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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 />

forced vortex <strong>and</strong> the axial velocity changes correspondingly from a wakelike<br />

to a jet-like. This change, however, starts at cross-sectional planes close to<br />

cylinder outlet <strong>and</strong> moves to upstream positions. At 50% port closure, the<br />

mean axial velocity in the whole cylinder attains a jet like pr<strong>of</strong>ile. The<br />

tangential velocity resembles more to a wall-jet than a forced vortex pr<strong>of</strong>ile.<br />

With 75% port closure, the jet-like axial velocity pr<strong>of</strong>ile at cross-sectional<br />

plane close to intake port changes back to wake-like at the adjacent crosssectional<br />

plane <strong>and</strong> downstream. This indicates a vortex breakdown like<br />

characteristic. The tangential velocity then has forced vortex pr<strong>of</strong>ile<br />

throughout the cylinder. The non-dimensional pr<strong>of</strong>iles <strong>of</strong> velocity<br />

components have no significant variation with the variation in Reynolds<br />

number.<br />

<strong>Numerical</strong> simulations are conducted only for the fully open intake port<br />

case. The turbulence models include RNG k <strong>and</strong> Reynolds stress<br />

models. The simulation results, however, do not show satisfactory<br />

agreement with the experimental data. The models predicted a larger vortex<br />

core size with a reverse flow. The downstream decay in the swirl is predicted<br />

to be lower than observed from experimental results. However, there are<br />

some qualitative features like distribution <strong>of</strong> modeled Reynolds stress<br />

components that, to some extent, have reasonable agreements. The factors<br />

affecting the performance <strong>of</strong> the CFD models possibly lie both in the<br />

treatment <strong>of</strong> turbulence <strong>and</strong> the numerical aspects.

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