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Liquid inertia versus bubble cloud buoyancy in circular plunging jet experiments

Published online by Cambridge University Press:  05 January 2024

Narendra Dev
Affiliation:
Univ Lyon, Univ Claude Bernard Lyon 1, CNRS, Ecole Centrale de Lyon, INSA Lyon, LMFA, UMR5509, 69622 Villeurbanne, France
J. John Soundar Jerome
Affiliation:
Univ Lyon, Univ Claude Bernard Lyon 1, CNRS, Ecole Centrale de Lyon, INSA Lyon, LMFA, UMR5509, 69622 Villeurbanne, France
Hélène Scolan
Affiliation:
Univ Lyon, Univ Claude Bernard Lyon 1, CNRS, Ecole Centrale de Lyon, INSA Lyon, LMFA, UMR5509, 69622 Villeurbanne, France
Jean-Philippe Matas*
Affiliation:
Univ Lyon, Univ Claude Bernard Lyon 1, CNRS, Ecole Centrale de Lyon, INSA Lyon, LMFA, UMR5509, 69622 Villeurbanne, France
*
Email address for correspondence: jean-philippe.matas@univ-lyon1.fr

Abstract

When a liquid jet plunges into a pool, it can generate a bubble-laden jet flow underneath the surface. This common and simple phenomenon is investigated experimentally for circular jets to illustrate and quantify the role played by the net gas/liquid void fraction on the maximum bubble penetration depth. It is first shown that an increase in either the impact diameter or the jet fall height to diameter ratio at constant impact momentum leads to a reduction in the bubble cloud size. By measuring systematically the local void fraction using optical probes in the biphasic jet, it is then demonstrated that this effect is a direct consequence of the increase in air content within the cloud. A simple momentum balance model, including only inertia and the buoyancy force, is shown to predict the bubble cloud depth without any fitting parameters. Finally, a Froude number based on the bubble terminal velocity, the cloud depth and also the net void fraction is introduced to propose a simple criterion for the threshold between the inertia-dominated and buoyancy-dominated regimes.

Information

Type
JFM Papers
Creative Commons
Creative Common License - CCCreative Common License - BY
This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (https://creativecommons.org/licenses/by/4.0), which permits unrestricted re-use, distribution, and reproduction in any medium, provided the original work is properly cited.
Copyright
© The Author(s), 2024. Published by Cambridge University Press
Figure 0

Figure 1. (a) Schematic of the control volume of the bubble cloud. (b) Schematic of the experimental set-up, illustrating flow lines to generate the bubble cloud, the backlighting imaging set-up and the void fraction measurement set-up with optical probes.

Figure 1

Table 1. Flow conditions in previous works on vertical ($\downarrow$), inclined ($\swarrow$) and oscillating ($\rightleftarrows$) plunging jets from circular ($\bigcirc$) and planar ($\unicode{x25AD}$) nozzles. All authors used water. Data in Lin & Donnelly (1966) refer also to oil and glycol jets.

Figure 2

Figure 2. Variation of $H$ with the square root of the impact momentum $\sqrt {V_iV_n}\,D_n$ for $D_n = 2.7$ and 8 mm at various $Z_f/D_n$. The dotted line shows the trend expected from (1.1). The dashed line shows the $2/3$ scaling law expected at large scales. The inset graph is a blow-up of the $D_n=8$ mm data showing that increasing $Z_f$ at constant impact momentum leads to a decrease in $H$. The data points I–VI correspond to the flow conditions that are compared in § 3.2.

Figure 3

Figure 3. (a) Axial evolution of the void fraction $\phi _0 (z)$ for two different ratios $Z_f/D_n$ at a fixed jet diameter $D_n = 2.7$ mm and $\sqrt {V_iV_n}\,D_n = 0.016\pm 0.0002\ {\rm m}^2\ {\rm s}^{-1}$. Instantaneous images of the freely falling jet just before impact: (b) $Z_f /D_n = 20$; (c) $Z_f /D_n = 50$.

Figure 4

Figure 4. (a,c) Instantaneous pictures of the falling jet just before impact for $D_n = 2.7$ and $8$ mm, respectively, at constant $\sqrt {V_iV_n}\,D_n = 0.028\ {\rm m}^2\ {\rm s}^{-1}$ and $Z_f/D_n = 20$. Corresponding bubble clouds are shown as well. (b,d) The radial variation of $\phi (r, z)$ at three different depths in the bubble cloud, for the $2.7$ mm and $8$ mm jets, respectively.

Figure 5

Figure 5. Images of the $D_n = 8$ mm jet just before impact for (a) $Z_f/D_n = 20$ and (c) $Z_f/D_n =100$, for a constant $\sqrt {V_iV_n}\,D_n = 0.075\ {\rm m}^2\ {\rm s}^{-1}$. Corresponding bubble clouds are shown as well. (b,d) The radial variation of $\phi$ at various depths in the bubble clouds for $Z_f/D_n = 20$ and 100, respectively.

Figure 6

Figure 6. Variation of $\epsilon$ and $\bar {\phi }_{0}$ with $\sqrt {V_iV_n}\,D_n$ for $D_n = 8$ mm, where $\bar {\phi }_{0}$ is the average over depth of the maximum void fraction measured along the axis. Both $\epsilon$ and $\bar {\phi }_{0}$ increase when $Z_f$ is increased for a constant jet momentum.

Figure 7

Figure 7. Measured profiles of air/water void fraction for the nozzle diameter $D_n = 8$ mm and different fall heights (a) $Z_f/D_n = 20$, (b) $Z_f/D_n = 50$ and (c) $Z_f/D_n = 100$, at various values of Q = $\sqrt {V_iV_n}\,D_n$. Gaussian fits are represented by continuous lines.

Figure 8

Figure 8. (a) Comparison of the experimental depth $H$ with values predicted by the model $H_b$. (b) Normalized depth $H/H_i$ at various values of $Fr$ for injectors from current and past studies whose void fraction is known. Equation (3.2) is represented by the continuous line.

Figure 9

Figure 9. (a) Bubble cloud depth ($H$) data from previous investigations are presented here as a function of $\sqrt {V_iV_n}\,D_n$, a measure of the impact momentum, to illustrate the two distinct dynamical regimes identified in our study over a wide range of scales. (b) When the void fraction is not known, $Fr^*$ can still sort past experiments into inertia- or buoyancy-dominated regimes, even though more dispersion is observed.

Figure 10

Figure 10. (a) Definition of $\phi _{b}$ and $R_{b}$. (be) Variation of $\phi _{b}$ and $\gamma _{b}$ with $Z_f/D_n$ for the two injector sizes at various impact momentum values. Two colour bars are provided for the two ranges of $\sqrt {V_iV_n}\,D_n$, corresponding to both $D_n$ values.

Supplementary material: File

Dev et al. supplementary movie 1

Dn= 2.7 mm Vi = 5.92m/s Hf/Dn=20
Download Dev et al. supplementary movie 1(File)
File 7 MB
Supplementary material: File

Dev et al. supplementary movie 2

Dn=2.7 mm Vi =6.05 m/s Hf/Dn=50
Download Dev et al. supplementary movie 2(File)
File 7.2 MB
Supplementary material: File

Dev et al. supplementary movie 3

Dn= 2.7 mm Vi = 10.26m/s Hf/Dn=20
Download Dev et al. supplementary movie 3(File)
File 4.6 MB
Supplementary material: File

Dev et al. supplementary movie 4

Dn= 2.7 mm Vi = 10.26m/s Hf/Dn=20
Download Dev et al. supplementary movie 4(File)
File 7 MB
Supplementary material: File

Dev et al. supplementary movie 5

Dn=8 mm Vi =3.76 m/s Hf/Dn=20
Download Dev et al. supplementary movie 5(File)
File 5.8 MB
Supplementary material: File

Dev et al. supplementary movie 6

Dn=8 mm Vi =3.76 m/s Hf/Dn=20
Download Dev et al. supplementary movie 6(File)
File 2 MB
Supplementary material: File

Dev et al. supplementary movie 7

Dn= 8 mm Vi = 9.6 m/s Hf/Dn=20
Download Dev et al. supplementary movie 7(File)
File 5.4 MB
Supplementary material: File

Dev et al. supplementary movie 8

Dn= 8 mm Vi = 9.6 m/s Hf/Dn=20
Download Dev et al. supplementary movie 8(File)
File 9.6 MB
Supplementary material: File

Dev et al. supplementary movie 9

Dn=8 mm Vi = 9.8 m/s Hf/Dn=100
Download Dev et al. supplementary movie 9(File)
File 9.9 MB
Supplementary material: File

Dev et al. supplementary movie 10

Dn=8 mm Vi = 9.8 m/s Hf/Dn=100
Download Dev et al. supplementary movie 10(File)
File 5 MB