Experimental and Numerical Study of Swirling ... - Solid Mechanics
Experimental and Numerical Study of Swirling ... - Solid Mechanics
Experimental and Numerical Study of Swirling ... - Solid Mechanics
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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 6<br />
<strong>Numerical</strong> Modeling<br />
This chapter presents the results from the numerical modeling <strong>of</strong> the swirling flow<br />
test case. Unsteady simulations are conducted using two RANS based approaches<br />
<strong>and</strong> the results are compared with the experimental data. The simulations results<br />
only represent the case with fully open cylinder intake port <strong>and</strong> at Reynolds<br />
number <strong>of</strong> 65,000. A discussion has also been made on the possible approaches for<br />
improving the simulation results.<br />
The results <strong>of</strong> the numerical models included in this chapter are those<br />
obtained until the time <strong>of</strong> writing this thesis. For mesh generation, Ansys ®<br />
GAMBIT v2.4 is used <strong>and</strong> for CFD processing Ansys ® FLUENT v12.1 is used.<br />
The post processing <strong>of</strong> the numerical data is done in Fieldview ® v 12.<br />
The computational domain does not include the guide vanes <strong>and</strong> the inlet to<br />
the domain is defined at a radial distance <strong>of</strong> 200 mm from the axis <strong>of</strong><br />
rotation (Figure 6.1). In the experimental setup the inlet to the setup is at a<br />
radial distance <strong>of</strong> 300 mm with guide vanes mounted at 250mm radial<br />
distance from the cylinder axis/ axis <strong>of</strong> rotation (Figure 4.1). This is adopted<br />
to avoid the inlet to be in the region with large wake effects behind the guide<br />
vanes <strong>and</strong> also not close to the contraction section. The LDA measurements<br />
in section 4.1 show a very small wake effect at this radial distance. Another<br />
purpose is to see if it is possible to achieve good results by neglecting the<br />
guide vanes region in the computational mesh <strong>and</strong> defining the magnitude<br />
<strong>of</strong> radial <strong>and</strong> tangential velocity components at some radial position after the<br />
guide vanes region. The computational mesh has Y-axis as its rotational axis,<br />
therefore, the velocity component along Y-axis represents the axial<br />
component <strong>and</strong> for velocity component along Z-axis it is vice versa.<br />
147<br />
<strong>Numerical</strong> Modeling