hc y7a ff2 fs8 fc0 sc0 ls1 ws1">Mirror
1
2
Pr
o
fil
e
x
y
z
Figure 2. Scheme of the test section.
2.2. Running Conditions of Experiments
The investigations have been carried out for the coflow-to-jet
flow rate ratio equal to 5 at which the exit jet velocity was tur-
bulent at the Reynolds number Red =104.
The intensity of mixing was controlled by mouthpieces that
were installed in the nozzle (Figure 3).
Four mouthpieces with the same inner diameter (d=0.01 m)
were used: the reference one without tabs (D0), the mouthpiece
with rectangular tabs h = 1.5 10-3 m (D1), the mouthpieces with
triangular tabs h=1.3 and 1.8 10-3 m (D2) and (D3) correspon-
dently. So, the influence of sizes and configurations of the tabs
on mixing can be estimated. The exit cross sections of the
mouthpieces were reduced to 12 % for D1 and to 8 and 16% for
D2 and D3 in comparison with the cross section of the refer-
ence one (D0). This reduction of cross sections resulted in the
higher exit velocities because the value of the jet flow rate was
the same in these investigations.
The laser sheet crossed the mixer in the vertical plane along
its centre line (z = 0). This light was reflected from the particles
in the flow and exited the dye molecules, which started to radi-
ate the light at the longer wavelength. The reflected light off the
particles was collected by camera with the laser-line band pass
interference filter 532nm (Edmund Optics). The radiated light
of the dye molecules passed through the broad pass filter
BP600 nm with 50nm FWHM (Edmund Optics) and was col-
lected by another camera.
Preliminary studies of different but uniform dye concentra-
tions of Rh 6G were executed. A short glass cylindrical volume
identical to the mixer was filled with dye solutions and placed
into the same glass box with the water. Series of 200 images
were recorded and then averaged at each pixel. Besides, series
dark images were recoded to determine the grey value offset for
each pixel. The difference of these images yields the light in-
tensity distribution that corresponds to the determined dye con-
centration. Due to the each pixel calibration, the Gaussian na-
ture of the laser beam, which results in the variations of the dye
intensity over the laser sheet, were taken into account.
To calculate statistical characteristics of the velocity and
scalar fields of the mixed flows 2000 images were captured by
each camera at seven positions along the mixer length.
3. Results
The jet bifurcation was developed just behind the nozzle with
the mouthpieces D1-D3. Therefore the measurements were
done for two positions of these mouthpieces in the planes dif-
fering by 45°. At first the mouthpiece was installed in the noz-
zle so that the vertical laser sheet coincided with the two oppo-
site tabs (the plane of 0°). In this case the pairs of the
counter-rotating vortices generated by the tabs produced the
vertical fluxes to the jet axis, i.e. the positive cross velocities
appeared at the lower jet part and the negative one at the upper
jet part (Figure 4(a)).
Figure 3. The mouthpieces applied in experiments, from left to
right D0, D1, D2 - D3.
Copyright © 2012 SciRes. AMPC
V. ZHDANOV, E. HASSEL
136
The longitudinal velocity and scalar profiles in this plane
be
ases of the
m
y field started to be uniform at x/D=9 where the
fl
came narrower (left part of Figure 4(b),(c)). The second row
measurements were done when the mouthpieces were rotated
by 45°. At this position the fluxes generated by the vortices
from different pairs were ejected outside the jet axis and the
velocities and concentrations profiles became wider (right part
of Figure 4(b),(c)). The distributions of the velocity and con-
centrations in the measured cross sections were normalized on
their values at the mixer centre line (U0 and C0).
The jet bifurcation decays downstream and in the c
outhpieces of D1 and D2 the longitudinal velocity and fluc-
tuations profiles at the distance x/D=3 did not differ in both
measured plans while the concentrations profiles showed some
differences even downstream in the case of D2 (Figure 5). The
jet expanded stronger than the jet issued from the reference
mouthpiece.
The velocit
uctuations did not practically distinguish for all considered
cases (Figure 6(a)). The cross velocity and its fluctuations had
the same order and varied a few across the mixe r (Figure 6(b)).
Figure 4. The distributions of the cross velocity (a) longitudinal
velocities (b) and concentrations (c) just behind the nozzle at dif-
ferent positions of the mouthpieces.
Figure 5. The velocity and concentration distributions behind the
mouthpieces D0 and D2 at the distance x/D=3.0.
Figure 6. The velocities and scalar distributions at the distance x/D
he uniform scalar field was formed already at x/D=7 when
= 7, 9.
T
mouthpieces D1-D3 were used (Figure 6(c)). The difference in
the concentration distributions in two planes was already insig-
nificant. The application of the mouthpiece D3 provided the
Copyright © 2012 SciRes. AMPC
V. ZHDANOV, E. HASSEL
Copyright © 2012 SciRes. AMPC
137
inal mean velocities, con-
ce
oncentration (U, C) and the
va
e en-
tr
s in mixing, as already has
be
us mixture, where the
ve
faster formation of the quasi-homogeneous mixture in com-
parison with the other mouthpieces.
Decays of the normalized longitud
ntrations and their fluctuations along the mixer axis down-
stream the nozzle demonstrate the dynamics of the tabs influ-
ence on mixing (Figure 7(a),(b)).
Exit values of the velocity and ci i
lues of these parameters at the mixer axis (U0 and C0) at the
measured cross sections were used for the normalization of the
fluctuations downstream the flow. The first normalisation shows
the evolution of velocity and scalar fields along the mixer length
and the second one gives the dynamics of the fluctuation–to-
local velocity ratio. This parameter presents the development of
the turbulence level in the flow. The correlation of the present
measurements with the known ones [13] was quite well.
The tabs forced the co-flow entrainment into the jet. Th
ainment started earlier and was accompanied by the decrease
of the mean velocity and the concentration, and by the growth
of the fluctuations. Maximum of the fluctuations was moved to
the nozzle directions (at x/D=0.3 for D3). Because the mean
values of the velocity and the concentration decreased stronger
than the fluctuations ones, the local ratios u’/U0, c’/C0 at the
mixer axis increased downstream. The scalar parameters de-
cayed faster than the velocity one.
The advantage of the triangle tab
en noted in the references [1,9], can be seen within the inter-
val of 0 < x/D < 3 for the mouthpiece D2 against D1. With
smaller blockage effect the mouthpiece D2 more intensively
involved the co-flow fluid to the jet and resulted in the same
mixture quality to the distance x/D=5.
The formation of the quasi-homogeneo
locity and scalar gradients fast degenerated and the fluctua-
tions distributions across the mixer were nearly uniform, was
completed in the case of the mouthpiece D3 minimum about
10d earlier in comparison with the case when the jet was issued
from the mouthpiece D0.
Figure 7. Decay of the velocity and concentration fields inhe
l jet mixer was investigated applying si-
fluxes generated by tabs resulted in the earlier en-
tr
y the German Research Founda-
[1] K. B. M. Q. Zamristics of compressible
and X. K. Wang, “Measurements in the
d Measurements in an Equilatera Trian-
os, J. W. Bitting, B. Rouge, and S. Gogineni,
J. Majamaki, I. T. Lam, O Delabroy, A.
mith, and A. R. Karagozian, “Passive
he distortion of a jet by
er, “Effect of
mimy, “Control of an
y, “The evolution of a jet with vor-
rtical
. Koh, “Experimental Investigation of
Hassel and A. Chorny, “Mixing of
tmixer confined coaxial flows”, Int. J. Heat and Mass Transfer, pp.
3942-3956, 2006
with different mouthpieces.
4. Conclusions
Mixing in the coaxia
multaneously methods PIV and PLIF. The development of the
velocity and concentration field was controlled by the mouth-
pieces with different tabs installing in the nozzle. The mixing
enhancement has been observed at all kinds of investigated tabs,
i.e., the tabs of relative small sizes (0.13 h/d 0.18) are quite
effective also in the developed turbulent jet. The advantage of
the triangular tabs against the rectangular ones also has been
supported.
The cross
ainment of the co-flow fluid to the jet and forced the jet to
expand faster.
5. Acknowledgements
The study has been supported b
tion (DFG).
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