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Settling behaviour of thin curved particles in quiescent fluid and turbulence

Published online by Cambridge University Press:  16 July 2021

Timothy T.K. Chan
Affiliation:
Physics of Fluids Group, Max Planck Center Twente for Complex Fluid Dynamics, Faculty of Science and Technology, MESA+ Research Institute, and J. M. Burgers Centre for Fluid Dynamics, University of Twente, P.O. Box 217, 7500 AE Enschede, The Netherlands Aerodynamics and Flight Mechanics Group, Faculty of Engineering and Physical Sciences, University of Southampton, Southampton SO17 1BJ, UK
Luis Blay Esteban
Affiliation:
Aerodynamics and Flight Mechanics Group, Faculty of Engineering and Physical Sciences, University of Southampton, Southampton SO17 1BJ, UK
Sander G. Huisman
Affiliation:
Physics of Fluids Group, Max Planck Center Twente for Complex Fluid Dynamics, Faculty of Science and Technology, MESA+ Research Institute, and J. M. Burgers Centre for Fluid Dynamics, University of Twente, P.O. Box 217, 7500 AE Enschede, The Netherlands
John S. Shrimpton
Affiliation:
Aerodynamics and Flight Mechanics Group, Faculty of Engineering and Physical Sciences, University of Southampton, Southampton SO17 1BJ, UK
Bharathram Ganapathisubramani*
Affiliation:
Aerodynamics and Flight Mechanics Group, Faculty of Engineering and Physical Sciences, University of Southampton, Southampton SO17 1BJ, UK
*
†Email address for correspondence: g.bharath@soton.ac.uk

Abstract

The motion of thin curved falling particles is ubiquitous in both nature and industry but is not yet widely examined. Here, we describe an experimental study on the dynamics of thin cylindrical shells resembling broken bottle fragments settling through quiescent fluid and homogeneous anisotropic turbulence. The particles have Archimedes numbers based on the mean descent velocity $0.75 \times 10^{4} \lesssim Ar \lesssim 2.75 \times 10^{4}$. Turbulence reaching a Reynolds number of $Re_\lambda \approx 100$ is generated in a water tank using random jet arrays mounted in a coplanar configuration. After the flow becomes statistically stationary, a particle is released and its three-dimensional motion is recorded using two orthogonally positioned high-speed cameras. We propose a simple pendulum model that accurately captures the velocity fluctuations of the particles in still fluid and find that differences in the falling style might be explained by a closer alignment between the particle's pitch angle and its velocity vector. By comparing the trajectories under background turbulence with the quiescent fluid cases, we measure a decrease in the mean descent velocity in turbulence for the conditions tested. We also study the secondary motion of the particles and identify descent events that are unique to turbulence such as ‘long gliding’ and ‘rapid rotation’ events. Lastly, we show an increase in the radial dispersion of the particles under background turbulence and correlate the time scale of descent events with the local settling velocity.

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 (http://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), 2021. Published by Cambridge University Press
Figure 0

Figure 1. The $Re$–$I^{*}$ phase space explored in the current study. The regime boundaries are taken from Field et al. (1997) and Smith (1971). Markers denote the particles considered, whose properties are listed in table 1.

Figure 1

Figure 2. (a) Bottle-fragment-like particle considered in this study. The dash–dot line is the axis of revolution used to obtain the dimensionless moment of inertia $I^{*}$, whereas $\alpha$ and $\beta$ are the pitch and roll angles, respectively. (b) Front view and (c) top view of particle with $\beta = 0$. (d) Drawings (to scale) of the four tested particles whose dimensions are listed in table 1. (e) Tank and release mechanism employed. Pumps and wire meshes are installed on both sides for symmetry, though only those on the right are shown to reduce clutter. The distance between the pumps is 165 cm. The tank rests on a steel frame with a rectangular window at the bottom to allow optical access. The coordinate system is shown on the top left.

Figure 2

Table 1. Dimensions of the particles dropped. Here $R$ is roughly constant at 19 mm while $\theta$ and $D$ are varied. The uncertainty is captured by the number of digits reported.

Figure 3

Figure 3. Reconstructed three-dimensional trajectories of particle no. 2 ($\theta = 73^{\circ }$, $D = 39$ mm) in quiescent fluid.

Figure 4

Table 2. The mean horizontal drift velocity $V_{drift}$, the dimensionless gliding section amplitude $A_g/R_g$, the precession rate $\dot {\gamma }$ of each particle and the moment of inertia of rotating it about an axis passing through its centre of gravity and parallel to its uncurved diagonal $I_{roll}$.

Figure 5

Figure 4. Descent of particle no. 2 ($\theta = 73^{\circ }$, $D = 39$ mm) after removing transient motions and dedrifting. (a) Three-dimensional and (b) top view of the trajectory reconstruction. (c) (From top to bottom) The radial displacement along the direction of motion $r_h$, the depth $z$ and the pitch angle $\alpha$ plotted against time $t$. No rolling motions are observed. (d) Velocity in the $y$-direction $V_y$ plotted against that in the $x$-direction $V_x$. (e) Instantaneous vertical velocity $V_z$ against the horizontal velocity $V_h= \pm (V_x^{2} +V_y^{2})^{{1}/{2}}$ whose sign switches every swing. All velocities and positions are normalised with the mean descent velocity $\langle V_z \rangle$ and diagonal length $D$ of the particle, respectively.

Figure 6

Figure 5. The mean settling velocities $\langle V_z \rangle$ of the particles. Unless further specified, the definitions of the data markers follow table 1 and vertical error bars represent the standard deviation of the measurements.

Figure 7

Figure 6. Plot of $Re$ against $Ar$. A linear relation is observed for the first three points and a kink seen for the last, which suggests a transition in settling style. As $Re(Ar)$ is one-to-one in the investigated range, the two are used interchangeably.

Figure 8

Figure 7. The (a) dimensionless radius of curvature of the trajectory in a vertical cross-section $L_{pend}/D$, (b) magnitude of the maximum pitch angle $\alpha _{max}$, (inset) average vertical slip angle over gliding sections $\varDelta \alpha$, (c) dimensionless radial oscillation amplitude $A/D$ and (d) Strouhal number $St = fD/\langle V_z \rangle$, where $f$ is the radial oscillation frequency, versus the Archimedes number $Ar$.

Figure 9

Figure 8. (a) Plot of the non-dimensional maximum horizontal speed in a swing $V_{h,max}/\langle V_z \rangle$. (b) Behaviour of the maximum vertical acceleration $a_{z,max}$. The grey symbols represent the descending pendulum model introduced in § 2.3. Inset shows $\alpha _{max}$ versus $a_{z,max}$ together with the best-fit line: $\alpha _{max} = (0.03\pm 0.01)a_{z,max} + (20.8\pm 6.8)$.

Figure 10

Figure 9. Model pendulum trajectory (grey line) overlaid on the experimental data of particle no. 2.

Figure 11

Figure 10. Fitting parameter $C$ as a function of $Ar$. In the context of underwater pendulums, $C$ is related to the added-mass coefficient $m_a^{*}$. Inset shows $m_a^{*}$ versus $Ar$.

Figure 12

Table 3. Statistics of the background turbulence such as the r.m.s. velocity fluctuations, the mean flow factor ($MFF$), homogeneity deviation ($HD$), integral length scales and Taylor microscales. Here $\lambda _f$ and $\lambda _g$ denote the longitudinal and transverse Taylor microscales, respectively. The reader is referred to Appendix A for the full definitions. The values in brackets correspond to the respective quantities in the column on the left.

Figure 13

Figure 11. Trajectories of particles in turbulent flow. Four special types of motions are observed though the underlying zigzag mode seen in quiescent fluid remains: (a) ‘slow descent’, (b) ‘rapid rotation’, (c) ‘vertical descent’ and (d) ‘long gliding motion’. The positions of the events within the trajectories are marked by square brackets on the side. Square markers denote locations corresponding to local minima of $V_z$.

Figure 14

Figure 12. (a) The p.d.f.s of $r_h/D$ along the descent. The solid line and solid data points are for quiescent fluid while the dotted one and hollow data points are for turbulent settling. The p.d.f.s of particles no. 1 (turbulent case only) and no. 3 are displayed. The inset shows the same quantity but for all the objects dropped. The symbols follow those introduced in table 1. (b) Vertical fluctuation kinetic energy per unit mass $E_{fluc}$ of the various particles.

Figure 15

Figure 13. (a) Mean descent velocities $\langle V_z \rangle$ of the various particles in turbulence and quiescent fluid. (b) Dimensionless version of the descent velocity plot, $Re(Ar)$.

Figure 16

Figure 14. (a) Scatter plots showing the relationship between the average descent velocities $V_{event}$ and frequencies $f_{event}$ per event. To better visualise the effect of background turbulence, these quantities are normalised by the mean descent velocity $\langle V_q \rangle$ and the dominant vertical oscillation frequency $f_q$ in quiescent fluid. The points corresponding to the special events shown in figure 11 – slow descent, rapid rotation, long gliding motion and vertical descent – are annotated. (b) The average $V_{event}$ against $f_{event}$ of all the events in panel (a).

Figure 17

Figure 15. The instantaneous descent velocities $V_z$ (solid lines) and the mean values $V_{event}$ (dotted lines) of the four types of events identified: (a) slow descent, (b) rapid rotation, (c) long gliding motion and (d) vertical descent. The green lines show the locations of the events.

Figure 18

Figure 16. The p.d.f. of $V_{event}$ relative to $\langle V_q \rangle$. To avoid overcounting slow events, the successive ones with $V_{event} < 0.4 \langle V_q \rangle$ have been merged.

Figure 19

Figure 17. The PIV measurements of the flow in the turbulence box. The time-averaged (a) r.m.s. flow velocity fluctuation field and (b) mean flow field at the middle of the tank. The subscripts $(x,z)$ denote the corresponding velocity components.

Figure 20

Figure 18. Autocorrelation functions $\rho _{ij}$ of the $j$-component velocity fluctuations along the $i$-direction. The solid lines give the measured data while the dashed line shows the exponential fit. The spacing between markers is not indicative of the resolution.

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