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Drop impact on viscous liquid films

Published online by Cambridge University Press:  06 March 2023

Vatsal Sanjay*
Affiliation:
Physics of Fluids Group, Max Planck Center for Complex Fluid Dynamics, Department of Science and Technology, and J. M. Burgers Centre for Fluid Dynamics, University of Twente, P. O. Box 217, 7500 AE Enschede, The Netherlands
Srinath Lakshman*
Affiliation:
Physics of Fluids Group, Max Planck Center for Complex Fluid Dynamics, Department of Science and Technology, and J. M. Burgers Centre for Fluid Dynamics, University of Twente, P. O. Box 217, 7500 AE Enschede, The Netherlands
Pierre Chantelot*
Affiliation:
Physics of Fluids Group, Max Planck Center for Complex Fluid Dynamics, Department of Science and Technology, and J. M. Burgers Centre for Fluid Dynamics, University of Twente, P. O. Box 217, 7500 AE Enschede, The Netherlands
Jacco H. Snoeijer*
Affiliation:
Physics of Fluids Group, Max Planck Center for Complex Fluid Dynamics, Department of Science and Technology, and J. M. Burgers Centre for Fluid Dynamics, University of Twente, P. O. Box 217, 7500 AE Enschede, The Netherlands
Detlef Lohse*
Affiliation:
Physics of Fluids Group, Max Planck Center for Complex Fluid Dynamics, Department of Science and Technology, and J. M. Burgers Centre for Fluid Dynamics, University of Twente, P. O. Box 217, 7500 AE Enschede, The NetherlandsMax Planck Institute for Dynamics and Self-Organization, Am Fassberg 17, 37077 Göttingen, Germany

Abstract

When a liquid drop falls on a solid substrate, the air layer between them delays the occurrence of liquid–solid contact. For impacts on smooth substrates, the air film can even prevent wetting, allowing the drop to bounce off with dynamics identical to that observed for impacts on superamphiphobic materials. In this paper, we investigate similar bouncing phenomena, occurring on viscous liquid films, that mimic atomically smooth substrates, with the goal to probe their effective repellency. We elucidate the mechanisms associated with the bouncing to non-bouncing (floating) transition using experiments, simulations, and a minimal model that predicts the main characteristics of drop impact, the contact time and the coefficient of restitution. In the case of highly viscous or very thin films, the impact dynamics is not affected by the presence of the viscous film. Within this substrate-independent limit, bouncing is suppressed once the drop viscosity exceeds a critical value, as on superamphiphobic substrates. For thicker or less viscous films, both the drop and film properties influence the rebound dynamics and conspire to inhibit bouncing above a critical film thickness. This substrate-dependent regime also admits a limit, for low-viscosity drops, in which the film properties alone determine the limits of repellency.

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, provided the original article is properly cited.
Copyright
© The Author(s), 2023. Published by Cambridge University Press.
Figure 0

Figure 1.(a) Schematic (not to scale) of the experimental set-up. (b) Side-view visualization of the drop impact process as viewed using the high-speed camera. The inset also shows the axisymmetric domain used in the DNS, and defines the symbols used. The domain boundaries are chosen to be far enough not to influence the drop impact process. Furthermore, we ensure that the waves formed on the film are not reflected back from these boundaries. Consequently, for $\mathit {Oh}_{f} < 0.1$, $\mathcal {L}_{{max}} \gg 8R$. On the other hand, if $\mathit {Oh}_{f} > 0.1$ and waves on the film are damped, then we choose $\mathcal {L}_{{max}} = 8R$.

Figure 1

Table 1.Properties of the liquids used in the experiments, where $\rho$ and $\eta$ are the density and viscosity of the liquid, and $\gamma$ denotes the liquid–air surface tension coefficient. Throughout the paper, the subscripts $d$, $f$ and $s$ represent drop, film and surrounding, respectively. The silicone oil manufacturers are Shin Etsu (SE) and Wacker Chemie AG (AK).

Figure 2

Figure 2.Effect of the film thickness on the drop impact process: comparison of the experimental and DNS snapshots of the impact process on films with differing $h_f$ values (a) $0.01\ {\rm mm}$, (b) $0.35\ {\rm mm}$, and (c) $0.85\ {\rm mm}$. In each panel, the top row contains the experimental images with (green) interface outline from DNS, and the bottom row contains numerical snapshots showing the dimensionless rate of viscous dissipation per unit volume ($\tilde {\xi }_\eta = 2\,\mathit {Oh}\,(\tilde {\boldsymbol {\mathcal {D}}}:\tilde {\boldsymbol {\mathcal {D}}})$) on the left and the magnitude of the dimensionless velocity field ($\tilde {\boldsymbol {v}}$) on the right. We show $\tilde {\xi }_\eta$ on a $\log _{{10}}$ scale to identify regions of maximum dissipation (marked with black for $\tilde {\xi }_\eta \geqslant 10$). For all cases in this figure, $R = 1\ {\rm mm}$, $V = 0.3\ {\rm m}\ {\rm s}^{-1}$, $\eta _{d} = 4.6\ {\rm mPa}\ {\rm s}$ and $\eta _{f} = 96\ {\rm mPa}\ {\rm s}$, corresponding to $(\mathit {We}_{d}, \mathit {Oh}_{d}, \mathit {Oh}_{f}) = (4, 0.034, 0.67)$. Supplementary movies 1–3 are available at https://doi.org/10.1017/jfm.2023.13.

Figure 3

Figure 3.Effect of the film thickness on the rebound characteristics for $R = 1\ {\rm mm}$, $V = 0.3\ {\rm m}\ {\rm s}^{-1}$, $\eta _{d} = 4.6\ {\rm mPa}\ {\rm s}$ and $\eta _{f} = 96\ {\rm mPa}\ {\rm s}$, i.e. $(\mathit {We}_{d}, \mathit {Oh}_{d}, \mathit {Oh}_{f}) = (4, 0.034, 0.67)$: (a) contact time $t_{c}$, and (b) restitution coefficient $\varepsilon$, as a function of film thickness $h_{f}$. Circles and hexagrams represent experiments and DNS, respectively. In (a,b), the horizontal black dashed lines represent the substrate-independent limits of contact time and restitution coefficient, respectively, while the solid black lines show the results from the phenomenological model (see § 4) with parameters $c_{k} = 2$, $c_{d} = 5.6$ and $c_{f} = 0.46$. The vertical grey dashed line marks the transition from the bouncing to the non-bouncing (floating) regime. The inset of (b) illustrates the variation of the restitution coefficient normalized by its substrate-independent value $\varepsilon ^*$ as a function of the film thickness. Here, the horizontal grey line represents $\varepsilon = 0.9\varepsilon ^*$, marking the transition from substrate-independent to substrate-dependent bouncing at $h_f = h_{f, 1}$. (c) Schematic diagram of the phenomenological model that describes the drop impact process on a liquid film. The parameters $\rho _d R^{3}$, $\eta _{d}R$ and $\gamma$ are associated with the drop properties, and $\eta _{f} \varGamma ^{-3} R$ is associated with the film properties.

Figure 4

Figure 4.Influence of the film parameters on the impact characteristics: variation of the coefficient of restitution $\varepsilon$ as a function of (a) the film thickness $\varGamma$, and (b) the film mobility $\varGamma / \mathit {Oh}_{f}^{1/3}$. In (a,b), the circles and hexagrams correspond to the results from experiments and simulations, respectively. The coloured dashed lines in (a) and the solid black line in (b) illustrate the results from the phenomenological model (4.13) with parameters $c_{k} = 2$, $c_{d} = 5.6$ and $c_{f} = 0.46$. Black dashed lines in (a,b) mark the substrate-independent limit of the restitution coefficient $\varepsilon ^*$. For all cases in this figure, $\mathit {Oh}_{d} = 0.034$ and $\mathit {We}_{d} = 4$.

Figure 5

Figure 5.Influence of the drop parameters on the rebound elasticity: variation of (a) the coefficient of restitution $\varepsilon$, and (b) the coefficient of restitution normalized with its substrate-independent value $\varepsilon /\varepsilon ^*$, as a function of the normalized film thickness $\varGamma$. The circles and hexagrams correspond to the results from the experiments and simulations, respectively. In (a), the dashed lines denote the plateau values of the restitution coefficient $\varepsilon ^*(\mathit {Oh}_{d})$. In (a,b), the solid lines represent the results from the phenomenological model (4.13) with parameters $c_{k} = 2$, $c_{d} = 5.6$ and $c_{f} = 0.46$. For all cases in this figure, $\mathit {Oh}_{f} = 0.667$ and $\mathit {We}_{d} = 4$.

Figure 6

Figure 6.Critical film thickness marking the transition from (a) substrate-independent to substrate-dependent bouncing $\varGamma _1$, and (b) bouncing to non-bouncing (floating) $\varGamma _2$ as a function of $\mathit {Oh}_{f}$ at different $\mathit {Oh}_{d}$. Prefactors (c) $\alpha _{1}$ and $\beta _{1}$, and (d) $\alpha _{2}$ and $\beta _{2}$, as a function of $\mathit {Oh}_{d}$. The solid black line in (c) represents the model prediction for $\beta _1$, (5.1). The solid black lines in (d) represent the model predictions for $\beta _2$ using (4.5) and (4.6), and the black dashed lines show the two asymptotes, (4.7) and (4.8).

Figure 7

Figure 7.$\mathit {Oh}_{f}$ independent inhibition of bouncing. (a) Typical drop impact dynamics on low-viscosity films. The snapshots show the dimensionless rate of viscous dissipation per unit volume on the left and the magnitude of dimensionless velocity field on the right. (b) Energy budgets for the two representative cases shown in (a), normalized by the available energy at the instant of impact. Here, the subscripts $g$, $k$, $\gamma$ and $\eta$ denote gravitational potential, kinetic, surface and viscous dissipation energies, respectively. The superscripts $d$, $f$ and $a$ represent drop, film and air, respectively. The grey dashed line in each plot marks the instant when the normal reaction force between the drop and the film is minimum, and represents the last time instant when the drop could have bounced off the film. For all cases, $(\mathit {We}_{d}, \mathit {Oh}_{d}, \varGamma ) = (4, 0.034, 1)$.

Figure 8

Figure 8.Dimensionless film deflection $\tilde {\delta }_f = \delta _f/R$ measured from the initial film free surface (see the inset in a) as a function of (a) the film thickness $\varGamma$, and (b) the film mobility $\varGamma / \mathit {Oh}_{f}^{1/3}$ in the DNS. The solid black lines represent $\delta _f/R = \varGamma$ and $\delta _f/R = \varGamma /\mathit {Oh}_{f}^{1/3}$ in (a,b), respectively. For all cases in this figure, $\mathit {Oh}_{d} = 0.034$ and $\mathit {We}_{d} = 4$.

Figure 9

Figure 9.Regime map in terms of the drop Ohnesorge number $\mathit {Oh}_{d}$ and dimensionless film thickness $\varGamma$ for $\mathit {Oh}_{f} < 0.1$, showing the transitions between the different regimes identified in this work. Here, $\varGamma _1$ (green symbols) marks the transition from substrate-independent bouncing to substrate-dependent bouncing, whereas $\varGamma _2$ (red symbols) marks the transition from bouncing to non-bouncing (floating). The black dashed line represents the substrate-independent asymptote for the bouncing to non-bouncing (floating) transition (4.7), and the grey dashed line, depicting the inviscid drop asymptote for the bouncing to non-bouncing (floating) transition, is drawn as a guide to the eye.

Figure 10

Figure 10.Regime map in terms of the drop Ohnesorge number $\mathit {Oh}_{d}$ and film mobility $\varGamma /\mathit {Oh}_{f}^{1/3}$ for $\mathit {Oh}_{f} \geqslant 0.1$, showing the transitions between the different regimes identified in this work. Here, $\varGamma _1$ (green symbols) marks the transition from substrate-independent to substrate-dependent bouncing, whereas $\varGamma _2$ (orange symbols) marks the transition from bouncing to non-bouncing (floating). The background contour illustrates the theoretical values of the coefficient of restitution $\varepsilon$ (see (4.13)) normalized with its (a) substrate-independent limit $\varepsilon ^* = \varepsilon (\varGamma /\mathit {Oh}_{f}^{1/3} \to 0)$ (see (B2)), and (b) inviscid drop and substrate-independent limit $\varepsilon _0 = \varepsilon ^*(\mathit {Oh}_{d} \to 0)$. The black solid lines shows the predicted bouncing to non-bouncing (floating) transition using the phenomenological model (4.5)–(4.6), and the black dashed lines show the two asymptotes (4.7) and (4.8) of bouncing to non-bouncing (floating) regimes. Finally, in (a), the grey solid line shows the prediction for $\varGamma _1$.

Figure 11

Figure 11.Rupture of the air layer and subsequent coalescence of impacting drops with the liquid coating. Rupture can occur due to: (a) impact as $\mathit {We}_{d}$ increases; (b) downward jetting as $\mathit {Oh}_{d}$ decreases; and (c) film distortions due to surface waves as $\mathit {Oh}_{f}$ decreases. For (a,c), $\varGamma = 0.03$, and for (b), $\varGamma = 0.01$ (dry-substrate limit).

Figure 12

Figure 12.Substrate-independent bouncing: variation of (a) the contact time $t_c^*$ normalized with the inertio-capillary time scale $\tau _\gamma$, and (b) the coefficient of restitution $\varepsilon ^*$ with the drop Ohnesorge number $\mathit {Oh}_{d}$. The solid black lines represent (B1)–(B2). These predictions are consistent with those of Jha et al. (2020), and set the prefactors $c_{k}$ and $c_{d}$ to $2.0 \pm 0.1$ and $5.6 \pm 0.1$, respectively. Here, $\mathit {We}_{d} = 4$ and $\mathit {Bo} = 0.5$.

Figure 13

Figure 13.Influence of the impact Weber number on the rebound: variation of (a) the contact time $t_c$ normalized with the inertio-capillary time scale $\tau _\gamma$, (b) the restitution coefficient, and (c) the restitution coefficient normalized with its dry-substrate value as a function of the dimensionless film thickness $\varGamma$. Here, $(\mathit {Oh}_{d}, \mathit {Oh}_{f}) = (0.034, 0.67)$. In each panel, the solid black line represents the model prediction for $(c_k, c_d, c_f) = (2, 5.6, 0.46)$, and the vertical dashed grey line indicates $\varGamma _2$, above which drops do not bounce. In (a,b), black dashed lines show the $\mathit {We}_{d}$-dependent values in the dry-substrate limit at fixed $\mathit {Oh}_{d}$, i.e. $\varepsilon ^*(\mathit {Oh}_{d} = 0.034, \mathit {We}_{d})$. Finally, in (c), the horizontal dashed grey line denotes the $0.9\varepsilon ^*$ criterion used to determine the substrate-independent to substrate-dependent transition for bouncing drops.

Figure 14

Figure 14.Experimental side-view snapshots at the instant of impact, $t = 0$. Each snapshot shows the wall location denoted by a green horizontal line and the film free interface denoted by a red horizontal line. The film thickness is estimated from the vertical difference between the two lines, which results in dimensionless film thickness $\varGamma = h_{f}/R$ values (a) $0.05$, (b) $0.11$, (c) $0.23$, and (d) $0.48$.

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