experimental study of droplet clustering in polydisperse...
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18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
Experimental study of droplet clustering in polydisperse sprays
Manish M1, Srikrishna Sahu 1,* 1: Department of Mechanical Engineering, IIT Madras, Chennai, India
* Correspondent author: [email protected]
Keywords: Droplet clustering, ILIDS, RDF, number density, turbulent flux
ABSTRACT
The clustering of droplets in a polydispersed spray is experimentally studied. The aim here is to understand
the cause of droplet clustering in sprays and study its consequence on local turbulent number flux of droplets.
Planar measurement of droplet position, number density and velocity is achieved by application of PIV technique,
while ILIDS technique is used for droplet sizing. Measurements are reported for an axial location 30 cm
downstream of the injector exit and different radial stations. Based on the measured droplet number count and
inter-droplet-distances, the length scale of the droplet clusters were quantified following two independent statistical
approaches, namely, droplet counting in a cell method and estimation of Radial Distribution function (RDF). The
results from both approaches are in agreement with each other. Towards outer region of the spray the length scale
of droplet clusters is found to be larger as well as the tendency of droplets to form clusters is higher. The
measurement area at any radial station is considered to consist of cells of same size, and both steady and turbulent
components of the average droplet number flux were calculated for cells of different sizes in comparison to the
length scale of the droplet clusters. While the steady number flux is almost independent of the cell size, the
magnitude of turbulent number flux is found to be higher for cell size similar to typical dimension of droplet
clusters in comparison to larger cell sizes. Also, relative to its steady value, the turbulent number flux increases
towards the edge of the spray. The correlation coefficient between fluctuations of droplet number density and
droplet velocity is found to be negative indicating smaller droplet velocity fluctuations for a droplet cluster for the
local drag seen by droplets within a cluster is different from individual droplets. The results show that droplet
clustering can lead to considerable local turbulent number flux especially towards the outer region of the spray.
1. Introduction
In liquid fuelled combustion, the combustion performance and emissions are mainly governed
by the atomization of the liquid fuel, the motion and evaporation of the fuel droplets and mixing
of fuel and air. So, spray dynamics studies are important to ensure efficient utilization of energy
as well as to better understand the mechanism of pollutants formation and control. Thereby,
unsteady spray behavior such as droplet clustering is of concern, for example, in problems
related to the unsteady flow of fuel into and through the combustion chamber (Heinlein and
Fritsching 2006). Droplet clustering can be caused due to unsteady disintegration of liquid
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
jets/sheets close to the injector. However, away from the injector due to wide range of droplet
size distribution in sprays, different dynamic behavior of droplet dispersion and interaction with
the surrounding gas lead to formation of clusters of droplets (Zimmer et al. 2003). Previous
studies on particle laden turbulent flows (Longmire & Eaton 1992; Wang and Maxey 1993;
Squires and Eaton, 1990) showed that neither large particles (with high Stokes number) nor small
particles (with very small Stokes number) exhibit the tendency to form clusters. Between these
two extremes exists a range of stokes number within which particles respond to some eddies but
not to others, and these particles tend to preferentially concentrate in certain flow structures
(Fessler et al. 1994; Ferrante and Elghobashi 2003). For a spray, the consequence of droplet
clustering can be critical since the instantaneous spatial distribution of droplets in sprays might
have dense and dilute regions, which strongly influence the subsequent evaporation of droplets,
and so the process of air-fuel mixture preparation. Sufficiently small inter-particle spacing with
in a droplet cluster prevents penetration of oxygen. Consequently, a fuel-rich mixture is formed
in which droplets do not burn individually, but rather in a group, which may affect flame
location and distributions of temperature, fuel vapor and oxygen (Chiu and Liu 1977).
The aim of the present paper is to understand the cause and consequence of droplet
clustering in isothermal sprays. A twin-fluid internal mixing air-assist atomizer is considered for
this purpose such that the liquid break-up process is completed close to the injector exit and
droplet clustering downstream is expected only due to interaction of droplets with the
surrounding air. Planar measurements of spray droplets are obtained using different laser based
diagnostic techniques. The focus of the paper is on quantifying the degree of droplet clustering
and estimation of clusters properties (cluster size and velocity, droplet size distribution).
Different statistical approaches have been developed in past (Fessler et al. 1994; Sundaram and
Collins 1999; Monchaux et al. 2010) for quantifying preferential accumulation of inertial particles
in particle-laden turbulent flows mostly in channels and wind tunnels. However, application of
such methods for quantitative measurement of droplet clustering in sprays has been considered
by few researchers in past (for example, see Lian et al. 2013; Sahu et al 2016). The present paper
also includes results for measurement of average liquid number flux (both steady and turbulent
fluxes), which is associated with the ability of the liquid fuel to react and vital for the
stability and extinction of the flames (Hardalupas et al. 1994). The correlation between droplet
number density and droplet velocity is obtained. Such correlation, which is apparently found to
be a consequence of droplet clustering, signifies spray unsteadiness. One of the purposes of the
present work is to obtain a comprehensive data set for droplet clustering statistics for different
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
liquid mass loading (by varying the air and the liquid volume flow rates). The results are
presented here for a water spray under ambient conditions.
2. Flow and Optical arrangement
Experiments are conducted with an air-assist internal mixing type injector (Spraying
system Co. 1/4 J series) generating a solid cone spray under ambient conditions. The flow circuit
and the optical arrangements are shown in figure 1. Water, pressurized at 1.5 bars in a pressure
vessel, was fed to the nozzle. The volume flow rates of water and air were controlled by different
rotameters with operating ranges of 20-200 ml/min and 7-70 lpm, respectively.
Measurement of droplet clusters and number density are achieved by planar laser sheet
imaging of the droplets. For this purpose, a double pulse Nd:YAG laser (Quantel, EverGreen:
145 mJ/pulse at 532 nm; 5 mm beam diameter) was used to illuminate the flow. The green laser
beam was expanded in to a sheet using a cylindrical lens (focal length: -25 mm) and a spherical
lens (focal length: +250 mm). The height and beam waist of the laser sheet were about 5 cm and 1
mm, respectively. The scattered light from droplets was collected through a lens (50 mm; f/1.8D
Nikon lens) along with a suitable band-pass optical filter. The images of focused droplets were
captured through a camera (PCO Pixelfly: 14 bit, 1,040 × 1,392pixels2) placed at an angle of 90◦
with respect to the laser sheet. The field of view was about 1.3 cm × 1.6 cm such that the spatial
resolution and magnification were 12 µm/pixel and 0.52, respectively. The droplet velocity is
measured by Particle Image Velocimetry (PIV) by capturing double frame images corresponding
to dual pulses of the laser. Since droplet size is not known, this way size-averaged droplet
velocity was measured. Thus, the first frame of each PIV image pair is used for measurement of
droplet clustering, while both frames are used for determining droplet velocity.
The droplet size is measured by the Interferometric Laser Imaging for Droplet Sizing
(ILIDS) technique. ILIDS is a planar defocusing technique based on detecting the reflected and
the first order refracted light scattered from a droplet, which, at a specific forward scattering
angle, interfere to produce parallel fringes on a defocused plane (Glover et al. 1995). The
characteristic interferogram is observed with a far field arrangement of receiving optics. The
number of fringes present in each of the recorded fringe patterns is proportional to the droplet
diameter. ILIDS has been successfully applied for droplet measurements for different spray
applications (Kawaguchi et al. 2002; Damaschke et al. 2005; Hardalupas et al. 2010). For ILIDS
measurements the camera was set at an angle of 69◦ forward scattering angle. The object distance
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
was about 16 cm and the collecting angle was about 10◦ resulting in diameter/fringe equals to
about 4.5 microns.
Fig. 1 Schematic of the experimental setup.
The nozzle was mounted on an aluminum frame and was traversed for measurements at
different axial and radial locations within the spray. The laser repetition rate was set to 5 Hz
such that the acquired images remained statistically uncorrelated. For each measurement
locations 1000 images are captured. In house developed image processing software‟s based on
MATLAB were used for processing the raw images from different techniques.
3. Results & Discussion
Fig. 2 Shadowgraph images of the spray for various air and water flow rates.
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
In order to depict the influence of liquid mass loading on droplet dispersion in the spray few
shadowgraph images of the spray are presented in Fig. 2. Figures 2(a-e) show the images for
different air flow rates (𝑄��) while the water flow rate (𝑄��) is kept constant. As the droplet size is
expected to be smaller with increasing air flow rate for the same flow rate of water, and small
droplets show better response to the carrier flow partly induced by the spray itself, branches like
structures appear within the spray. However, as the water flow rate increases for the same air
flow (compare Fig.2f to Fig.2e), though the droplet size is expected to increase these structures
are more noticeable and droplet clustering is qualitatively more prominent. This suggests
importance of quantitative measurements of clustering in the spray.
The results presented below correspond to two different operating flow conditions where
the air flow rate is maintained constant (𝑄��= 25 ml/min and 𝑄𝑎 = 25 lpm; 𝑄��=50 ml/min and
𝑄��= 25 lpm). The measurements are obtained 30 cm downstream of the nozzle exit, and the
measurement stations are situated at different radial stations from the spray axis (denoted as R =
0 mm, 20 mm and 30 mm, respectively).
3.1 Measurement of droplet clustering
The tendency of droplets to form clusters and also the length scale of the clusters were quantified
based on two independent statistical methods viz. “droplet counting in a cell approach” and
estimation of “radial distribution function (RDF)”, respectively. For this purpose, the positions of
droplets on images must be identified. In the present work, the center of each droplet on an
image is identified following Otsu‟s method of image thresholding and subsequent reduction of
a graylevel image to a binary image. Usually before binarizing, the images are band-pass filtered
to remove the noise due to multiple reflections and current leekage from saturated pixels. We
studied the influence of the cut-off values of the employed band-pass filter using the image
processing software, ImageJ on droplet clustering measurements. It was found that for the
present measurements, the choice of those cut-off values has minimal influence on the
estimated length scale of droplet clusters. Also, though, droplet number count reduces with
increasing the cut-off values, as expected, the relative values of fluctuations to mean droplet
count is not affected. Hence, the results presented in the paper corresponds to the case of no
band-pass filtering. A typical raw image of the droplets and the identified droplet centers are
shown in Fig. 3.
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
(a)
(b)
Fig. 3: (a) Typical instantaneous image of the spray (b) Binarized image showing identified droplets
In the “droplet counting in a cell” approach the image is divided in to certain number of equally
sized cells (as shown in fig 3). The probability density function (PDF) of the droplet number
density is obtained by counting the number of droplets inside each cell. The ensemble averaged
PDF (over all images) is compared with that arising from a purely random distribution of
droplets (given by a Poisson distribution). The normalized difference between the standard
deviations of the PDF‟s is termed as D1 parameter, such that (D1 = 𝜎−𝜎𝑝
𝜆 , where λ is the average
droplet count in a cell). The value of D1 indicates the degree of clustering such that the box size
for which D1 is the maximum indicates the length scale of the droplet clusters (Lc). This is
demonstrated in Figure 4 for the two different operating flow conditions and same location at R
= 0 mm. Figure 4 also shows that clustering is higher for the case of larger flow rate of water
though the length scales of the droplet clusters remain nearly same (150 pixels or about 2 mm).
Similarly, D1 is evaluated for other measurement locations. Figure 5 shows radial variation of D1
for a given box size of 150 by 150 pixel2. The figure indicates greater preferential accumulation of
droplets towards the edge of the spray.
Fig. 4 Demonstration of the “droplet counting in a cell” method for the considered operating flow conditions and location R = 0 mm.
Fig. 5 Radial variation of D1
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
Though the droplet counting in a cell approach provides local information on droplet
clustering, the result is always ensemble averaged. On the other hand, the radial distribution
function (RDF) can provide instantaneous cluster size and the information is not local. RDF is
defined as the probability of finding a second droplet at a given separation distance from a
reference droplet compared to a case where the droplets are homogeneously distributed
(Sundaram et al 1999). Figure 6a schematically shows the method of calculation of RDF. In this
process, a series of concentric circles are considered around a droplet on an image. The droplet
count between consecutive radii (r-Δr and r+Δr) provides the number of droplets within the
annular area around a separation distance, „r‟. This is repeated for the different radial separation
distances and for all droplets on the image. The ensemble average of droplet counts for each „r‟
provides the RDF according to the following equation,
𝑅𝐷𝐹 (𝑟) = [(𝑁_𝑎𝑛𝑛𝑢𝑙𝑎𝑟 (𝑟)) ⁄ (𝐴_𝑎𝑛𝑛𝑢𝑙𝑎𝑟 (𝑟) )]/ [𝑁𝑡𝑜𝑡𝑎𝑙 ⁄ 𝐴𝑡𝑜𝑡𝑎𝑙 ]
where Ntotal/Atotal denotes average number of particles per unit area of the image. A typical RDF
corresponding to an instantaneous image is shown in Fig. 6b. RDF > 1 indicates clustering, while
RDF < 1 implies presence of voids in the image. Thus, the separation distance where RDF = 1
should provide an estimation of length scale of droplet clusters.
(a) (b)
Fig. 6: (a) Method of calculation of RDF (b) An instantaneous RDF indicating drpolet clustrs and voids.
Fig 7: RDF for different instantaneous
images calculated for 𝑄��=50 ml/min and
𝑄��= 25 lpm for R = 0 mm location.
Fig. 7 shows the RDF‟s for several instantaneous images for 𝑄��=50 ml/min and 𝑄��= 25 lpm for R
= 0 mm location. It can be observed that even if the air and water flow rates are constant the
length scale of droplet clusters (corresponding to RDF = 1) as well as the tendency of droplets to
form clusters denoted as RDFmax(maximum value of a given RDF at minimum separation
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
distance) vary considerably as depicted by double ended arrows in the same figure. The average
cluster length is obtained by arithmetic mean of the instantaneous values. Fig. 8a and 8b
respectively present variation of average cluster length (Lc) and average RDFmax for the two
liquid flow rates and different radial measurement locations. The error bars indicate statistical
uncertainty with 95% confidence interval. The results are in good agreement with the findings
via evaluation of the D1 parameter. It can be observed in Figure 8 that towards the edge of the
spray the droplets have greater tendency to preferentially accumulate in certain regions of the
flow which was in accordance with the trend of D1 parameter presented earlier.
Below we show in Fig. 9 the same quantities as in Fig. 8 for different cut-offs for the band-pass
filter, which confirms that such thresholding has minimal influence on droplet cluster
characteristics.
(a) (b)
Fig. 8: (a) Radial evolutionof average cluster length scale (b) average RDFmax for the two flow operating conditions.
(a) (b)
Fig. 9: Effect of band-pass filtering on average (a) cluster length scale (b) RDFmax. Here two sets of the cut-off limits
are considered for band-pass filtering (1-10 and 1-20).
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
3.2 Measurement of droplet size by ILIDS
A typical ILIDS image is presented in Fig. 10a, which shows circular fringe patterns
corresponding to each droplet. The images are first binarized using Otsu algorithm followed by
Hough transform to identify the centers of each droplet fringe pattern and measure its diameter.
The intensity values along a horizontal line passing through center of a circular pattern and
corresponding to a length few pixels more than its diameter are considered, whose Fourier
transform (in conjunction with Gaussian sub pixel interpolation) determines the spatial
frequency of the fringe pattern. A hanning window is used to minimize the spectral leakage. A
histogram of the droplet size measured by ILIDS corresponding to liquid flow rate of 50 lpm and
location R = 0 mm is shown in Fig. 10b. It can be observed that small droplets (20-30 µm)
dominate the size distribution. The Arithmetic Mean Diameter (AMD) was estimated to be about
30 μm, while the Sauter Mean Diameter (SMD) was about 40 μm.
(a) (b)
Fig. 10: (a) Typical ILIDS image (b) Histogram of droplet diameter 𝑄��=50 ml/min and 𝑄��= 25 lpm for R = 0 mm
location
3.3 Measurement of droplet velocity and number density
For measurement of instantaneous droplet velocity and number density each PIV image is
divided into cells of equal size and these quantities are calculated for each cell. The cell size is
always kept same for both quantities, and decided on the basis of estimated average cluster
dimension as determined in the previous section by D1 parameter and RDF. The purpose behind
this is to study the role of droplet clustering on local mean and turbulent droplet number fluxes,
which, as mentioned earlier, have significance in temporal and spatial distribution of liquid
volume in spray combustion systems. The results presented below are for interrogation window
size of 150 pixels in both directions, which is same as the estimated length scale of the droplet
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
clusters (Lc). The consequence of choice of window dimension either larger or smaller than the
cluster length scale will be explained later. In order to restrict the length of the paper, we present
results only for one operating flow condition ( Qw= 50 ml/min and Qa= 25 lpm)
Each pair of double exposure PIV images were processed based on direct image cross-
correlation (Raffel et al 2013) to obtain instantaneous droplet velocity vectors. The instantaneous
PIV realizations are ensemble averaged over all images to obtain mean droplet velocity. Fig. 11
presents vector plots for the mean droplet velocity downstream measurement locations. It can be
observed in Fig 11 that as expected the mean droplet velocity is mostly axial and it reduces away
from the spray axis. The fluctuations in droplet velocities are determined by subtracting the
mean velocity from instantaneous values.
Fig. 11: Mean droplet velocity vector plots for different radial location for 𝑄��=50 ml/min and 𝑄��= 25 lpm
For measurement of instantaneous droplet number density (N), the number of identified
droplets is counted for each cell whose volume is defined by the cell area and laser sheet
thickness.
The results presented in rest of the paper correspond to the row of cells passing through the
center of a measurement location. The variation of any statistics with respect to the radial
locations is presented for the three radial measurement stations together in a single plot. The
radial variation of mean and root mean square (rms) of fluctuations of droplet axial velocity and
droplet number density are shown in figures 12a and 12b, respectively. The errorbars represent
uncertainty with 95% confidence interval. The mean and fluctuations, as expected, reduce away
from the central spray region, the fluctuations of droplet velocity and number density are
considerable (30-50%) relative to the respective mean values.
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
(a) (b)
Fig. 12: Radial variation of average and fluctuations of (a) droplet velocity (b) droplet number density.
In order to estimate the droplet response to gas velocity fluctuations and also compare the
droplet cluster dimension to different length scales of the surrounding turbulent flow, the air
turbulence must be characterized. Since the air velocity is not measured in our experiments, we
assume that the droplets follow the air flow faithfully since the measurement location is far
below the injector exit and we calculate the turbulent characteristics based on the fluctuations of
droplet velocity. The integral length scale is estimated as one-fifth of the spray radius. The
Kolmogorov scales are obtained via dissipation rate, which is calculated from the droplet rms
velocity and integral length scale (Tennekes & Lumley 1972). We emphasize that because of the
assumptions made above the turbulent characteristics as presented in Table 1 can only be
considered in an order of magnitude sense.
Gas velocity fluctuation≈ ur 1.25 m/s
Integral length scale ≈ 1.0 cm
Integral time scale ≈ 8.55 ms
Dissipation rate ≈ 160 m2
/s3
Kolmogorov length scale ≈ 67 µm
Kolmogorov time scale ≈ 0.31 ms
Turbulent Reynolds number ≈ 780
Particle relaxation time ≈ 4.8 ms
Table 1: Turbulent characteristics of the flow at the center of the spray
Table 1 shows that most droplets are smaller than the Kolmogorov length scale but not
negligible. The droplet Stokes numbers based on integral and Kolmogorov time scales are StL=
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
0.5, Stη = 15, indicating partial and poor response of droplets to large and small turbulent eddies.
Also the cluster length scale is about 30 times the Kolmogorov scale.
3.3 Measurement of droplet number flux
The droplet number flux i.e. number of droplets moving across unit area normal to the flow per
unit time is obtained as a product of droplet number density and velocity. It can be shown that
the average number flux (denoted as 𝑁𝑈 ) is the sum of the steady flux (𝑁 × 𝑈 ) and the turbulent
flux (𝑛′ × 𝑢′ ). The latter is essentially the correlation between fluctuations of droplet number
density and velocity. Though, the turbulent flux is often neglected, which is partly due to the
difficulty associated with its measurement, it can be important when droplets partially respond
to the carrier phase turbulent gas flow, as in the present case. The situation can be of even more
significance when droplets tend to form clusters as a consequence of the two-phase interaction
process since this directly affects the evaporation rate of droplets and ability of droplets to react.
Figure 13a and 13b show, respectively, the radial variation of the steady and the turbulent
components of the average number flux, which reduce away from the central region of the
spray. It can also be observed that the correlation between fluctuations of droplet number
density and velocity is negative and non-negligible at the present measurement locations as its
importance relative to the steady flux (ratio between the two quantities) increases towards the
spray edge from about 5% to about 50%. The correlations normalized with rms values (or the
correlation coefficients) are presented in figures 14a and 14b for both axial and radial velocity
components. For both cases the correlation coefficients are negative and increase towards the
edge of the spray. This is attributed to droplet clustering for the drag on droplets in a cluster is
different from the case when droplets are transported individually. Thus, the gas velocity
fluctuations are smaller (𝑢′< 0) for a group of droplets passing through the measurement
location (𝑛′>0), and positive (𝑢′> 0) after the passage of the droplet group (𝑛′<0), hence the
correlation is negative. Since the significance of radial transport of droplets is realized away from
the spray axis, the correlation coefficient for radial velocity component is high (≈ 0.5) near the
spray boundary though the magnitude of correlation is much lower in comparison to that for the
axial velocity. The above result signifies that the average droplet number flux is overestimated if
the turbulent flux is not taken in to account.
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
(a)
(b)
Fig. 13 : Radial variation of (a) steady number flux and (b) turbulent number flux
(a)
(b)
Fig. 14 : Radial variation of (a) normalized axial flux, 𝑛′ × 𝑢′ and (b) normalized radial flux, 𝑛′ × 𝑣′
3.3.1 Effect of cell size on droplet number flux
Since droplet clustering occurs predominantly at viscous scales, while transport of clusters are
affected by large scale eddies, the turbulent number flux of droplets is a scale variant quantity.
Hence, the measured droplet statistics are obtained for different cell sizes relative to the
estimated length scale of the droplet clusters (cell size ranging from half of the cluster dimension
(0.5×Lc) up to 8 times the dimension of clusters (8×Lc)). In general, the uncertainty for the
smallest cell size is higher. The largest cell size nearly corresponds to the whole measurement
window.
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
(a) (b)
Fig. 15: Radial variation of (a) steady number flux. (b) turbulent number flux for various cell sizes.
Figures 15a and 15b present the steady and the turbulent number flux for cells of different sizes.
The respective statistical uncertainties with 95% confidence interval are about 3 - 8% and 27 - 30
%. The uncertainty is higher for smaller cell sizes due to less number of droplets present within a
cell. It is observed that the steady flux is nearly independent of the cell size though it is
consistently higher for cell size equal to Lc. Though not shown here similar observation was
found for the mean droplet number density, which was higher for cell size equal to Lc especially
for locations away from the spray axis, and this trend is in agreement with the results based on
D1 parameter and RDF. However, the mean droplet velocity was nearly independent of the cell
size, which is in accordance with the vector plots in Fig. 11. Thus, the trends in figure 15a are
justified. However, the fluctuations of droplet number density was found to reduce for larger
cells consistently (not shown here). The droplet velocity fluctuations were nearly independent of
the cell size though the uncertainty was higher for the smaller cell size. Figure 15b shows that for
cell sizes larger than the dimension of clusters the turbulent number flux is smaller. The results
presented here indicate that preferential accumulation of droplets can lead to turbulent mass
flux when measured over a length scale of the order of dimension of droplet clusters and
especially for near spray boundary region, and hence may not be considered negligible.
4. Conclusion
The present work focuses on quantitative measurement of droplet clustering in sprays
with an aim to study some of the important consequence of clustering including uneven
distribution of liquid fuel mass within the spray and increased significance of turbulent mass
flux. Experiments were conducted for a polydispersed spray generated by a twin fluid air-assist
atomizer. Droplet number density and droplet velocity measurements were obtained by the
18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
application of planar laser sheet imaging of the spray droplets, while droplet sizing was
achieved by ILIDS technique. Two independent statistical methods are used to quantify the
length scales of droplet clusters as well as the tendency of droplets to form clusters. The
measurement area at any radial station is considered to consist of cells of same size, and results
including measurements of basic spray characteristics and droplet number flux are presented for
row of cells through the center of the measurement area. The statistical uncertainties of the
measured quantities are also presented. The effect of the choice of intensity cut-off values while
band-pass filtering the images was found to negligibly affect the measured droplet clustering
statistics.
The preferential accumulation of droplets was found to be higher towards the spray boundary,
where the length scale of the droplet clusters was also larger. As a consequence, the turbulent
number flux was negative and its magnitude was comparable to the steady number flux
especially away from the spray axis. Also, importantly, the turbulent number flux was smaller
for cell sizes larger than the estimated cluster dimension. The presented results are also of
significance for two-phase flow models for spray simulations.
The authors would like to acknowledge the support given by IITM for the conduct of the
research. MM acknowledges his teammates Abhijeet, Shirin, Kumari, Sai, Chaithanya, Visnu and
Azhivazhagan for all the help provided.
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18th International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics・LISBON | PORTUGAL ・JULY 4 – 7, 2016
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