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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 />

that have been used by the scientific community <strong>and</strong> this <strong>of</strong>ten makes it<br />

difficult to compare the results <strong>of</strong> one case <strong>of</strong> swirling flow with the other. In<br />

its simplest definition, the swirl parameter is defined as ‘the ratio <strong>of</strong><br />

maximum tangential velocity to the maximum axial velocity’ (Alekseenko et<br />

al., 2007). Greitzer et al. (2004) has adopted the definition as the ratio <strong>of</strong><br />

tangential to axial velocity. The definition by Gupta et al (1984) defines swirl<br />

number as ‘the ratio <strong>of</strong> axial flux <strong>of</strong> angular momentum to axial flux <strong>of</strong> axial<br />

momentum times the size L (which in case <strong>of</strong> cylindrical vortex chamber is<br />

the internal radius R <strong>of</strong> the chamber)’ (Alekseenko et al., 2007).<br />

Where<br />

S<br />

F<br />

mm<br />

(2.5)<br />

Fm<br />

L<br />

<br />

F v v vv r dA (2.6)<br />

mm a z<br />

A<br />

is the angular momentum flux taking into account the component <strong>of</strong> the<br />

Reynolds shear stress tensor <strong>and</strong><br />

<br />

2 2 <br />

F v vp p dA (2.7)<br />

m a a<br />

A<br />

is the momentum flux in axial direction taking in to account the normal<br />

component <strong>of</strong> Reynolds stress tensor in axial direction. The pressure<br />

represents the axial thrust (Khanna V. K., 2001).<br />

The calculation <strong>of</strong> swirl number based on above equations (2.5-2.7) is <strong>of</strong>ten<br />

very difficult because the velocity fields are usually unknown a priori<br />

(Alekseenko et al., 2007). The above equations are also simplified by<br />

dropping the shear stress <strong>and</strong> pressure terms. In case <strong>of</strong> experimental results,<br />

the use <strong>of</strong> above equations requires a complete knowledge <strong>of</strong> the velocity<br />

field for both axial <strong>and</strong> tangential components for a given cross-sectional<br />

plane. Consequently, for experiments where measurements are conducted<br />

for a part <strong>of</strong> the cross-sectional plane, the aforementioned equations cannot<br />

be used to estimate the degree <strong>of</strong> swirl.<br />

Another estimate <strong>of</strong> the swirl parameter is based on the geometrical<br />

parameters <strong>of</strong> the vortex chamber called as ‘design swirl parameter’<br />

(Alekseenko et al., 2007):<br />

Ddc<br />

S <br />

(2.8)<br />

A<br />

i<br />

20<br />

<strong>Swirling</strong> Flows

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