velocity region. The velocity magnitude in the vortex core is very low compared to its surroundings and mean position of the vortex core is slightly eccentric to the geometric center of the cylinder. A low velocity region exists at larger radial positions close to the cylinder wall. Moreover, it can be observed that the core size, in case of ReB is relatively smaller than the velocity field at ReA. The flow decays downstream and the size of vortex core region increases indicating smaller localized velocity gradients compared to upstream positions (Figure 4.7). Moreover, the high velocity region exists at larger radial distances from the vortex core and the thickness of the high velocity region is also not uniform at all circumferential positions at the given radial distance from the core. This demonstrates the flow having three dimensional features. The size of the vortex core has further increased and the relative difference in the core size at two Reynolds numbers still exists. 54 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 4.6: Averag ged 3D Velocity Field at a z1 for L=4D (Color Contour represen nt the Normalized out of the pla ane velocity compon nent Vz / Vb. Chapter 4 If the size of vortex core c is to be ddefined as thee radial distannce from vortex core to the high velocity region theen at z5 the sizze of the vorteex has increaseed to almo ost half of the e cylinder radiius. Moreoverr it can also bbe observed thhat from ax xial location z1 z to z5 the floww decays dowwnstream and also position of vortex core moves in clockwisee direction foollowing the in-plane swiirl velocity y. For both Reynolds R nummbers the size of vortex is nnow nearly thhe same an nd the asymm metry/ three-dimmensionality of the velocityy field seems to have increased. 55 Swirling Flow in a Pipe
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<strong>Experimental</strong> <strong>and</strong> <strong>Numerical</strong> <strong>Study</strong> <strong>of</strong> <strong>Swirling</strong> Flow in Scavenging Process for 2-Stroke<br />
Marine Diesel Engines<br />
Chapter 4<br />
Based on the average angle <strong>of</strong> 28.6° at the radial position <strong>of</strong> 200 mm, using<br />
the conservation <strong>of</strong> angular momentum, the design swirl parameter for<br />
current experimental setup is 0.34 (Equation 2.8).<br />
4.2 PIV <strong>Experimental</strong> Results (L3)<br />
The PIV experimental results are discussed here by describing the mean data<br />
for each flow characteristic. In order to present the results in a<br />
comprehensive <strong>and</strong> more underst<strong>and</strong>able manner, at first, the results for the<br />
base case <strong>of</strong> cylinder length L3 are discussed <strong>and</strong> then the effect <strong>of</strong> change in<br />
cylinder length is discussed by comparing the results for L1, L2 <strong>and</strong> L3 at<br />
selected positions. The results for the remaining positions are presented in<br />
appendix A.<br />
4.2.1 Mean Velocity Field<br />
The mean velocity field at z1 is presented for both the Reynolds numbers in<br />
figure 4.6. Each velocity component is non-dimensionalized with bulk flow<br />
velocity Vb.<br />
It can be seen that the resulting in-cylinder swirling flow is comprised <strong>of</strong> a<br />
concentrated vortex with a small core surrounded by a high velocity region.<br />
The velocity magnitude in the vortex core is very low compared to its<br />
surroundings <strong>and</strong> mean position <strong>of</strong> the vortex core is slightly eccentric to the<br />
geometric center <strong>of</strong> the cylinder. A low velocity region exists at larger radial<br />
positions close to the cylinder wall. Moreover, it can be observed that the<br />
core size, in case <strong>of</strong> ReB is relatively smaller than the velocity field at ReA.<br />
The flow decays downstream <strong>and</strong> the size <strong>of</strong> vortex core region increases<br />
indicating smaller localized velocity gradients compared to upstream<br />
positions (Figure 4.7). Moreover, the high velocity region exists at larger<br />
radial distances from the vortex core <strong>and</strong> the thickness <strong>of</strong> the high velocity<br />
region is also not uniform at all circumferential positions at the given radial<br />
distance from the core. This demonstrates the flow having three dimensional<br />
features. The size <strong>of</strong> the vortex core has further increased <strong>and</strong> the relative<br />
difference in the core size at two Reynolds numbers still exists.<br />
54<br />
<strong>Swirling</strong> Flow in a Pipe