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 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