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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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