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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 />

Chapter 2<br />

levels etc. (Sloan et al., 1986). The adoption <strong>of</strong> a relation that local stresses<br />

being directly proportional to local strain rates rules out any special<br />

sensitivity to the streamline curvature (Craft et al., 2008). The assumption <strong>of</strong><br />

turbulent/ eddy viscosity as isotropic cannot be valid in flows influenced by<br />

body forces acting in a preferred direction, such as buoyancy, rotation <strong>and</strong><br />

streamline curvature (Sloan et al., 1986). Algifri et al. (1988) proposed, using<br />

experimental data on confined swirling flow, that the eddy viscosity is<br />

function <strong>of</strong> Reynolds <strong>and</strong> swirl numbers. Further, the k model is a<br />

simplistic function <strong>of</strong> a single time scale (proportional to a turbulence energy<br />

turnover time k ) which implies that the spectral energy transfer rates for<br />

production <strong>of</strong> turbulent kinetic energy by mean shear, the intermediate<br />

transferal regime <strong>and</strong> the viscous dissipation regime are equal without any<br />

characteristic lag (Sloan et al., 1986).<br />

The second order closure schemes having transport equations for individual<br />

components <strong>of</strong> Reynolds Stress tensor account for the curvature <strong>of</strong><br />

streamlines however the effect is at least an order <strong>of</strong> magnitude large than<br />

expected (Moene A.F., 2003) i.e. a 1% curvature strain produces for a<br />

boundary layer a 10% or greater effect on the turbulent stresses (Bradshaw,<br />

1973). The source terms in dissipation equation, to a significant degree<br />

control the magnitude <strong>of</strong> turbulent kinetic energy, mean velocity decay <strong>and</strong><br />

the spreading rates (Sloan et al., 1986). However, the transport equations for<br />

k <strong>and</strong> have no specific terms (source) to account for sensitiveness to<br />

rotation <strong>and</strong> swirl (Jakirlic´ et al., 2002). Since both <strong>of</strong> these transport<br />

equations are common in two-equation <strong>and</strong> second order closure schemes,<br />

the performance <strong>of</strong> second order closure schemes are also affected to some<br />

degree for modeling the swirling flows. <strong>Numerical</strong> issues also have<br />

significant impact on predicting the behavior <strong>of</strong> swirling flows (Craft et al.,<br />

2008).<br />

Different modeling approaches so far have been adopted to improve the<br />

performance <strong>of</strong> the aforementioned turbulence models <strong>and</strong> some <strong>of</strong> them are<br />

discussed here in brief. In order to include a rapid response to streamline<br />

curvature, the coefficient C in the turbulent viscosity equation (2.12) has<br />

been altered to a functional form (see Leshcziner et al., 1981). Sloan et al.,<br />

(1986) reports that more complex versions <strong>of</strong> C have been developed that<br />

include non-equilibrium turbulence <strong>and</strong> wall damping.<br />

2<br />

k<br />

t C. . (2.12)<br />

<br />

Where t is turbulent viscosity, C is a constant <strong>and</strong> has empirically<br />

determined value <strong>of</strong> 0.09 <strong>and</strong> is the fluid density.<br />

Yakhot et al., (1992) developed the RNG k model which, unlike the<br />

st<strong>and</strong>ard k model, is derived using a statistical technique called<br />

29<br />

<strong>Swirling</strong> Flows

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