Drops falling on substrates with varying wettability exhibit distinct morphologies. However, the relation between the impact force exerted by a water drop and the substrate wettability has not been thoroughly explored. In this paper, we investigate the effect of contact angle (ranging from 40° to 180°) on the impact force of water drops, along with the spreading diameter, rim height, and retracting velocity. Our attention is focused to the inertial regime with the Weber number ranging from 30 to 100, which enables us to rationalize the dynamic relations and to correlate the kinematics of the drop with the impact force through scaling analysis. We find that substrate wettability has insignificant effect on the first force peak, which arises mainly from the momentum change during the initial impact. However, it does influence the second force peak, which originates from the momentum change in the flow redirecting from the radial inward direction to the vertical direction, accompanied by a column-shape Worthington jet. The second peak force gradually diminishes as the contact angle decreases, until it becomes indistinguishable below 40°, while the time at which the second peak force emerges is delayed.

The phenomenon of drops impacting solid surface is extensively observed in rainfall,1,2 pesticide spraying,3,4 ink-jet painting,5 and spray cooling.6 The wettability of the substrate plays a significant role in the dynamics of drop impact on solid surfaces, leading to different outcomes such as deposition, rebounding, or splashing.7–13 Hydrophilic surfaces prompt spreading and result in larger maximum spreading diameters, which is desirable in spray coating and ink-printing applications. Conversely, superhydrophobic surfaces possess intrinsic features that enable drop repellency, inspiring their applications in anti-icing,14 self-cleaning,15 anti-corrosion,16 and reducing the spread of respiratory disease.17 The impact force governs drop deformation and can even result in substrate erosion or wetting transitions on superhydrophobic surfaces.18,19 To gain insights into the underlying physics, it is crucial to investigate the transient impact force of falling drops.

Early studies on the impact forces of falling drops primarily focused on hydrophilic surfaces.20–27 When a water drop impacts a hydrophilic surface, a distinctive peak with a rapidly increasing stage followed by a relatively slowly decreasing stage can be observed in the impact force curve.22,23 In the regime dominated by inertia with Re > 200 and We > 68, the peak force is approximately expressed as F ≈ 0.83ρlV02D02, which is independent of the Reynolds number Re = ρlV0D0/μl and the Weber number We = ρlV02D0/γ, where ρl, V0, and D0 are the mass density, the initial impact velocity, and the drop diameter, respectively; μl is the dynamic viscosity; and γ is the surface tension. In the case of Re < 200, however, viscosity plays a significant role in the impact process, and the normalized peak force F increases with decreasing Re.24,25 It has been demonstrated that, in the regime dominated by inertia, the normalized temporal evolution of the impact force exhibits self-similarity and collapses into a master curve.24–26 Furthermore, the initial evolution of the impact force before the peak force follows a square-root scaling law,25 and the later evolution of the impact force after the peak force follows an exponential decay.26 

In the recent years, there has been growing interest among researchers in studying the impact force of drops falling on superhydrophobic surfaces.28–31 Zhang et al.28 conducted comprehensive experimental, numerical, and theoretical investigations on the impact force of water drops falling on a superhydrophobic surface with 1 < We < 400 and 800 < Re < 105. They revealed the presence of two prominent peaks in the temporal evolution of the impact force. The first peak force is attributed to the momentum change during the initial impact, while the second arises from the momentum change resulting from the converging flow during rebound, accompanied by a Worthington jet. By analyzing the characteristics of the peak forces and the morphology of the impacting drops, they identified four distinct regimes in terms of We: capillary, singular jet, inertial, and splashing. In the inertial regime, the value of the second peak can be estimated using the recoiling velocity, jet velocity and spreading diameter at the instant of the second peak. Interestingly, they found that while there is no significant difference in the first peaks observed when drops fall on hydrophilic surfaces (with an equivalent contact angle θ = 40° ± 4°) and superhydrophobic surfaces (θ = 165° ± 1°), the second peak only occurs on superhydrophobic surfaces and is nearly absent on hydrophilic surfaces.

Though these previous studies have primarily examined the impact forces of drops falling on hydrophilic and superhydrophobic surfaces, the influence of surface wettability on the impact forces (especially the second peak) has been rarely explored. In this study, we aim to fill this gap and investigate the impact force in relation to surface wettability. We will first describe the experimental and numerical methods. Then, the evolution of the impact force on surfaces with different levels of wettability, along with the corresponding geometric relations, will be illustrated. We perform scaling analysis to rationalize these relations in the inertial regime (30 < We < 100). Finally, we will summarize our main findings.

Figure 1(a) illustrates the schematics of the experimental setup. A water drop with a diameter of D0 impacts a substrate at an initial velocity of V0. The normal impact force is measured by a highly sensitive piezoelectric transducer, while the deformation of the drop shape is simultaneously recorded by a high-speed camera in a side-view. The camera is triggered to record the drop morphology when the impact force exceeds 1 mN. For the present experiments, de-ionized water is used, which has the mass density ρl = 1000 kg/m3, surface tension γ = 0.073 N/m, and dynamic viscosity μl = 1.0 mN m. The drop diameter is D0 = 2.05 mm, and the falling height is adjusted to vary the impact velocity. A hydrophilic surface (advancing and receding contact angles are 47° ± 2° and 13° ± 2°, respectively) and a superhydrophobic surface (advancing and receding contact angles are 167° ± 2° and 154° ± 2°, respectively) are compared in the experiment. More details of the experimental method can be found in the supplementary material and the work of Zhang et al.28 

FIG. 1.

(a) Schematics of the experimental setup. (b) Simulation domain with boundary conditions.

FIG. 1.

(a) Schematics of the experimental setup. (b) Simulation domain with boundary conditions.

Close modal

Figure 1(b) illustrates the domain of the simulation, which is axisymmetric with respect to the z axis. The top and outer parts of the domain are set as pressure outlet boundaries, with zero pressure. At the bottom of the domain, a no-slip boundary condition is applied. The drop is initially generated as a sphere with a diameter of 2.05 mm, positioned at 0.1 mm above the substrate. To achieve different Weber numbers, the initial velocity is varied. In the simulations, the physical properties of water are the same as those in the experiments. The mass density and dynamic viscosity of air are set as ρa = 1.20 kg/m3 and μa = 0.0181 mN m, respectively. Gravitational acceleration is included with a value of 9.81 m/s2. Contact angle hysteresis is not considered, and a user-specified contact angle θ is set for each simulation. In other words, the advancing and receding contact angles in each simulation are set to be identical. The first peak of the impact force is independent of the contact angle. The second peak is a result of the redirection of liquid flow during the retraction phase of the drop, and therefore, it is influenced by the receding contact angle rather than the advancing contact angle. To compare the numerical and experimental results depicted in Fig. 2 and verify the accuracy of our simulations, the experimental values of the receding contact angles are assigned to simulate the entire impinging process [i.e., θ = 13° for Figs. 2(a) and 2(c) and θ = 154° for Figs. 2(b) and 2(d)]. It is important to emphasize that in all of our simulations, the assigned contact angle θ corresponds to the receding contact angle expected in real experiments. The simulations are conducted using the OpenFOAM computational fluid dynamics (CFD) software, and further details are given in the supplementary material.

FIG. 2.

Temporal evolutions of impact force with representative drop shapes for both experimental and numerical results. (a) Transient force profile of a drop falling on a hydrophilic surface at We = 50, with experimental values of advancing and receding contact angles being 47° ± 2° and 13° ± 2°, respectively. (b) Transient force profile of a drop falling on a superhydrophobic surface at We = 50, with experimental values of advancing and receding contact angles of 167° ± 2° and 154° ± 2°, respectively. (c) Representative drop shapes corresponding to Fig. 2(a), displaying experimental images in the top row and numerical snapshots in the bottom row. (d) Representative drop shapes corresponding to Fig. 2(b), featuring experimental images in the top row and numerical snapshots in the bottom row.

FIG. 2.

Temporal evolutions of impact force with representative drop shapes for both experimental and numerical results. (a) Transient force profile of a drop falling on a hydrophilic surface at We = 50, with experimental values of advancing and receding contact angles being 47° ± 2° and 13° ± 2°, respectively. (b) Transient force profile of a drop falling on a superhydrophobic surface at We = 50, with experimental values of advancing and receding contact angles of 167° ± 2° and 154° ± 2°, respectively. (c) Representative drop shapes corresponding to Fig. 2(a), displaying experimental images in the top row and numerical snapshots in the bottom row. (d) Representative drop shapes corresponding to Fig. 2(b), featuring experimental images in the top row and numerical snapshots in the bottom row.

Close modal

In this section, we first revisit the temporal evolutions of the impact force and shape deformation of drops colliding on hydrophilic and superhydrophobic surfaces to comprehensively understand the impact dynamics. Subsequently, we examine the influence of surface wettability on the two peak forces and their corresponding instants. In addition, we elucidate the mechanisms behind the transient force and drop morphologies with varying contact angles. In this study, our primary focus is to examine the influence of surface wettability on impact forces. Therefore, we specifically investigate drop impacts in the inertial regime (30 < We < 100). Within this regime, the Ohnesorge number ( O h = μ l / ρ l D 0 γ) remains constant at 0.0026. Moreover, by estimating the Froude number ( F r = V 0 / g D 0) for a drop with a diameter of D0 = 2.05 mm and an impact velocity of V0 = 1 m/s, we find Fr = 69. These estimations suggest that the influence of viscous and gravitational forces can be neglected. Here, g represents the acceleration of gravity. Moreover, the influence of contact line pinning is not considered in the simulations.

Figure 2(a) presents both the experimental and numerical results of the temporal evolution of the impact force for a drop with We = 50 (D0 = 2.05 mm and V0 = 1.33 m/s) on the hydrophilic surfaces. For this case, Fig. 2(c) illustrates the representative snapshots of the drop shape, with the top row depicting the experimental images and the bottom row displaying the numerical simulations. In each snapshot of the numerical results, the left part gives the pressure field and the right part displays the velocity field. The white velocity vectors with the snapshots indicate the internal flow, with the vector size indicating the magnitude of velocity. During the initial impact, the transient force rapidly increases and reaches the first peak F1 = 6.16 mN at t1 = 0.40 ms when the spreading diameter approaches the drop diameter D0 (as seen in the snapshot at t = 0.40 ms). Subsequently, the impact force gradually decreases as the spreading diameter continues to increase. Throughout the initial impact and the subsequent spreading regime, the velocity vectors shift from the vertical direction to the horizontal. As the spreading diameter reaches its maximum, the impact force approximates 0 mN. Finally, the drop recedes and undergoes oscillation until it settles as a deposited drop on the surface. The receding and oscillation are relatively gentle, and the impact force remains near 0 mN. A notable characteristic observed during drop impact on hydrophilic surfaces is the presence of only one peak force in the force profile.22–26 

Rich impact dynamic phenomena are observed when a drop collides with a superhydrophobic surface.28  Figure 2(b) illustrates the experimental and numerical impact forces of a drop falling on superhydrophobic surfaces at We = 50 (D0 = 2.05 mm and V0 = 1.33 m/s), accompanied by representative drop shapes shown in Fig. 2(d). During the initial impact and subsequent spreading, the temporal evolution of the impact force and drop shape on the superhydrophobic surface is similar to that on the hydrophilic surface. The first peak (F1 = 6.19 mN at t1 = 0.40 ms) of the drop on the superhydrophobic surface also undergoes a sudden increase followed by a decrease. Simultaneously, the liquid flux switches from the vertical direction to the horizontal as the spreading diameter approaches its maximum, Dm. At the moment of maximum diameter, tm, the drop becomes a thin liquid film in the center and thick rims along the edges, as depicted in the numerical snapshot at t = 2.3 ms. Subsequently, the drop retracts due to the capillary force. During the early stage of retraction, the drop maintains the configuration of a thin film bounded by a thick rim, with the impact force remaining close to 0 mN. As the receding mass converges toward the center, the velocity vector shifts from the horizontal direction to the vertical (as observed in the snapshot at t = 4.9 ms), leading to the second peak force F2 = 2.76 mN at t2 = 4.85 ms, accompanied by an upward Worthington jet. As the drop rebounds on the substrate, the impact force gradually decreases to 0 mN, and ultimately the drop detaches from the surface. Figure 2 demonstrates that for both the impact processes on hydrophilic and superhydrophobic surfaces, the simulations accurately predict the characteristics of force evolution and drop deformation. Thus, it is reasonable to believe that our numerical simulations can also accurately predict the impact dynamics of drops falling on surfaces with other wettabilities.

Figure 3(a) compares the transient force profiles of drops falling on surfaces with different contact angles ranging from 13° to 180° at We = 50 (D0 = 2.05 mm and V0 = 1.33 m/s). It is illustrated that all force profiles exhibit a consistent master curve for the first peak, including the increasing and the decreasing stages, in agreement with previous research.28 The overlapping profiles indicate that the first peak is insensitive to the surface wettability. The notable characteristic of these force profiles is the second peak, which diminishes with decreasing contact angle. At θ = 13°, no second peak is discernible. In the sequel, hence, our focus is on the contact angles ranging from 40° to 180°. Additionally, t2 increases with decreasing contact angle. These characteristics of the second peak force arise from the effect of surface wettability. During retraction, different wettabilities affect the force balance in the radial direction, resulting in varying retracting velocities of the surrounding rim and subsequent changes in momentum rate (i.e., transient impact force) when the flow converges at the drop center. As depicted in Fig. 3(b), higher contact angles correspond to a higher retraction velocity and increased pressure at the drop center at t2. Further details regarding the influence of surface wettability on the experimental force profiles can be found in the supplementary material.

FIG. 3.

Impact of surface wettability on (a) temporal evolution of impact force and (b) drop shape at t2, for drops at We = 50 (D0 = 2.05 mm, V0 = 1.33 m/s).

FIG. 3.

Impact of surface wettability on (a) temporal evolution of impact force and (b) drop shape at t2, for drops at We = 50 (D0 = 2.05 mm, V0 = 1.33 m/s).

Close modal

Figure 4(a) presents the instants of the first peak, t1, normalized by the inertial-capillary timescale τγ = (ρlD03/γ)1/2, as a function of the Weber number for different contact angles. It is illustrated that the normalized instant of the first peak is unaffected by wettability but influenced by the Weber number, i.e., t1/τγWe−1/2 (red solid line). This scaling law can be understood by considering that the drop undergoes momentum changes over the vertical length D0 at velocity V0, implying t1D0/V0. Moreover, Fig. 4(b) illustrates the first peak force F1, normalized by ρlV02D02, as a function of θ for different Weber numbers. It is observed that the normalized peak force remains unaffected by surface wettability and We, i.e., F1/(ρlV02D02) ≈ 0.81 (black solid line). At t1, the spreading diameter approximates D0 without considering the spreading lamella. Thus, the peak force can be estimated by the dynamic pressure ρlV02 over the contact area D02, i.e., F1ρlV02D02 (Refs. 23, 28, and 30).

FIG. 4.

(a) Relation between t1 and We in the dimensionless form on surfaces with varying wettabilities. The red solid line represents the scaling relation t1/τγ ≈ 0.24We−1/2. (b) Relation between F1 and θ at different We. The black solid line indicates the best straight-line fit to the numerical data, F1 ≈ 0.81ρlV02D02.

FIG. 4.

(a) Relation between t1 and We in the dimensionless form on surfaces with varying wettabilities. The red solid line represents the scaling relation t1/τγ ≈ 0.24We−1/2. (b) Relation between F1 and θ at different We. The black solid line indicates the best straight-line fit to the numerical data, F1 ≈ 0.81ρlV02D02.

Close modal

For drops on surfaces with varying wettabilities, the second peak forces arise from the momentum changes occurring when the horizontally converging liquid redirects vertically. This momentum change is closely related to the kinematics of the impacting drops. To further understand the physical mechanisms behind the second peak force, we will initially examine the kinematics of retracting drops at t2. Figure 5(a) illustrates the drop morphology on the surface with θ = 80° at t2, characterized by the spread diameter D2, drop height h2 (see the supplementary material for the measurement of h2), horizontal receding velocity Ut2, jet diameter Dj, and jet velocity Uj. Importantly, it is noted that these physical quantities are specific to the instance of t2, which distinguishes our work from previous investigations that examined the average values or characteristic values in the entire retracting stage.11,32–35

FIG. 5.

(a) Drop morphology at t2 for We = 50 and θ = 80° illustrating the drop spreading diameter D2, drop height h2, jet diameter Dj, retracting velocity Ut2, and jet velocity Uj. (b) Sketch of retracting liquid film. Parameters w, h, and s denote width, height, and move distance of the liquid film, respectively. Parameters γ, γSL, and γSA denote the surface tension of liquid–air, solid–liquid, and solid–air, respectively. Ut denotes the retracting velocity and θ denotes the contact angle. (c) The normalized retracting velocity U ̃t2 as a function of (1 − cos  θ) for drops at different We. The red solid line represents U ̃t2 ≈ 1.3(1 − cos  θ)1/2. (d) The normalized t ̃2 and t ̃m as functions of (1 − cos  θ) for drops at different We. The red solid and blue dashed lines represent t ̃2 ≈ 0.66(1 − cos  θ)−1/2 and t ̃m ≈ 0.27(1 − cos  θ)−1/2, respectively. (e) Effect of surface wettability on the velocity of the Worthington jet Uj for drops at different We. The red solid line corresponds to U ¯j = 2.07(1 − cos  θ)1/2, provided as a visual aid.

FIG. 5.

(a) Drop morphology at t2 for We = 50 and θ = 80° illustrating the drop spreading diameter D2, drop height h2, jet diameter Dj, retracting velocity Ut2, and jet velocity Uj. (b) Sketch of retracting liquid film. Parameters w, h, and s denote width, height, and move distance of the liquid film, respectively. Parameters γ, γSL, and γSA denote the surface tension of liquid–air, solid–liquid, and solid–air, respectively. Ut denotes the retracting velocity and θ denotes the contact angle. (c) The normalized retracting velocity U ̃t2 as a function of (1 − cos  θ) for drops at different We. The red solid line represents U ̃t2 ≈ 1.3(1 − cos  θ)1/2. (d) The normalized t ̃2 and t ̃m as functions of (1 − cos  θ) for drops at different We. The red solid and blue dashed lines represent t ̃2 ≈ 0.66(1 − cos  θ)−1/2 and t ̃m ≈ 0.27(1 − cos  θ)−1/2, respectively. (e) Effect of surface wettability on the velocity of the Worthington jet Uj for drops at different We. The red solid line corresponds to U ¯j = 2.07(1 − cos  θ)1/2, provided as a visual aid.

Close modal
As depicted in Fig. 5(b) from a two-dimensional point of view, the recoiling of the liquid film is driven by the competition between the capillary force and the inertia of the recoiling liquid film. Based on the momentum conservation, the force balance of the drop film can be expressed as
d d t ( m d s d t ) = F c ,
(3.1)
where m, s, and Fc represent the mass of the liquid film, the distance the liquid film moves, and the capillary force acting on it, respectively. The mass is estimated as mρlshw, where h and w denote the height and width of the liquid film, respectively. The capillary force is expressed as Fcw(γ + γSLγSA), with γ, γSL, and γSA representing the liquid–air, solid–liquid, and solid–air interfacial tensions, respectively. Using the Young–Laplace equation, cos  θ = (γSAγSL)/γ, we can further obtain Fc(1 − cos  θ). By considering the initial condition, i.e., t = 0, s = 0, and ds/dt = 0, the retracting velocity Ut = ds/dt is solved from Eq. (3.1) as
U t = γ ρ l h ( 1 cos θ ) .
(3.2)
When θ = 180°, Eq. (3.2) degenerates into the classical Taylor–Culick velocity,36,37 U t = 2 γ / ( ρ l h ). In Fig. 5(c), the dots represent the relation between U ̃ t 2 U t 2 / γ / ( ρ l h 2 ) and (1 − cos  θ), with Ut2, h2, and θ being the experimental values. The red solid line represents U t / γ / ( ρ l h ) = 1 cos θ, indicating a fine agreement between Eq. (3.2) and the numerical data.
The time interval from the initial impact to t2 is divided into two regimes, t2 = tm + (t2tm), where tm denotes the moment when the spreading diameter reaches the maximum Dm, and (t2tm) is the retracting time. In Fig. 5(d), the normalized time instant tm/τγ decreases with increasing contact angle, following the relation tm/τγ ∼ (1 − cos  θ)−1/2, which is plotted as a blue dashed line. On the other hand, the time duration (t2tm) can be calculated as (t2tm) ≈ (DmD2)/Ut2, where (DmD2) scales with D2 and (DmD2)/D2 ≈ 0.76, as illustrated in Fig. S4 in the supplementary material. Considering the volume conservation relation D2 ∼ (D03/h2)1/2, we finally obtain (t2tm) ∼ D2/Ut2τγ (1 − cos  θ)−1/2 by taking Eq. (3.2) into consideration. The above analysis clearly suggests t2τγ (1 − cos  θ)−1/2, which is rewritten into the following dimensionless form
t ̃ 2 = t 2 τ γ ( 1 cos θ ) 1 / 2 ,
(3.3)
as indicated by the red solid line in Fig. 5(d), which fits the numerical data very well. Moreover, it is seen from Fig. 5(e) that the normalized jet velocity U ¯ j = U j / V 0 increases as the contact angle increases. The red solid line corresponding to (1 − cos  θ)1/2 is used to guide the eye.
In the retracting regime, the liquid flow converges at the center of the drop and redirects from the horizontal direction to the vertical. Considering that the total contact time (including the spreading and retraction times) τγ is dominated by the retraction time (∼80% of τγ),35,38–40 we estimate the characteristic acceleration of the drop in the vertical direction during retraction as g* = D0/τγ2 = γ/(ρlD02). Consequently, we can express the nominal capillary length as l c * = γ / ( ρ l g * ) = D 0. For the retracting drop at the moment t2 under g*, we can determine its thickness as h2 = 2 lc*sin(θ/2),41 which can be rewritten as
h ¯ 2 = h 2 D 0 ( 1 cos θ ) 1 / 2 .
(3.4)
As shown in Fig. 6(a), Eq. (3.4) is plotted as a red solid line that fits the numerical data well. By considering the volume conservation D22h2D03, we obtain
D ¯ 2 = D 2 D 0 ( 1 cos θ ) 1 / 4 ,
(3.5)
as depicted by a red solid in Fig. 6(b), which also fits the numerical data very well. However, it is crucial to emphasize that the excellent agreement observed is primarily attributed to the inertial regime (30 < We < 100) we have analyzed. The understanding of the morphology evolution of impinging drops on surfaces with certain wettability have been provided in previous research works.11,34 However, in the present work, we aim to comprehensively investigate the effect of surface wettability on drop dynamics at a specific moment t2, as clarified above. Notably, the second peaks observed in our study arise from the receding of liquid rims. In this context, we assume that the contact angle θ used in the above simulations and scaling relations should correspond to the receding contact angle θr in practical cases.
FIG. 6.

(a) Influence of surface wettability on the drop height h2 for drops at different We. The red solid line represents h ¯2 ≈ 0.30 (1 − cos  θ)1/2. (b) The normalized diameter D ¯2 as a function of (1 − cos  θ) for drops at different We. The red solid line represents D ¯2 ≈ 1.70 (1 − cos  θ)−1/4.

FIG. 6.

(a) Influence of surface wettability on the drop height h2 for drops at different We. The red solid line represents h ¯2 ≈ 0.30 (1 − cos  θ)1/2. (b) The normalized diameter D ¯2 as a function of (1 − cos  θ) for drops at different We. The red solid line represents D ¯2 ≈ 1.70 (1 − cos  θ)−1/4.

Close modal
Based on the understanding of the kinematics of the retracting drop, we now establish a correlation between the kinematics of the drop and the second peak force. We employ the theoretical model proposed by Zhang et al.28 to analyze the second peak force of drop impingement on superhydrophobic surfaces. Specifically, as depicted in Fig. 3(b), the velocity vectors far from the drop center are parallel to the substrates, indicating that the momentum changes (i.e., the transient forces) primarily arise from the redirected flow in the opposite direction of the upward Worthington jet. Therefore, we employ the rate of momentum change in the Worthington jet to estimate the second peak force, i.e., F2ρlUj2Dj2. The conservation of volume flux for the horizontal converging flow and the upward Worthington jet results in UjDj2Ut2D2h2. Using the volume conservation condition D22h2D03, we can write the second peak force as F2ρlUjUt2D03/D2. It is normalized by the inertial pressure force ρlV02D02 as
F ¯ 2 = F 2 ρ l V 0 2 D 0 2 U ¯ j U ¯ t 2 D ¯ 2 ,
(3.6)
where U ¯ t 2 = U t 2 / V 0 represents the normalized retracting velocity and D ¯ 2 = D 2 / D 0 represents the normalized spreading diameter. Moreover, as shown in Fig. 7, Eq. (3.6) well predicts the numerical second peak force for a larger range of contact angles (40° < θ < 180°) in the inertial regime (30 < We < 100).
FIG. 7.

Comparation between the second peak force F ¯ 2 and its theoretical prediction F ¯ 2 theory in dimensionless form. The markers of different shapes represent varying contact angles, while the color bar characterizes the Weber number ranging from 30 to 100. The red solid line represents U ¯ j U ¯ t 2 / D ¯ 2 1.8 F 2 / ( ρ l V 0 2 D 0 2 ).

FIG. 7.

Comparation between the second peak force F ¯ 2 and its theoretical prediction F ¯ 2 theory in dimensionless form. The markers of different shapes represent varying contact angles, while the color bar characterizes the Weber number ranging from 30 to 100. The red solid line represents U ¯ j U ¯ t 2 / D ¯ 2 1.8 F 2 / ( ρ l V 0 2 D 0 2 ).

Close modal

In summary, we have combined numerical simulations and scaling arguments to investigate the influence of wettability on the impact force of a falling drop on flat surfaces under various Weber numbers and contact angles. It is revealed that the momentum changes during the initial impact leads to the first peak force F1ρlV02D02, and the normalized instant of the first peak follows t1/τγWe−1/2, which are insensitive to surface wettability. During the retracting regime, the normalized second peak force can be expressed as F 2 / ( ρ l V 0 2 D 0 2 ) U ¯ j U ¯ t 2 / D ¯ 2, reminiscent of the momentum change in the converging flow from the horizontal direction to the vertical on superhydrophobic surfaces during drop impingement.28 Here, we extend this discovery to a wider range of contact angles (40° < θ < 180°) for inertial impact (30 < We < 100). Furthermore, at the instant of the second peak force t2, simpler scaling relations closely linked to the surface wettability are established, including t2/τγ ∼ (1 − cos  θ)−1/2, h2/D0 ∼ (1 − cos  θ)1/2, D2/D0 ∼ (1 − cos  θ)−1/4, and U t 2 / γ / ( ρ l h 2 ) ( 1 cos θ ) 1 / 2. Notably, these relations remain independent of the Weber number. These findings distinguish our work from previous investigations that primarily focused on the impact force of drop impingement on hydrophilic or superhydrophobic surfaces or the morphological evolution of impinging drops.

It is emphasized that our investigations primarily focus on the inertial regime (30 < We < 100) and rely on scaling arguments to understand the main mechanisms. As a result, other factors such as viscous effect, contact line pinning, gravitational force and the complex inner fluid field within the drop have been ignored in this study, which could account for the deviations observed in some experimental data. To achieve a comprehensive understanding, future research should encompass a more extensive survey considering these impact factors. Furthermore, we have observed that as the contact angle decreases, the magnitude of the second peak force diminishes until it reaches zero. It is plausible that viscosity and gravitational force play important roles.10 Exploring the threshold of the second peak force in relation to surface wettability and its connection to rebounding is also an interesting topic for future effort. Finally, while Eq. (3.6) effectively characterize the second peak force, our ultimate objective is to express the second peak force as an explicit function of We and θ. This would provide a deeper understanding of the drop impact force, along with the underlying physics.

See the supplementary material for details of the experimental setup, numerical method, mesh size independence, experimental impact force on surfaces with different wettabilities, relationship between Dm and D2, and measurement of the height h2 (PDF).

This study was supported by the National Natural Science Foundation of China (Grant Nos. 11902179, 12172189, 52111540269, and 11921002) and the Tsinghua University Initiative Scientific Research Program (Grant No. 20221080070).

The authors have no conflicts to disclose.

Bin Zhang and Chen Ma contributed equally to this work.

Bin Zhang: Data curation (equal); Formal analysis (equal); Investigation (equal); Software (equal); Validation (equal); Visualization (equal); Writing – original draft (equal). Chen Ma: Data curation (equal); Formal analysis (equal); Investigation (equal); Software (equal); Validation (equal); Visualization (equal); Writing – original draft (equal). Huanlei Zhao: Data curation (equal); Visualization (equal); Writing – review & editing (equal). Yinggang Zhao: Data curation (equal); Validation (equal); Writing – review & editing (equal). Pengfei Hao: Resources (equal); Validation (equal); Writing – review & editing (equal). Xi-Qiao Feng: Funding acquisition (equal); Resources (equal); Supervision (equal); Writing – review & editing (equal). Cunjing Lv: Conceptualization (equal); Formal analysis (equal); Funding acquisition (equal); Project administration (lead); Resources (equal); Supervision (equal); Writing – review & editing (equal).

The data that support the findings of this study are available within the article and its supplementary material.

1.
P. I. A.
Kinnell
, “
Raindrop-impact-induced erosion processes and prediction: A review
,”
Hydrol. Process.
19
,
2815
2844
(
2005
).
2.
Y.
Bhosale
,
E.
Esmaili
,
K.
Bhar
, and
S.
Jung
, “
Bending, twisting and flapping leaf upon raindrop impact
,”
Bioinspir. Biomim.
15
,
036007
(
2020
).
3.
V.
Bergeron
,
D.
Bonn
,
J. Y.
Martin
, and
L.
Vovelle
, “
Controlling droplet deposition with polymer additives
,”
Nature
405
,
772
775
(
2000
).
4.
M.
Song
,
J.
Ju
,
S.
Luo
,
Y.
Han
,
Z.
Dong
,
Y.
Wang
,
Z.
Gu
,
L.
Zhang
,
R.
Hao
, and
L.
Jiang
, “
Controlling liquid splash on superhydrophobic surfaces by a vesicle surfactant
,”
Sci. Adv.
3
,
e1602188
(
2017
).
5.
D.
Lohse
, “
Fundamental fluid dynamics challenges in inkjet printing
,”
Annu. Rev. Fluid Mech.
54
,
349
382
(
2022
).
6.
J.
Breitenbach
,
I. V.
Roisman
, and
C.
Tropea
, “
From drop impact physics to spray cooling models: A critical review
,”
Exp. Fluids
59
,
55
(
2018
).
7.
R.
Rioboo
,
M.
Marengo
, and
C.
Tropea
, “
Outcomes from a drop impact on solid surfaces
,”
At. Sprays
11
,
155
166
(
2001
).
8.
A. L.
Yarin
, “
Drop impact dynamics: Splashing, spreading, receding, bouncing
,”
Annu. Rev. Fluid Mech.
38
,
159
192
(
2006
).
9.
C.
Josserand
and
S. T.
Thoroddsen
, “
Drop impact on a solid surface
,”
Annu. Rev. Fluid Mech.
48
,
365
391
(
2016
).
10.
V.
Sanjay
,
P.
Chantelot
, and
D.
Lohse
, “
When does an impacting drop stop bouncing?
,”
J. Fluid Mech.
958
,
A26
(
2023
).
11.
S.
Wildeman
,
C. W.
Visser
,
C.
Sun
, and
D.
Lohse
, “
On the spreading of impacting drops
,”
J. Fluid Mech.
805
,
636
655
(
2016
).
12.
W.
Fang
,
K.
Zhang
,
Q.
Jiang
,
C.
Lv
,
C.
Sun
,
Q.
Li
,
Y.
Song
, and
X.-Q.
Feng
, “
Drop impact dynamics on solid surfaces
,”
Appl. Phys. Lett.
121
,
210501
(
2022
).
13.
H.
Li
,
W.
Fang
,
Y.
Li
,
Q.
Yang
,
M.
Li
,
Q.
Li
,
X.-Q.
Feng
, and
Y.
Song
, “
Spontaneous droplets gyrating via asymmetric self-splitting on heterogeneous surfaces
,”
Nat. Commun.
10
,
950
(
2019
).
14.
L.
Wang
,
Z.
Tian
,
G.
Jiang
,
X.
Luo
,
C.
Chen
,
X.
Hu
,
H.
Zhang
, and
M.
Zhong
, “
Spontaneous dewetting transitions of droplets during icing & melting cycle
,”
Nat. Commun.
13
,
378
(
2022
).
15.
S.
Nishimoto
and
B.
Bhushan
, “
Bioinspired self-cleaning surfaces with superhydrophobicity, superoleophobicity, and superhydrophilicity
,”
RSC Adv.
3
,
671
690
(
2013
).
16.
E.
Vazirinasab
,
R.
Jafari
, and
G.
Momen
, “
Application of superhydrophobic coatings as a corrosion barrier: A review
,”
Surf. Coat. Technol.
341
,
40
56
(
2018
).
17.
H.
Zhong
,
Z.
Zhu
,
J.
Lin
,
C. F.
Cheung
,
V. L.
Lu
,
F.
Yan
,
C.-Y.
Chan
, and
G.
Li
, “
Reusable and recyclable graphene masks with outstanding superhydrophobic and photothermal performances
,”
ACS Nano
14
,
6213
6221
(
2020
).
18.
D.
Bartolo
,
F.
Bouamrirene
,
E.
Verneuil
,
A.
Buguin
,
P.
Silberzan
, and
S.
Moulinet
, “
Bouncing or sticky droplets: Impalement transitions on superhydrophobic micropatterned surfaces
,”
Europhys. Lett.
74
,
299
305
(
2006
).
19.
B.
Amirzadeh
,
A.
Louhghalam
,
M.
Raessi
, and
M.
Tootkaboni
, “
A computational framework for the analysis of rain-induced erosion in wind turbine blades, part I: Stochastic rain texture model and drop impact simulations
,”
J. Wind. Eng. Ind. Aerodyn.
163
,
33
43
(
2017
).
20.
M. A.
Nearing
,
J. M.
Bradford
, and
R. D.
Holtz
, “
Measurement of force vs. time relations for waterdrop impact
,”
Soil Sci. Soc. Amer. J.
50
,
1532
1536
(
1986
).
21.
A.
Sahaya Grinspan
and
R.
Gnanamoorthy
, “
Impact force of low velocity liquid droplets measured using piezoelectric PVDF film
,”
Colloids Surf., A
356
,
162
168
(
2010
).
22.
J.
Li
,
B.
Zhang
,
P.
Guo
, and
Q.
Lv
, “
Impact force of a low speed water droplet colliding on a solid surface
,”
J. Appl. Phys.
116
,
214903
(
2014
).
23.
D.
Soto
,
A. B.
De Larivière
,
X.
Boutillon
,
C.
Clanet
, and
D.
Quéré
, “
The force of impacting rain
,”
Soft Matter
10
,
4929
4934
(
2014
).
24.
B.
Zhang
,
J.
Li
,
P.
Guo
, and
Q.
Lv
, “
Experimental studies on the effect of Reynolds and Weber numbers on the impact forces of low-speed droplets colliding with a solid surface
,”
Exp. Fluids
58
,
125
(
2017
).
25.
L.
Gordillo
,
T. P.
Sun
, and
X.
Cheng
, “
Dynamics of drop impact on solid surfaces: Evolution of impact force and self-similar spreading
,”
J. Fluid Mech.
840
,
190
214
(
2018
).
26.
B. R.
Mitchell
,
J. C.
Klewicki
,
Y. P.
Korkolis
, and
B. L.
Kinsey
, “
The transient force profile of low-speed droplet impact measurements and model
,”
J. Fluid Mech.
867
,
300
322
(
2019
).
27.
R.
Zhang
,
B.
Zhang
,
Q.
Lv
,
J.
Li
, and
P.
Guo
, “
Effects of droplet shape on impact force of low-speed droplets colliding with solid surface
,”
Exp. Fluids
60
,
64
(
2019
).
28.
B.
Zhang
,
V.
Sanjay
,
S.
Shi
,
Y.
Zhao
,
C.
Lv
,
X.-Q.
Feng
, and
D.
Lohse
, “
Impact forces of water drops falling on superhydrophobic surfaces
,”
Phys. Rev. Lett.
129
,
104501
(
2022
).
29.
Z.
Hu
,
F.
Chu
, and
X.
Wu
, “
Double-peak characteristic of droplet impact force on superhydrophobic surfaces
,”
Extreme Mech. Lett.
52
,
101665
(
2022
).
30.
B.
Zhang
,
H.
Zhao
,
Y.
Zhao
,
P.
Hao
, and
C.
Lv
, “
Impact force of ring bouncing on superhydrophobic surface with a bead
,”
Phys. Fluids
35
,
052104
(
2023
).
31.
W.
Fang
,
S.
Wang
,
H.
Duan
,
S. A.
Tahir
,
K.
Zhang
,
L.
Wang
,
X.-Q.
Feng
, and
M.
Song
, “
Target slinging of droplets with a flexible cantilever
,”
Droplet
2
,
e72
(
2023
).
32.
C.
Clanet
,
C.
Beguin
,
D.
Richard
, and
D.
Quere
, “
Maximal deformation of an impacting drop
,”
J. Fluid Mech.
517
,
199
208
(
2004
).
33.
D.
Bartolo
,
C.
Josserand
, and
D.
Bonn
, “
Retraction dynamics of aqueous drops upon impact on non-wetting surfaces
,”
J. Fluid Mech.
545
,
329
338
(
2005
).
34.
N.
Laan
,
K. G.
de Bruin
,
D.
Bartolo
,
C.
Josserand
, and
D.
Bonn
, “
Maximum diameter of impacting liquid droplets
,”
Phys. Rev. Appl.
2
,
044018
(
2014
).
35.
S.-R.
Gao
,
B.-J.
Wei
,
J.-X.
Jin
,
J.-S.
Ye
,
Y.-F.
Wang
,
S.-F.
Zheng
,
Y.-R.
Yang
, and
X.-D.
Wang
, “
Contact time of a droplet impacting hydrophobic surfaces
,”
Phys. Fluids
34
,
067104
(
2022
).
36.
G. I.
Taylor
, “
The dynamics of thin sheets of fluid. III. Disintegration of fluid sheets
,”
Proc. R. Soc. London, Ser. A
253
,
313
321
(
1959
).
37.
F. E. C.
Culick
, “
Comments on a ruptured soap film
,”
J. Appl. Phys.
31
,
1128
1129
(
1960
).
38.
D.
Richard
,
C.
Clanet
, and
D.
Quéré
, “
Contact time of a bouncing drop
,”
Nature
417
,
811
811
(
2002
).
39.
Y.
Liu
,
L.
Moevius
,
X.
Xu
,
T.
Qian
,
J. M.
Yeomans
, and
Z.
Wang
, “
Pancake bouncing on superhydrophobic surfaces
,”
Nat. Phys.
10
,
515
519
(
2014
).
40.
H.
Zhan
,
C.
Lu
,
C.
Liu
,
Z.
Wang
,
C.
Lv
, and
Y.
Liu
, “
Horizontal motion of a superhydrophobic substrate affects the drop bouncing dynamics
,”
Phys. Rev. Lett.
126
,
234503
(
2021
).
41.
P.-G.
de Gennes
,
F.
Brochard-Wyart
, and
D.
Quéré
,
Capillarity and Wetting Phenomena: Drops, Bubbles, Pearls, Waves
(
Springer
,
New York
,
2004
).

Supplementary Material