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Freely falling sphere with a rigid rear-side filament

Published online by Cambridge University Press:  09 May 2025

Seungho Choi
Affiliation:
Department of Mechanical Engineering, KAIST, Daejeon 34141, Republic of Korea
Minhyeong Lee
Affiliation:
Department of Mechanical Engineering, KAIST, Daejeon 34141, Republic of Korea
Chris Roh
Affiliation:
Department of Biological and Environmental Engineering, Cornell University, Ithaca 14853, USA
Daegyoum Kim*
Affiliation:
Department of Mechanical Engineering, KAIST, Daejeon 34141, Republic of Korea
*
Corresponding author: Daegyoum Kim, daegyoum@kaist.ac.kr

Abstract

In aerodynamic and hydrodynamic devices and locomotive organisms, passive appendages have practical purposes such as drag reduction and flow control. Although these appendages also affect the dynamics of freely falling bodies, underlying principles of their functions remain elusive. We investigate experimentally the dynamics of a falling sphere with a filament appended on its rear side by varying the ratio of filament length to sphere diameter ($l/D=0{-}3.0$) and sphere-to-fluid density ratio ($\rho _s/\rho _f= 1.06{-}1.36$), and maintaining a similar dimensionless moment of inertia ($I^* \approx 0.96$). At the Reynolds number of $O(10^3)$, a sphere without any filament exhibits vertical descent. However, the falling of the sphere with a filament is accompanied by periodic horizontal displacements, and the degree of zigzag motion is maximised under specific filament length. The filament induces periodic rotation of the sphere by shifting the centre of mass of the entire model and through the hydrodynamic interaction of the filament with the surrounding fluid. The rotation of the sphere increases the drag force acting on the model, reducing tangential velocity along the trajectory by 14 % compared to a plain sphere. Furthermore, the sphere rotation enhances the lift force normal to the trajectory, extending trajectory length by 5 %. These combined effects improve falling time over a certain vertical distance by 20 % compared to the plain sphere. With increasing sphere density, the effects of the filament on the falling dynamics weaken, because the offset distance between the centre of mass of the model and the geometric centre of the sphere becomes smaller.

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, provided the original article is properly cited.
Copyright
© The Author(s), 2025. Published by Cambridge University Press
Figure 0

Figure 1. (a) Geometry of a sphere with a filament and internal configuration of the sphere. (b) Schematic of experimental set-up.

Figure 1

Figure 2. Trajectories of falling spheres with different filament lengths $l/D$: (a) 0 (plain sphere), (b) 1.0, and (c) 3.0. Here, $\rho _{s}/\rho _{f}= 1.06$ and $I^* = 0.967$, as for all figures and the table in §§ 3.1–3.3. The upper and lower panels are top and side views, respectively, and the $z$-axis aligns with the gravitational direction. See supplementary movie 1.

Figure 2

Figure 3. (a) Description of 2-D trajectory plane (blue) and length parameters to represent zigzag trajectory. The upper inset shows the top view of the trajectory. (b) Degree of zigzag motion $w^*$, with respect to $l/D$. The error bar represents the standard deviation from the mean for each measurement point.

Figure 3

Figure 4. (a) Falling time $t/t_0$, (b) trajectory length $L/L_0$, and (c) average tangential velocity $\bar {v}_t/\bar {v}_{t,0}$ with respect to $l/D$.

Figure 4

Figure 5. (a) Sign convention of angular velocity $\omega$ and definition of filament angle $\theta$. (b) Inner product of unit angular velocity vector $\boldsymbol {\omega }/|\boldsymbol {\omega }|$ and unit normal vector of the trajectory plane, $\boldsymbol {n}$, for $l/D = 1.0$.

Figure 5

Figure 6. Time histories of (a) filament angle $\theta$ and (b) sphere angular velocity $\omega /\overline {|\omega _0|}$ for $l/D = 1.0$. (c) The 3-D trajectory corresponding to (a) and (b). The insets (c) depict the orientation of the filament at each position represented by the red dots.

Figure 6

Figure 7. (a) Average magnitude of sphere angular velocity $\overline {|\omega |}/\overline {|\omega _0|}$. (b) Maximum magnitude of filament angle $|\theta |_{max}$ for different filament lengths.

Figure 7

Figure 8. (a) Schematic illustrating a wake region (grey) and the components of forces and torques acting on the model. The reference frame is fixed with the sphere. Time histories of sphere angular velocity $\omega$ (solid line) and lift force $F_L$ (dashed line) for (b) $l/D= 1.0$ and (c) $l/D = 2.0$.

Figure 8

Figure 9. (a) Sequential snapshots of wake visualisation for $l/D = 1.0$ with strong zigzag motion. (b) Corresponding simplified schematics illustrating the rotation process. For (a), see supplementary movie 2.

Figure 9

Figure 10. (a) Snapshots of wake visualisation for a long filament ($l/D = 2.0$). (b) Corresponding simplified schematics of the rotation process.

Figure 10

Figure 11. Simplified schematics of the rotation process for a short filament.

Figure 11

Figure 12. (a) Average drag coefficient $\bar {C}_D$ and (b) average lift coefficient $\bar {C}_L$ with respect to $l/D$.

Figure 12

Figure 13. Schematics of the models with (a) $l/D = 1.0$ and $\gamma /D = 0.2\, \%$, (b) $l/D = 1.0$ and $\gamma /D = 0$, and (c) $l/D = 0$ and $\gamma /D = 0.2\, \%$. The geometric centre of the sphere and the centre of mass of the entire model are denoted by $\bullet$ and $\otimes$, respectively.

Figure 13

Table 1. Degree of zigzag motion $w^*$, average magnitude of sphere angular velocity $\overline {|\omega |}$, maximum magnitude of filament angle $|\theta |_{max}$, average tangential velocity $\bar {v}_t$, trajectory length $L$, and falling time $t$ for two models with different configurations: (i) $l/D = 1.0$ and $\gamma /D = 0$; (ii) $l/D = 0$ and $\gamma /D = 0.2\,\%$. The models of (i) and (ii) correspond to those in figures 13(b) and 13(c), respectively. The subscript 1 denotes the result of the model with $l/D= 1.0$ and $\gamma /D = 0.2\,\%$ in figure 13(a).

Figure 14

Figure 14. (a) Degree of zigzag motion $w^*$, and (b) average magnitude of sphere angular velocity $\overline {|\omega |}/\overline {|\omega _0|}$, for $\rho _s/\rho _f = 1.06$ (black) and $\rho _s/\rho _f = 1.12$ (blue). Here, $I^* = 0.967$ for $\rho _s/\rho _f = 1.06$, and $I^* = 0.959$ for $\rho _s/\rho _f = 1.12$.

Figure 15

Figure 15. (a) Trajectory length $L/L_0$, (b) average tangential velocity $\bar {v}_t/\bar {v}_{t,0}$, and (c) falling time $t/t_0$, for $\rho _s/\rho _f = 1.06$ (black) and $\rho _s/\rho _f = 1.12$ (blue).

Figure 16

Figure 16. (a) Degree of zigzag motion $w^*$, (b) average magnitude of angular velocity $\overline {|\omega |}/\overline {|\omega _0|}$, (c) trajectory length $L/L_0$, (d) average tangential velocity $\bar {v}_t/\bar {v}_{t,0}$, and (e) falling time $t/t_0$, with respect to $\rho _s/\rho _f$ for the spheres with $l/D= 1.0$. Here, $I^* \approx 0.96$ for all cases.

Figure 17

Figure 17. Schematic of perspective projection geometry for an objective plane and an image sensor. The $\circledcirc$ symbol represents the focal point of the camera.

Figure 18

Figure 18. Measured angle difference $\Delta \alpha _{exp}$ between the initial and final orientations of the fixed but rotatable sphere versus predetermined angle difference $\Delta \alpha _{pre}$. The sphere rotates with respect to a vertical axis in the validation experiment.

Supplementary material: File

Choi et al. supplementary material movie 1

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Supplementary material: File

Choi et al. supplementary material movie 2

Movie 2 for figure 9(a)
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