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Experimental and Numerical Study of Swirling ... - Solid Mechanics

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V θ / V b<br />

V θ / V b<br />

V θ / V b<br />

1.5<br />

5.0<br />

1.0<br />

measurement 1<br />

5.0<br />

measurement 1<br />

0.0<br />

0.5<br />

4.0<br />

−5.0<br />

0.0<br />

3.0<br />

−10.0<br />

−0.5<br />

2.0<br />

−15.0<br />

−1.0<br />

1.0<br />

−20.0<br />

measurement 1<br />

−1.5<br />

−1.0 −0.5 0.0 0.5 1.0<br />

0.0<br />

−1.0 −0.5 0.0 0.5 1.0<br />

−25.0<br />

−1.0 −0.5 0.0 0.5 1.0<br />

X / R<br />

v (a)<br />

X / R<br />

v (b)<br />

X / R<br />

v<br />

(c)<br />

1.5<br />

5.0<br />

1.0<br />

0.5<br />

0.0<br />

measurement 1<br />

measurement 2<br />

measurement 3<br />

measurement 4<br />

5.0<br />

4.0<br />

3.0<br />

measurement 1<br />

measurement 2<br />

measurement 3<br />

measurement 4<br />

0.0<br />

−5.0<br />

−10.0<br />

−0.5<br />

2.0<br />

−15.0<br />

measurement 1<br />

measurement 2<br />

−1.0<br />

1.0<br />

−20.0<br />

measurement 3<br />

measurement 4<br />

−1.5<br />

−1.0 −0.5 0.0 0.5 1.0<br />

0.0<br />

−1.0 −0.5 0.0 0.5 1.0<br />

−25.0<br />

−1.0 −0.5 0.0 0.5 1.0<br />

X / R<br />

v<br />

(d)<br />

X / R<br />

v<br />

(e)<br />

X / R<br />

v (f)<br />

1.5<br />

5.0<br />

1.0<br />

0.5<br />

measurement 1<br />

measurement 2<br />

5.0<br />

4.0<br />

measurement 1<br />

measurement 2<br />

0.0<br />

−5.0<br />

0.0<br />

3.0<br />

−10.0<br />

−0.5<br />

2.0<br />

−15.0<br />

−1.0<br />

1.0<br />

−20.0<br />

measurement 1<br />

measurement 2<br />

−1.5<br />

−1.0 −0.5 0.0 0.5 1.0<br />

0.0<br />

−1.0 −0.5 0.0 0.5 1.0<br />

−25.0<br />

−1.0 −0.5 0.0 0.5 1.0<br />

X / R<br />

v (g)<br />

X / R<br />

v (h)<br />

X / R<br />

v (i)<br />

V z / V b<br />

V z / V b<br />

V z / V b<br />

Fig. 8 Normalized time averaged pr<strong>of</strong>iles with 75 % closed ports: (a) tangential velocity pr<strong>of</strong>ile at z/D = 0.963; (b) axial velocity pr<strong>of</strong>ile at<br />

z/D = 0.963; (c) axial vorticity Pr<strong>of</strong>ile at z/D = 0.963; (d) tangential velocity pr<strong>of</strong>ile at z/D = 1.489; (e) axial velocity pr<strong>of</strong>ile at z/D = 1.489; (f)<br />

axial vorticity Pr<strong>of</strong>ile at z/D = 1.489; (g) tangential velocity pr<strong>of</strong>ile at z/D = 3.068; (h) axial velocity pr<strong>of</strong>ile at z/D = 3.068; (i) axial vorticity<br />

Pr<strong>of</strong>ile at z/D = 3.068.<br />

A significant change in the vz pr<strong>of</strong>ile is observed at z/D =<br />

1.489 where vz changes back from jet-like to wake-like pr<strong>of</strong>ile<br />

(Fig. 8e) which is characteristic <strong>of</strong> a vortex breakdown<br />

(Escudier et al, 1982). The pr<strong>of</strong>ile for vz remains the same<br />

i.e. wake-like at all downstream positions (Fig. 8h), however,<br />

the peak value vz is observed at large radial distance<br />

from the vortex center indicating an increase in the vortex<br />

core size downstream the flow.<br />

When the intake port is closed by 75 % (Fig. 8c), compared<br />

to the other positions <strong>of</strong> the piston, at z/D = 0.963<br />

the strong vorticity <strong>of</strong> the vortex core region no longer exists.<br />

Instead the mean velocity field has nearly uniform ωzdistribution<br />

throughout the cylinder.<br />

The increase in the value <strong>of</strong> the turbulent kinetic energy<br />

continues with the partial closure <strong>of</strong> the intake port.<br />

For 75 %, similar to 50 %, the vortex core region has a low<br />

value <strong>of</strong> TKE at z/D = 0.963 (Fig. 9c). The distribution<br />

<strong>of</strong> TKE in the core region is comparatively more symmetric<br />

than at 50 %. This can be observed from the vz pr<strong>of</strong>ile<br />

(Fig. 8b) which is more symmetric than vz pr<strong>of</strong>ile at 50 %<br />

port closure (Fig. 7b).<br />

6Conclusion<br />

The magnitudes <strong>of</strong> the tangential <strong>and</strong> axial velocities decay<br />

downstream due to friction with the internal cylinder wall.<br />

ω z<br />

ω z<br />

ω z<br />

The tangential velocity pr<strong>of</strong>ile, at fully open port, is similar<br />

to a Burgers vortex i.e. an inner forced vortex core <strong>and</strong> free<br />

vortex outer region. The higher velocities are observed at<br />

some intermediate radial position between the cylinder wall<br />

<strong>and</strong> the geometric center where force <strong>and</strong> free vortex regions<br />

meet. With the downstream decay in swirl the size <strong>of</strong> the<br />

forced vortex region increases. At piston positions partially<br />

closing the port, the tangential velocity pr<strong>of</strong>ile starts changing<br />

to a forced vortex i.e. higher velocities are observed near<br />

the cylinder walls. This change in velocity pr<strong>of</strong>ile begins<br />

from cross-sectional positions near the cylinder outlet <strong>and</strong><br />

moves to upstream positions as the piston gradually closes<br />

the port. However, in case <strong>of</strong> piston position with 50 % port<br />

closure, the tangential velocity pr<strong>of</strong>iles resembled a walljet<br />

like pr<strong>of</strong>ile rather than the forced vortex. For the crosssectional<br />

positions close to the intake port, the partial closure<br />

<strong>of</strong> the intake port introduces asymmetry <strong>and</strong> variation in the<br />

mean tangential velocity pr<strong>of</strong>ile.<br />

Fully open ports result in an axial velocity with wakelike<br />

pr<strong>of</strong>ile at all measuring planes. However, no reverse<br />

flow at the vortex core has been observed. The downstream<br />

decay in swirl is decreasing the wake effect by transferring<br />

more mass into the wake region. As the piston starts closing<br />

the ports the axial velocity pr<strong>of</strong>ile changes from wake-like to<br />

jet-like at 50 % port closure. However, at 75 % port closure<br />

the jet-like mean axial velocity pr<strong>of</strong>ile at the cross-sectional<br />

position close to intake port changes back to wake-like at the<br />

9

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