2.1 Model

We first need to establish a convenient representation of the drop-on-pool geometry shown in figure 2(b). The problem consists of two axisymmetric liquid domains, the drop and the pool, which we describe by the position of their respective liquid–vapour interfaces $z=h$ (for the drop) and $z=e$ (for the pool), where the $z$ axis points vertically upwards with $z=0$ corresponding to the unperturbed pool surface far away from the drop. These are defined in more detail in figure 3. While $h$ and $e$ in principle provide a full description of the geometry, we also introduce the thickness of the vapour layer $t$ . This is convenient for describing the flow inside the thin vapour layer below the drop, where the two interfaces are essentially parallel.

Following previous theoretical developments on levitated drops (Jones & Wilson Reference Jones and Wilson1978; Lister et al. Reference Lister, Thompson, Perriot and Duchemin2008; Snoeijer et al. Reference Snoeijer, Brunet and Eggers2009; Sobac et al. Reference Sobac, Rednikov, Dorbolo and Colinet2014; Maquet et al. Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016), we consider the upper surfaces of the liquid drop and pool to be at hydrostatic equilibrium while the flow of the produced vapour is treated in the lubrication approximation. We first compute the vapour pressure $P_{v}$ by approaching it from the side of the pool,

(2.1) $$\begin{eqnarray}P_{v}=-\unicode[STIX]{x1D70C}_{p}ge+\unicode[STIX]{x1D6FE}_{p}\unicode[STIX]{x1D705}_{e}.\end{eqnarray}$$

Here we introduced the pool density $\unicode[STIX]{x1D70C}_{p}$ and surface tension $\unicode[STIX]{x1D6FE}_{p}$ , while the $\unicode[STIX]{x1D705}_{e}$ is the curvature of the pool interface. The first term represents the hydrostatic pressure inside the pool, while the curvature term is the Laplace pressure jump due to surface tension. Note that the hydrostatic pressure inside the pool was taken to be $-\unicode[STIX]{x1D70C}_{p}ge$ , i.e. the atmospheric pressure was set to zero. Similarly, we obtain an expression for the $P_{v}$ from the side of the drop

(2.2) $$\begin{eqnarray}P_{v}=k-\unicode[STIX]{x1D70C}_{d}gh-\unicode[STIX]{x1D6FE}_{d}\unicode[STIX]{x1D705}_{h},\end{eqnarray}$$

where $\unicode[STIX]{x1D70C}_{d}$ , $\unicode[STIX]{x1D6FE}_{d}$ , $\unicode[STIX]{x1D705}_{h}$ represent the droplet density, surface tension and curvature and $k$ is an integration constant. Equations (2.1), (2.2) give two separate expressions for $P_{v}$ , which in the lubrication approximation for thin layers must be identical. Therefore (2.1), (2.2) can also be seen as a relation between $h$ and $e$ .

Figure 3.

Sketch of a drop on a pool. Different zones are identified which are used for the asymptotic analysis for ${\mathcal{E}}\ll 1$ , ${\mathcal{R}}\gg 1$ for identical fluid properties ( $\unicode[STIX]{x1D6E4}=1$ , ${\mathcal{P}}=1$ ). The dominant force balances in the inner/outer regimes are indicated as capillary ( $\unicode[STIX]{x1D6FE}$ ), viscous ( $\unicode[STIX]{x1D702}_{v}$ ) and gravitational ( $g$ ). Also defined are the vapour-layer thickness $t$ , which is the separation between the drop interface $h$ and the pool interface $e$ , and $s$ and $n$ , which denote the orientation of the curvilinear coordinate system. Note that in the case of non-equal properties the thickness is also determined by the mechanical properties of both the drop and pool denoted by the subscripts ‘d’ for drop and ‘p’ for pool.

We now turn to the flow inside the vapour layer. It will be shown that for sufficiently small evaporation rates the gap thickness $t$ is asymptotically small, justifying the use of the lubrication theory. We therefore consider the reduced Stokes equation for the parallel velocity $u$ ,

(2.3) $$\begin{eqnarray}\unicode[STIX]{x2202}_{s}P_{v}=\unicode[STIX]{x1D702}_{v}\unicode[STIX]{x2202}_{nn}u,\end{eqnarray}$$

where $s$ is the curvilinear coordinate along the layer, while $n$ is the coordinate perpendicular to the vapour film (see figure 3). Owing to the small gas viscosity $\unicode[STIX]{x1D702}_{v}$ , we here assume that no flow is induced inside the drop and the pool. As a consequence, we can solve (2.3) with no-slip boundary conditions at $n=0$ and $n=t$ , yielding a parabolic profile

(2.4) $$\begin{eqnarray}u=6\bar{u}\left(\frac{n}{t}-\frac{n^{2}}{t^{2}}\right),\end{eqnarray}$$

where we introduced the thickness-averaged velocity

(2.5) $$\begin{eqnarray}\bar{u}=-\frac{t^{2}\unicode[STIX]{x2202}_{s}P_{v}}{12\unicode[STIX]{x1D702}_{v}}.\end{eqnarray}$$

Note that for an infinite drop slip could occur despite the significant viscosity contrast, since the ratio between the drop and film thickness is also large. In that case, the factor $1/12$ changes, depending on the slip length. Only a fully resolved numerical simulation of the Navier–Stokes equations in drop, film and pool will give insight into this effect, which is beyond the scope of this study. Here we stick with the no-slip assumption, frequently used in the literature (Wachters et al. Reference Wachters, Bonne and van Nouhuis1966; Hinch & Lemaitre Reference Hinch and Lemaitre1994; Quéré Reference Quéré2013; Maquet et al. Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016; Janssens, Koizumi & Fried Reference Janssens, Koizumi and Fried2017).

The lubrication problem is closed using the axisymmetric continuity equation,

(2.6) $$\begin{eqnarray}r{\dot{t}}+\unicode[STIX]{x2202}_{s}(rt\bar{u})=rj,\end{eqnarray}$$

where $r$ is the distance from the symmetry axis and ${\dot{t}}$ is a time derivative; in the remainder we will look for (quasi-)steady states (the evaporation time of the drop being much greater than the relaxation time of an initially deposited drop to its quasi-steady shape and in particular the viscous relaxation time in the vapour layer) so that time derivatives can be omitted. The source term $j$ on the right-hand side of (2.6) is due to the flux of vapour generated by evaporation, which modelled by Fourier’s law can be expressed as (Maquet et al. Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016)

(2.7) $$\begin{eqnarray}j=\frac{\unicode[STIX]{x1D716}}{t}\quad \text{with}~\unicode[STIX]{x1D716}=\frac{k_{v}\unicode[STIX]{x0394}T}{L\unicode[STIX]{x1D70C}_{v}}.\end{eqnarray}$$

In this expression $k_{v}$ and $\unicode[STIX]{x1D70C}_{v}$ respectively are the vapour thermal conductivity and density, $L$ the latent heat of evaporation and $\unicode[STIX]{x0394}T$ the temperature difference between the pool and the drop (the superheat). The result deviates here from the description of the drainage problem: while the source term is absent in the drainage problem, similar effects occur due to the thinning of the gap driving the gas flow. Note that in the case of the boules of Hickman, the pool is superheated and evaporating, which can be modelled using Newton’s law of cooling: , where (superheated) pool temperature far away from the drop (Bejan Reference Bejan1993). In this case, $j$ is approximately constant along the film. For now, we focus on the Leidenfrost case of (2.7). The consequences of this different mechanism of vapour generation will be discussed in (§ 3.5).

Thus, the vapour film is described by

(2.8) $$\begin{eqnarray}-\frac{1}{12\unicode[STIX]{x1D702}_{v}\,r}\unicode[STIX]{x2202}_{s}(rt^{3}\unicode[STIX]{x2202}_{s}P_{v})=\frac{\unicode[STIX]{x1D716}}{t}\end{eqnarray}$$

in conjunction with (2.1) and (2.2), which are three coupled equations for the vapour pressure $P_{v}$ and respectively for the droplet and pool surface profiles $h$ and $e$ . These equations need to be complemented by geometric expressions (see appendix A for more details) for the interface curvatures $\unicode[STIX]{x1D705}_{e,h}$ , for $r$ as a function of $s$ , viz.  $(\unicode[STIX]{x2202}_{s}e)^{2}+(\unicode[STIX]{x2202}_{s}r)^{2}=1$ , and for the thickness of the vapour layer, viz.

(2.9) $$\begin{eqnarray}t(s)\,\unicode[STIX]{x2202}_{s}r=h(s)-e(s).\end{eqnarray}$$

At the exit from the vapour film, where it joins the ambient atmosphere and where its thickness $t$ asymptotically diverges, the drop and pool surfaces are expected to attain equilibrium static shapes, described by

(2.10) $$\begin{eqnarray}P_{v}=0,\end{eqnarray}$$

with (2.2) and (2.1), respectively. It may be useful to regard (2.10) as a degenerate form of (2.8) as $t\rightarrow \infty$ . It is matching with such static shapes that is imposed in one way or another (to be specified at each concrete occurrence) as the boundary conditions there.

As for other boundary conditions, no singularity at the symmetry axis (i.e. at $r=0$ ) is imposed. Finally, the pool surface attains its unperturbed level $e=0$ far away from the drop (as $r\rightarrow \infty$ ).

The constant parameter $k$ entering the problem by means of (2.2) is eventually the one quantifying the size of the droplet, and in this sense could be taken as one of the system parameters in the analysis (along with the material properties of the liquids and the superheat). However, we shall rather prefer to quantify the size more directly by means of the radius of the droplet’s vertical projection, $R$ . Hence, with $R$ as a system parameter, $k$ now becomes yet another unknown to be determined. Most cases however yield no closed form for $R(k)$ , hence $k$ is used in the numerical calculations to converge the problem towards a certain desired drop size $R$ .

For the time being, we shall keep the formulation in dimensional form. Appropriate non-dimensionalisations will rather be introduced later on in a context-specific way. However, one can already establish that the results are ultimately governed by four dimensionless parameters, which can be chosen as

(2.11a-d ) $$\begin{eqnarray}\unicode[STIX]{x1D6E4}=\frac{\unicode[STIX]{x1D6FE}_{p}}{\unicode[STIX]{x1D6FE}_{d}},\quad {\mathcal{P}}=\frac{\unicode[STIX]{x1D70C}_{p}}{\unicode[STIX]{x1D70C}_{d}},\quad {\mathcal{R}}=\frac{R}{\unicode[STIX]{x1D706}_{c}},\quad \tilde{{\mathcal{E}}}=\frac{\unicode[STIX]{x1D702}_{v}\unicode[STIX]{x1D716}}{\unicode[STIX]{x1D70C}_{d}g\unicode[STIX]{x1D706}_{c}^{3}}.\end{eqnarray}$$

The first two are the ratios of surface tension and density of the pool and the liquid. The third parameter ${\mathcal{R}}$ is the dimensionless radius of the drop, scaled by the capillary length $\unicode[STIX]{x1D706}_{c}=(\unicode[STIX]{x1D6FE}_{d}/\unicode[STIX]{x1D70C}_{d}g)^{1/2}$ . Finally, the evaporation-induced viscous vapour flow is quantified by the evaporation number $\tilde{{\mathcal{E}}}$ , proportional to the value of the superheat. Note that a key dimensionless number $\tilde{{\mathcal{E}}}$ naturally appears upon substituting (2.2) into (2.8) and normalising all the length variables with $\unicode[STIX]{x1D706}_{c}$ (Sobac et al. Reference Sobac, Rednikov, Dorbolo and Colinet2014; Maquet et al. Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016).

2.2 Asymptotic approach

The values of the evaporation number $\tilde{{\mathcal{E}}}$ encountered in practice are typically rather small (Snoeijer et al. Reference Snoeijer, Brunet and Eggers2009; Celestini, Frish & Pomeau Reference Celestini, Frish and Pomeau2012; Sobac et al. Reference Sobac, Rednikov, Dorbolo and Colinet2014; Maquet et al. Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016). This is what eventually justifies the very structure of the problem assumed in § 2.1: a thin vapour layer between the substrate (here the pool), where the lubrication approximation is applicable, and equilibrium shapes of liquid surfaces (drop and pool) beyond the thin vapour layer. Direct computations of the Leidenfrost problem carried out under this premise confirm its self-consistency for both flat solid substrates (Snoeijer et al. Reference Snoeijer, Brunet and Eggers2009; Sobac et al. Reference Sobac, Rednikov, Dorbolo and Colinet2014) and deformed liquid ones (Maquet et al. Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016). Essential deviations from this scheme are only encountered, on the one hand, for sufficiently small drops, well below the capillary length (Celestini et al. Reference Celestini, Frish and Pomeau2012; Sobac et al. Reference Sobac, Rednikov, Dorbolo and Colinet2014). In the present paper, we shall deal only with drops larger than this (see below), and hence encounter no such limitation. On the other hand, the scheme breaks down on the verge of the chimney instability (Snoeijer et al. Reference Snoeijer, Brunet and Eggers2009; Sobac et al. Reference Sobac, Rednikov, Dorbolo and Colinet2014), which, as already anticipated, will not be encountered in the present case of a liquid substrate the same mechanical properties as the drop.

Thus, in fact, the formulation provided in § 2.1 already tacitly implies $\tilde{{\mathcal{E}}}\ll 1$ . Direct numerical computation for such a ‘full’ formulation can be realised e.g. using an approach largely similar to Sobac et al. (Reference Sobac, Rednikov, Dorbolo and Colinet2014) and Maquet et al. (Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016). Here it is just rendered geometrically more elaborate in order to handle large deformations of the pool surface, see appendix A for more details.

However, $\tilde{{\mathcal{E}}}\ll 1$ also opens the way to a systematic asymptotic analysis, consistently and thoroughly exploiting this limit. This is actually what the present paper is about. As is typically the case, such an asymptotic analysis will permit further insight into the physics of the problem. Here we shall in particular be interested in further details as far as the structure of the vapour layer is concerned. Importantly, this will also permit us to establish the scaling with $\tilde{{\mathcal{E}}}$ of various quantities of interest. In the case of a flat solid substrate, such a program has been realised e.g. by Snoeijer et al. (Reference Snoeijer, Brunet and Eggers2009) and Sobac et al. (Reference Sobac, Rednikov, Dorbolo and Colinet2014). As already stated, we anticipate essential differences in the case of the liquid substrate we are concerned with in the present paper. The hereby obtained asymptotic results will be validated against the direct numerical simulation mentioned earlier in the framework of the full formulation of § 2.1, while highlighting similarities and differences with the description of the drainage problem.

With the expected asymptotically small vapour-layer thickness $t$ in the limit of small evaporation numbers $\tilde{{\mathcal{E}}}\ll 1$ , one actually realises that the shape of our Leidenfrost drop must be asymptotically close to that of an equilibrium ‘superhydrophobic’ drop. The shape of the latter is governed by the static balance between surface tension and gravity. Namely, in this superhydrophobic configuration, the liquid–liquid interface is determined by (2.1) and (2.2) with $e\equiv h$ and formally possesses an interfacial tension $\unicode[STIX]{x1D6FE}_{dp}\equiv \unicode[STIX]{x1D6FE}_{p}+\unicode[STIX]{x1D6FE}_{d}$ ; the liquid–gas interface is described by (2.2) with (2.10) for the drop itself, and by (2.1) with (2.10) for the pool; at the contact (triple) line, the slopes of all the three interfaces coincide, and a contact angle of $180^{\circ }$ results from the side of each of the liquids (see appendix B for the computation method). It is important to note that the picture in terms of a superhydrophobic drop refers to a large-scale description: in the actual non-equilibrium configuration, the ‘contact line’ in fact represents the position of a thin neck region through which the vapour escapes to the surrounding atmosphere.

Once the superhydrophobic shape is known, the leading-order pressure distribution governing the vapour flow in (2.8) can immediately be drawn from (2.1), or equivalently from (2.2). This distribution will clearly not be constant in the pool case, with an appreciably non-flat surface, i.e. we end up with $\unicode[STIX]{x2202}_{s}P_{v}\neq 0$ independently (to leading order) of the actual vapour-layer profile $t(s)$ . This is in stark contrast to a drop on a flat rigid substrate, for which $\unicode[STIX]{x2202}_{s}P_{v}\neq 0$ does depend upon $t(s)$ (i.e. upon a higher-order approximation in terms of $\tilde{{\mathcal{E}}}\ll 1$ ). We shall see that this is the key factor giving rise to different vapour-layer structures and scalings for the two types of substrate, typical for drops on deformable surfaces (Jones & Wilson Reference Jones and Wilson1978; Maquet et al. Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016).

However, a common feature between the two types of substrate is that $P_{v}$ will not be continuous across the ‘triple line’, i.e. across the thin neck region through which the vapour escapes from below the drop. This is due to a mismatch in curvature on both sides of the neck, where $P_{v}$ exhibits a jump from $P_{v}>0$ under the drop to the ambient value $P_{v}=0$ . In experiments however $P_{v}$ will be continuous, which will be discussed in more detail in § 3.2.2. The appearance of this thin neck allows us to introduce and exploit the following hierarchy of length scales

(2.12) $$\begin{eqnarray}t_{n}\ll t_{0}\ll \unicode[STIX]{x1D706}_{c}\sim R,\end{eqnarray}$$

where $t_{0}$ and $t_{n}$ are, respectively, the typical vapour layer thicknesses outside and inside the neck region. Such a presence of separate distinguished regions with different spatial scales means that we resort to matched asymptotic expansions as the most appropriate asymptotic method for the problem at hand. Overall, it turns out that the problem can be split into the following regions, indicated schematically in figure 3. At large scales, there are two outer regions: region 1 below the drop, and region 2 above the drop and pool. In the limit of vanishing $t$ , these outer solutions will precisely correspond to superhydrophobic drops on a liquid pool. As already mentioned, these are equilibrium solutions that can be computed from the static balance between surface tension and gravity. These two outer regions are connected by a smaller inner region, which is nothing other than the earlier mentioned neck region. It will turn out that no direct matching between the outer and inner regions is possible in the vapour layer, and so yet another, intermediate region is implied, which is also marked in figure 3.

As already pointed out, the expected completely new type of solution and the $\tilde{{\mathcal{E}}}$ -scalings for the vapour layer basically owe themselves to the substrate surface deformability. Note however that, for smaller drops, $R<\unicode[STIX]{x1D706}_{c}$ ( ${\mathcal{R}}<1$ ), the pool surface becomes increasingly flat (Maquet et al. Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016). Therefore, for sufficiently small drops, the appropriate asymptotic theory is likely to involve other smallness parameters apart from $\tilde{{\mathcal{E}}}$ , viz. a geometric one characterising the small substrate non-flatness. Another kind of limitation for smaller drops and related to the mentioned intermediate region will be pointed out in § 4.1. However, in essence, we shall consider drops that are not sufficiently large to be beyond the scope of the present paper.

Furthermore, a large part of our analysis (§ 3) will be dedicated to very large drops, $R\gg \unicode[STIX]{x1D706}_{c}$ ( ${\mathcal{R}}\gg 1$ ). The expected hierarchy of length scales (2.12) then rewrites as

(2.13) $$\begin{eqnarray}t_{n}\ll t_{0}\ll \unicode[STIX]{x1D706}_{c}\ll R.\end{eqnarray}$$

Besides, inspired by the boules of Hickman (Reference Hickman1964a ), we launch the analysis by considering liquids with equal properties, $\unicode[STIX]{x1D6E4}=1$ and $P=1$ . Mathematically, this gives rise to the simplest possible configuration (the associated superhydrophobic drop assuming a hemispherical shape), where analytical solutions are possible and which is a good starting point for developing the essence of our asymptotic approach. Subsequently, in § 4, we extend our analysis to smaller drops, $R\sim \unicode[STIX]{x1D706}_{c}$ ( ${\mathcal{R}}\sim 1$ ), and to non-equal liquid properties, $\unicode[STIX]{x1D6E4}\neq 1$ and/or ${\mathcal{P}}\neq 1$ .

3.1 Outer region 1: below the drop

3.1.1 The droplet shape

The outer shape of the drop and pool can be obtained by combining (2.1) and (2.2):

(3.1) $$\begin{eqnarray}0=k-\unicode[STIX]{x1D70C}g(h-e)-\unicode[STIX]{x1D6FE}(\unicode[STIX]{x1D705}_{h}+\unicode[STIX]{x1D705}_{e}),\end{eqnarray}$$

where we assumed identical material properties $\unicode[STIX]{x1D6FE}=\unicode[STIX]{x1D6FE}_{d}=\unicode[STIX]{x1D6FE}_{p}$ and $\unicode[STIX]{x1D70C}=\unicode[STIX]{x1D70C}_{d}=\unicode[STIX]{x1D70C}_{p}$ . We anticipate the gap thickness, $t\sim h-e$ , to be much smaller than the radius, in which case $\unicode[STIX]{x1D705}_{h}\simeq \unicode[STIX]{x1D705}_{e}$ . The hydrostatic term can also be neglected when $t\sim (h-e)\ll 4\unicode[STIX]{x1D6FE}/\unicode[STIX]{x1D70C}gR\sim \unicode[STIX]{x1D706}_{c}^{2}/R$ , a condition that is much more severe and will be monitored for our solution a posteriori. Equation (3.1) then further simplifies,

(3.2) $$\begin{eqnarray}0=k-2\unicode[STIX]{x1D6FE}\unicode[STIX]{x1D705}_{h},\end{eqnarray}$$

imposing a shape of constant curvature. Below we will find that the matching condition requires the outer solution to be a perfect hemisphere. Hence, we can identify $k=4\unicode[STIX]{x1D6FE}/R$ , where $R$ is the maximum radius of the drop.

3.1.2 The vapour thickness

The spherical geometry of the outer solution, and thus of the vapour layer, suggests that the analysis of the lubrication flow will be most easily expressed using spherical coordinates (see figure 4). In this coordinate system, the lubrication equation (2.8) reads

(3.3) $$\begin{eqnarray}\displaystyle -\frac{1}{12\unicode[STIX]{x1D702}_{v}R^{2}~\sin \unicode[STIX]{x1D703}}\unicode[STIX]{x2202}_{\unicode[STIX]{x1D703}}\left[\sin \unicode[STIX]{x1D703}~t^{3}~\unicode[STIX]{x2202}_{\unicode[STIX]{x1D703}}P_{v}\right]=\frac{\unicode[STIX]{x1D716}}{t}. & & \displaystyle\end{eqnarray}$$

This equation needs to be complemented by an equation for the pressure gradient $P_{v}^{\prime }$ , for example (2.2), which in spherical coordinates simplifies to $\unicode[STIX]{x2202}_{\unicode[STIX]{x1D703}}P_{v}=-\unicode[STIX]{x1D70C}gR\sin \unicode[STIX]{x1D703}$ . The lubrication equation can then be expressed as

(3.4) $$\begin{eqnarray}\frac{1}{2t^{3}\sin \unicode[STIX]{x1D703}}\unicode[STIX]{x2202}_{\unicode[STIX]{x1D703}}[t^{3}\sin ^{2}\unicode[STIX]{x1D703}]=\frac{6\unicode[STIX]{x1D702}_{v}\unicode[STIX]{x1D716}R}{\unicode[STIX]{x1D70C}gt^{4}}.\end{eqnarray}$$

In this expression we have collected all dimensional parameters on the right-hand side, to form a dimensionless ratio.

Figure 4.

A sketch of outer region 1 is shown in (a). Since the shape below the drop reduces to a hemisphere, we adopt a spherical coordinate system where the gap thickness $t$ depends on the angle $\unicode[STIX]{x1D703}$ . (b) The local Cartesian coordinate system around $\unicode[STIX]{x1D703}=\unicode[STIX]{x03C0}/2$ , which is used for the analysis of the thin neck region at the exit of the vapour layer. The drop and pool interfaces are expressed as $d(x)$ and $p(x)$ respectively, while the vapour thickness reads $t=d-p$ . The vapour thickness profile (3.9), non-dimensionalised using the scale of (3.5), is represented in (c).

The above expression invites us to introduce a dimensionless thickness $\tilde{t}=t/t_{\ast }$ , where the characteristic scale for the thickness reads

(3.5) $$\begin{eqnarray}t_{\ast }=\left(\frac{6\unicode[STIX]{x1D702}_{v}R\unicode[STIX]{x1D716}}{\unicode[STIX]{x1D70C}g}\right)^{1/4}=\unicode[STIX]{x1D706}_{c}\,{\mathcal{E}}^{1/4},\end{eqnarray}$$

where a (modified) evaporation number

(3.6) $$\begin{eqnarray}{\mathcal{E}}=\frac{6\unicode[STIX]{x1D702}_{v}R\unicode[STIX]{x1D716}}{\unicode[STIX]{x1D70C}_{d}g\unicode[STIX]{x1D706}_{c}^{4}}=\frac{6R}{\unicode[STIX]{x1D706}_{c}}\,\tilde{{\mathcal{E}}}\end{eqnarray}$$

has been introduced, as it naturally occurs in this form in the present ${\mathcal{R}}\gg 1$ context. Inserting this rescaling into (3.4) and working out the derivatives gives

(3.7) $$\begin{eqnarray}\displaystyle \tilde{t}^{3}\unicode[STIX]{x2202}_{\unicode[STIX]{x1D703}}\tilde{t}=\frac{2\left[1-\tilde{t}^{4}\cos \unicode[STIX]{x1D703}\right]}{3\sin \unicode[STIX]{x1D703}}, & & \displaystyle\end{eqnarray}$$

which is a first-order ordinary differential equation (ODE) for the profile of the vapour layer $\tilde{t}(\unicode[STIX]{x1D703})$ . The solution to this equation can be cast in closed form

(3.8) $$\begin{eqnarray}\displaystyle \left[\tilde{t}(\unicode[STIX]{x1D703})\right]^{4} & = & \displaystyle \frac{\displaystyle 8\int _{0}^{\unicode[STIX]{x1D703}}\text{d}x\,(\sin x)^{5/3}}{3(\sin \unicode[STIX]{x1D703})^{8/3}}=\frac{8}{15}\frac{1}{(\sin \unicode[STIX]{x1D703})^{8/3}}\nonumber\\ \displaystyle & & \displaystyle \times ~\left(\frac{\unicode[STIX]{x03C0}^{1/2}\unicode[STIX]{x1D6E4}\left(\frac{1}{3}\right)}{\unicode[STIX]{x1D6E4}\left(\frac{5}{6}\right)}-\cos \unicode[STIX]{x1D703}\left(2\;_{2}\text{F}_{1}\left[\frac{1}{2},\frac{2}{3},\frac{3}{2},(\cos \unicode[STIX]{x1D703})^{2}\right]+3(\sin \unicode[STIX]{x1D703})^{2/3}\right)\right).\qquad\end{eqnarray}$$

Here, we imposed a non-singular behaviour at the symmetry axis, only possible with $\tilde{t}_{0}\equiv \tilde{t}(0)=1$ , which was anticipated in the definition in (3.5). Here $\unicode[STIX]{x1D6E4}(x)$ is the gamma function, $_{2}F_{1}$ is a generalised hypergeometric function (Weisstein Reference Weisstein2017) and this expression was obtained using Mathematica. The functional form is different here compared to the film drainage problem, as the present source term has a $1/t$ dependence, while in the latter case it is a function of $\unicode[STIX]{x1D703}$ (Jones & Wilson Reference Jones and Wilson1978). When plotting the solution (3.8), one observes that the vapour thickness is nearly constant, see figure 4(c). It very mildly increases from $\tilde{t}=1$ at $\unicode[STIX]{x1D703}=0$ , to a slightly larger value at $\unicode[STIX]{x1D703}=\unicode[STIX]{x03C0}/2$ (the exit of the gap):

(3.9) $$\begin{eqnarray}\tilde{t}_{exit}=2^{3/4}15^{-1/4}\unicode[STIX]{x03C0}^{1/8}\left(\frac{\unicode[STIX]{x1D6E4}\left(\frac{1}{3}\right)}{\unicode[STIX]{x1D6E4}\left(\frac{5}{6}\right)}\right)^{1/4}\approx 1.22386\cdots \,.\end{eqnarray}$$

Comparing the vapour film with that of a drop on a heated plate, we find that the film only mildly changes towards the free atmosphere. For a drop on a plate, a much stronger scaling was found for the dependency of the vapour thickness, depending on both the radius and evaporation number (Sobac et al. Reference Sobac, Rednikov, Dorbolo and Colinet2014). As a result, the global evaporation rate is much higher for the present case as the drop is close to the heat source throughout the vapour gap.

3.1.3 Summary and comparison to numerical solution

An important set of analytical results has thus been obtained. First, we found that the immersed part of the drop takes a hemispherical shape. Second, the vapour-layer thickness at the axis below the drop is given by $\tilde{t}_{0}=1$ . Third, the profile of the vapour layer in the outer zone is characterised by a single, universal profile, given by the expression (3.8). For the matching to the neck region (see figure 4), an important result is the thickness at the ‘gap exit’ at $\unicode[STIX]{x1D703}=\unicode[STIX]{x03C0}/2$ , for which the analytical expression (3.9) is found. In dimensional form, we thus obtain the relevant thicknesses

(3.10a,b ) $$\begin{eqnarray}t_{0}=\unicode[STIX]{x1D706}_{c}{\mathcal{E}}^{1/4},\quad t_{exit}=1.22386\cdots \,\unicode[STIX]{x1D706}_{c}{\mathcal{E}}^{1/4}.\end{eqnarray}$$

These results were obtained under the assumption of the hierarchy of scales (2.13), which is self-consistent as long as

(3.11) $$\begin{eqnarray}{\mathcal{E}}^{1/4}\ll 1\ll {\mathcal{R}}\ll {\mathcal{E}}^{-1/4}.\end{eqnarray}$$

Note the latter, strong inequality arising from neglecting the hydrostatic pressure difference across the vapour gap $(t\ll \unicode[STIX]{x1D706}_{c}^{2}/R)$ . To validate these findings, we compared the results to numerical solutions of the full problem formulated in § 2.1 (see also appendix A). Indeed, it is observed that for large drop volumes the immersed part of the droplet approaches a perfect hemisphere. In figure 5 we provide a further quantitative test, by plotting the central thickness $t_{0}$ for a droplet of radius $R=10\unicode[STIX]{x1D706}_{c}$ . Upon reducing the evaporation number ${\mathcal{E}}$ , the numerical result perfectly approaches the prediction (3.10). Moreover, note that the last inequality (3.11) is well satisfied in the given range of ${\mathcal{E}}$ . Evaluating $t_{0}$ for the experimental conditions of figure 1, we obtain $t_{0}\approx 70~\unicode[STIX]{x03BC}\text{m}$ .

Figure 5.

Results for the central thickness $t_{0}\equiv t(0)$ of the vapour layer versus the evaporation number for a drop of $R=10\unicode[STIX]{x1D706}_{c}$ on a pool having the same properties as the drop. The data points (numerical solution to the full problem) approach the curve $t_{0}=\unicode[STIX]{x1D706}_{c}{\mathcal{E}}^{1/4}$ obtained by asymptotic methods in the limit of small ${\mathcal{E}}$ .

3.2 Outer region 2

3.2.2 Mismatch with outer solution 1

Importantly, the puddle solution exhibits a finite curvature at the droplet’s edge, namely $\unicode[STIX]{x1D705}=2^{1/2}/\unicode[STIX]{x1D706}_{c}$ . This value of the curvature is obtained since, by symmetry, the puddle approaches the neck region vertically. This is to be contrasted with the curvature in the other outer region, below the drop, for which the curvature was found to be $1/R$ . For large drops, we thus find a ‘mismatch’ in curvature near the exit of the vapour layer. This implies that the problem requires an inner zone that smoothly joins the two outer regions. The matching is illustrated in figure 6, where we present a numerical solution to the problem (details are given in the paragraphs below). The centre panel provides a detailed view of the droplet and pool profiles, and reveals a thin neck that is connected to the outer vapour layer. The curvature of these profiles are presented in figure 6, for various values of ${\mathcal{E}}$ . The dashed line corresponds to the puddle solution; the numerical profiles smoothly join the puddle to the vapour film of vanishing curvature at $\hat{x}=0$ .

Figure 6.

The interface curvature $\unicode[STIX]{x1D705}$ in the neck region, obtained numerically from (3.15) for various evaporation rates ${\mathcal{E}}$ . A distinctive jump in curvature can be seen, indicating a sharp pressure jump through the thin neck. The dashed line shows the puddle solution for outer region 2.

3.3 Inner region: the neck profile

3.3.1 Matching conditions and numerical solution

By inspection of figure 6, the thin neck region represents a small vertical zone around $\unicode[STIX]{x1D703}=\unicode[STIX]{x03C0}/2$ . We therefore adopt a local Cartesian coordinate system, as sketched in figure 4, where gravity acts along the $x$ -axis towards $x<0$ . In this coordinate frame, we describe the drop interface as $d(x)$ and the pool interface as $p(x)$ . The gap thickness is then expressed as $t(x)=d(x)-p(x)$ and its curvature $\unicode[STIX]{x1D705}_{t}(x)=\unicode[STIX]{x1D705}_{d}(x)-\unicode[STIX]{x1D705}_{p}(x)$ . The expressions for the pressure in the film from (2.1) and (2.2), for equal liquid properties and $k=0$ , can be written as

(3.12) $$\begin{eqnarray}\displaystyle \left.\begin{array}{@{}c@{}}\displaystyle P_{v}=-\unicode[STIX]{x1D70C}gx-\unicode[STIX]{x1D6FE}\unicode[STIX]{x1D705}_{d}\\ \displaystyle P_{v}=-\unicode[STIX]{x1D70C}gx+\unicode[STIX]{x1D6FE}\unicode[STIX]{x1D705}_{p}.\end{array}\right\} & & \displaystyle\end{eqnarray}$$

Taking the difference of these equations, one finds $\unicode[STIX]{x1D705}_{d}=-\unicode[STIX]{x1D705}_{p}=\unicode[STIX]{x1D705}_{t}/2$ , resulting in a symmetric deformation for both $d$ and $p$ . Equation (2.8) then becomes

(3.13) $$\begin{eqnarray}\displaystyle \frac{1}{12\unicode[STIX]{x1D702}_{v}}\unicode[STIX]{x2202}_{x}\left[t^{3}\unicode[STIX]{x2202}_{x}\left[\unicode[STIX]{x1D70C}gx+\frac{1}{2}\unicode[STIX]{x1D6FE}\unicode[STIX]{x2202}_{xx}t\right]\right]=\frac{\unicode[STIX]{x1D716}}{t}\approx 0, & & \displaystyle\end{eqnarray}$$

where we used the small slope representation of the curvature $\unicode[STIX]{x1D705}_{t}=t^{\prime \prime }$ for consistency with the lubrication approximation. Since we expect the local vapour generation in the small inner region to be negligible compared to the total generated flux, we can also drop the right-hand side. Since we expect the total generated flux to mainly come from the outer region 1 (verifiable a posteriori), we can neglect the flux contribution from the inter region and hence drop the right-hand side in the framework of the leading-order approximation. Ultimately the gap profile needs to be matched to that of the puddle shape $d(x)$ . It is therefore convenient to express the lubrication profile by $d(x)=t(x)/2$ , and non-dimensionalise all lengths by $\unicode[STIX]{x1D706}_{c}$ :

(3.14a,b ) $$\begin{eqnarray}\hat{d}=\frac{d}{\unicode[STIX]{x1D706}_{c}}=\frac{t}{2\unicode[STIX]{x1D706}_{c}},\quad \hat{x}=\frac{x}{\unicode[STIX]{x1D706}_{c}}.\end{eqnarray}$$

With this, we obtain after integrating (3.13) once:

(3.15) $$\begin{eqnarray}\hat{d}^{\prime \prime \prime }=\frac{c^{3}}{\hat{d}^{3}}-1,\end{eqnarray}$$

where $c$ is an integration constant. This equation describes the shape of the drop interface inside the neck region, which is also found in the drainage problem, where $c$ is changing with time as the film thins.

The problem is closed by the matching conditions to the outer regions 1 and 2, respectively corresponding to negative and positive limits of $\hat{x}$ . The curvature of outer region 1 scales as $1/R$ , which in dimensionless variables gives $\hat{d}^{\prime \prime }\sim 1/{\mathcal{R}}$ and is thus asymptotically small for large drops, implying $\hat{d}^{\prime }(-\infty )=\hat{d}^{\prime \prime }(-\infty )=0$ . Therefore, we require that $\hat{d}(-\infty )$ approaches a constant value, which according to (3.15) can be equated to $c$ . This thickness must ultimately match the ‘exit’ thickness of outer zone 1, leading to the condition

(3.16) $$\begin{eqnarray}\frac{t_{exit}}{2}=d(-\infty )\Longrightarrow c=\frac{1}{2}\cdot 1.22386\cdots {\mathcal{E}}^{1/4}.\end{eqnarray}$$

The boundary condition for positive $\hat{x}$ comes from matching the curvature of the puddle solution, which in scaled units reads $\hat{d}^{\prime \prime }=\sqrt{2}$ (see § 3.2). We numerically solved (3.15) subject to these boundary conditions.

The resulting neck profiles are presented figure 7 for different values of ${\mathcal{E}}$ , corresponding to different gap thickness according to (3.16). One can observe that reducing the flux ${\mathcal{E}}$ leads to a localisation of the neck region, both in terms of thickness and lateral extent. To highlight these trends we have reported the profiles on two panels with double logarithmic scales, centred around the position $\hat{x}_{n}$ of the minimum neck thickness (see caption for details). The same data were used to show the mismatch in curvature in figure 6. It is interesting to note that the profiles are strongly reminiscent of dimple profiles observed in dip coating (Snoeijer et al. Reference Snoeijer, Ziegler, Andreotti, Fermigier and Eggers2008), which are indeed governed by an equation similar to (3.15). Apart from the dimple, the dip-coating solutions also exhibit the oscillations seen in figure 7(a), which were analysed in detail by Benilov et al. (Reference Benilov, Chapman, McLeod, Ockendon and Zubkov2010).

Figure 7.

Neck profiles obtained from numerical solution of (3.15) for various vapour-layer thicknesses $\hat{d}(-\infty )\sim {\mathcal{E}}^{1/4}$ for the case of equal drop and pool properties and large drops ( $R\gg \unicode[STIX]{x1D706}_{c}$ ). The double logarithmic representation of the two panels, with an inverse log-scale centred around the neck position $\hat{x}=\hat{x}_{n}$ , reveals the details of the thin neck region and the oscillations upon approaching the vapour film. The dotted line indicates the location of the oscillations, scaling as $\hat{d}\sim (\hat{x}_{n}-\hat{x})^{3}$ . The dashed line shows the puddle solution for outer region 2, exhibiting a $\hat{d}\sim (\hat{x}-\hat{x}_{n})^{2}$ upon approaching the neck.

3.3.2 Self-similar solution for the neck region

Based on our numerical results we observe that the neck region near position $\hat{x}_{n}$ becomes increasingly localised for small ${\mathcal{E}}$ , while the neck thickness $\hat{d}_{n}$ is found to decrease. This is in direct analogy to the neck region for both settling drops and normal Leidenfrost drops above a rigid surface (Yiantsios & Davis Reference Yiantsios and Davis1990; Snoeijer et al. Reference Snoeijer, Brunet and Eggers2009; Sobac et al. Reference Sobac, Rednikov, Dorbolo and Colinet2014). Owing to the smallness of $\hat{d}$ inside this region, (3.15) reduces to

(3.17) $$\begin{eqnarray}\hat{d}^{3}\hat{d}^{\prime \prime \prime }=c^{3},\end{eqnarray}$$

which means that the gravity is subdominant with respect to viscosity and surface tension. Indeed, equation (3.17) is identical to the neck equation studied, first by Wilson & Jones (Reference Wilson and Jones1983) in the context of film draining and later by Snoeijer et al. (Reference Snoeijer, Brunet and Eggers2009) in the case of Leidenfrost drops, which admits similarity solutions

(3.18) $$\begin{eqnarray}\hat{d}(x)=c^{\unicode[STIX]{x1D6FC}}\,T(\unicode[STIX]{x1D701}),\quad \text{with}~\unicode[STIX]{x1D701}=\frac{\hat{x}-\hat{x}_{n}}{c^{\unicode[STIX]{x1D6FD}}}.\end{eqnarray}$$

Inserting this ansatz into (3.17) gives

(3.19a,b ) $$\begin{eqnarray}T^{3}T^{\prime \prime \prime }=1\quad \text{and}\quad 4\unicode[STIX]{x1D6FC}-3\unicode[STIX]{x1D6FD}=3.\end{eqnarray}$$

The exponents $\unicode[STIX]{x1D6FC},\unicode[STIX]{x1D6FD}$ can be determined from a matching condition for $\unicode[STIX]{x1D701}\gg 1$ , for which the shape of the pool $\hat{d}(x)\simeq (\hat{x}-\hat{x}_{n})^{2}/\sqrt{2}$ must be approached, regardless of the value of $c$ . This implies for large $\unicode[STIX]{x1D701}$ ,

(3.20) $$\begin{eqnarray}c^{\unicode[STIX]{x1D6FC}}\,T(\unicode[STIX]{x1D701})\simeq c^{\unicode[STIX]{x1D6FC}}\,\unicode[STIX]{x1D701}^{2}/\sqrt{2}=c^{\unicode[STIX]{x1D6FC}-2\unicode[STIX]{x1D6FD}}\,(\hat{x}-\hat{x}_{n})^{2}/\sqrt{2},\end{eqnarray}$$

hence, $\unicode[STIX]{x1D6FC}-2\unicode[STIX]{x1D6FD}=0$ . Combined with (3.19), this gives the exponents $\unicode[STIX]{x1D6FC}=6/5$ and $\unicode[STIX]{x1D6FD}=3/5$ .

While for large positive $\unicode[STIX]{x1D701}$ we can impose the asymptotic boundary condition $T^{\prime \prime }\simeq \sqrt{2}$ , we still need to provide the asymptotics for negative $\unicode[STIX]{x1D701}$ . We now show that the matching to the film region implies $T^{\prime \prime }\simeq 0$ as the missing boundary condition. The matching to the film can in principle be obtained from a detailed analysis of the oscillatory approach to the thin film, in the spirit of the work on dip coating (Wilson & Jones Reference Wilson and Jones1983; Benilov et al. Reference Benilov, Chapman, McLeod, Ockendon and Zubkov2010). Here we focus only on the first oscillation, which is sufficient for the present purpose. The typical slope of the neck solution $\hat{d}^{\prime }\sim c^{3/5}\sim {\mathcal{E}}^{3/20}$ must be compared to that of the first bump. This bump has its own thickness scale $\hat{\unicode[STIX]{x1D6FF}}_{b}$ and lateral scale $\hat{\ell }_{b}$ , such that we demand $\hat{\unicode[STIX]{x1D6FF}}_{b}/\hat{\ell }_{b}\sim {\mathcal{E}}^{3/20}$ . For the approach of the bump we argue that all terms in (3.15) are involved, such that $\hat{d}^{\prime \prime \prime }$ must be of order unity, or $\hat{\unicode[STIX]{x1D6FF}}_{b}/\hat{\ell }_{b}^{3}\sim {\mathcal{E}}^{0}$ . This scaling indeed gives the correct estimation for the position of the first oscillations in figure 7(a) (dotted line). Combining these two equations on $\hat{\unicode[STIX]{x1D6FF}}_{b}$ and $\hat{\ell }_{b}$ we find $\hat{\unicode[STIX]{x1D6FF}}_{b}\sim {\mathcal{E}}^{9/40}$ and $\hat{\ell }_{b}\sim {\mathcal{E}}^{3/40}$ . The final step is to evaluate the curvature of the bump $\hat{\unicode[STIX]{x1D6FF}}_{b}/\hat{\ell }_{b}^{2}\sim {\mathcal{E}}^{3/40}$ , which as anticipated, vanishes for small ${\mathcal{E}}$ .

In summary, we expect the neck to be governed by a similarity solution $T(\unicode[STIX]{x1D701})$ , which can be computed from (3.19) subject to boundary conditions $T^{\prime \prime }(-\infty )=0$ and $T^{\prime \prime }(\infty )=\sqrt{2}$ . The numerical solution is given in figure 8, represented as a dashed line. The other curves correspond to the profiles of figure 7, scaled according to (3.18). We observe a collapse onto the similarity solution as the value of $c\sim {\mathcal{E}}^{1/4}$ is reduced. The relation for the minimum neck thickness can now be found by determining the minimum of the similarity function, which we numerically find to be $T_{n}=1.147\cdots \,$ . Hence, we find

(3.21) $$\begin{eqnarray}\hat{d}_{n}=1.147\cdots c^{6/5},\end{eqnarray}$$

which provides the minimum thickness at the neck, as confirmed in figure 8(b).

Figure 8.

The neck region exhibits a self-similar structure, captured by the similarity function $T(\unicode[STIX]{x1D701})$ given by the dashed line (a). The other curves represent numerical profiles of the neck shown in figure 7 for different $c$ , scaled according to $T=\hat{d}/c^{6/5}$ and $\unicode[STIX]{x1D701}=(\hat{x}-\hat{x}_{n})/c^{3/5}$ . Each of these profiles corresponds to a dot in (b), where the straight solid line corresponds to the similarity law (3.21). The case of equal drop and pool properties and large drops ( $R\gg \unicode[STIX]{x1D706}_{c}$ ).

3.4 Summary

Let us now conclude the analysis for ${\mathcal{E}}\ll 1$ , ${\mathcal{R}}\gg 1$ for the case where the drop and the pool consist of the same liquid ( $\unicode[STIX]{x1D6E4}=1$ , ${\mathcal{P}}=1$ ). We first recall the expressions for the vapour-layer thickness below the centre of the drop ( $t_{0}$ ) and the vapour thickness as it approaches the neck ( $t_{exit}$ ):

(3.22a,b ) $$\begin{eqnarray}t_{0}=\unicode[STIX]{x1D706}_{c}{\mathcal{E}}^{1/4},\quad t_{exit}=1.22386\cdots \unicode[STIX]{x1D706}_{c}{\mathcal{E}}^{1/4}.\end{eqnarray}$$

These can now be complemented by the minimum thickness of the neck

(3.23) $$\begin{eqnarray}t_{n}=2\unicode[STIX]{x1D706}_{c}\hat{d}_{n}=1.272\cdots \unicode[STIX]{x1D706}_{c}{\mathcal{E}}^{3/10},\end{eqnarray}$$

which was obtained using (3.16) and (3.21). The hierarchy of scales (2.13) is indeed satisfied and the approach is self-consistent as long as

(3.24) $$\begin{eqnarray}{\mathcal{E}}^{3/10}\ll {\mathcal{E}}^{1/4}\ll 1\ll {\mathcal{R}}\ll {\mathcal{E}}^{-1/4},\end{eqnarray}$$

which completes the analysis.

3.5 Hickman’s boules

We now briefly discuss the original boules of Hickman, where the vapour is generated from the superheated pool. As anticipated in § 2, the vapour generation can be described by Newton’s law of cooling: , where  is the heat transfer coefficient and the temperature difference now defined based on the (superheated) pool temperature far away from the drop (Bejan Reference Bejan1993). In this case, $j$ is approximately constant along the gap. Therefore, proceeding in a similar manner as discussed before in § 3 we now obtain for the vapour thickness in outer region 1:

(3.25) $$\begin{eqnarray}\frac{1}{2\sin \unicode[STIX]{x1D703}}\unicode[STIX]{x2202}_{\unicode[STIX]{x1D703}}\left[\sin ^{2}\unicode[STIX]{x1D703}~t^{3}\right]=\frac{6j\unicode[STIX]{x1D702}_{v}R}{\unicode[STIX]{x1D70C}g}.\end{eqnarray}$$

This is the equivalent of (3.4), now adapted to the Hickman boule. Solving this equation yields

(3.26) $$\begin{eqnarray}t(\unicode[STIX]{x1D703})=\left(2\frac{1-\cos \unicode[STIX]{x1D703}}{\sin ^{2}\unicode[STIX]{x1D703}}\right)^{1/3}\left(\frac{6j\unicode[STIX]{x1D702}_{v}R}{\unicode[STIX]{x1D70C}g}\right)^{1/3}.\end{eqnarray}$$

From this we deduce the (non-dimensional) vapour-layer thickness below the centre of the drop ( $\tilde{t}_{0}=\tilde{t}(0)$ ) and the vapour thickness as it approaches the neck ( $\tilde{t}_{exit}=\tilde{t}(\unicode[STIX]{x03C0}/2)$ ):

(3.27a,b ) $$\begin{eqnarray}\tilde{t}(0)=\left(\frac{6j\unicode[STIX]{x1D702}_{v}R}{\unicode[STIX]{x1D70C}g\unicode[STIX]{x1D706}_{c}^{3}}\right)^{1/3},\quad \tilde{t}(\unicode[STIX]{x03C0}/2)=1.25992\cdots \left(\frac{6j\unicode[STIX]{x1D702}_{v}R}{\unicode[STIX]{x1D70C}g\unicode[STIX]{x1D706}_{c}^{3}}\right)^{1/3}.\end{eqnarray}$$

An important consequence of this result is that the thickness $t$ scales as $\unicode[STIX]{x0394}T^{1/3}$ , which is fundamentally different from the $\unicode[STIX]{x0394}T^{1/4}$ scaling found previously. This new scaling law caries through to the thickness of the neck, according to $t_{neck}\sim {t_{0}}^{6/5}\sim \unicode[STIX]{x0394}T^{2/5}$ , see § 3.3.2.

4.1 Finite drop size

Let us first focus on finite-sized drops, while keeping $\unicode[STIX]{x1D6E4}={\mathcal{P}}=1$ . The size of the drop can be tuned by the value of $k$ appearing in (2.2), and a numerical example is presented in blue in figure 9. In this particular case the droplet radius ${\mathcal{R}}=R/\unicode[STIX]{x1D706}_{c}=3$ (as seen from above); in general, a relation ${\mathcal{R}}(k)$ can be established numerically (cf. appendix A). Comparing the droplet shape to that of the very large drops in figure 3, one finds that the immersed part of the drop still resembles a spherical cap, but the position of the neck has clearly shifted, resulting in the fact that drop radius ${\mathcal{R}}$ is now smaller than the (dimensionless) radius of curvature of the spherical cap, which we define as ${\mathcal{R}}_{c}$ . The inset shows details of the vapour layer, which also has a similar structure as compared to large drops at small ${\mathcal{E}}$ .

Figure 9.

Profiles calculated for equal property liquids, ${\mathcal{R}}=3$ and ${\mathcal{E}}=8.64\times 10^{-8}$ . Both the superhydrophobic drop calculation and the numerical simulation of the full problem yield a spherical cap solution of curvature $2/{\mathcal{R}}_{c}$ for the gap geometry, in agreement with (3.2). Note that for finite-sized drop ${\mathcal{R}}_{c}\neq {\mathcal{R}}$ and the neck is positioned at $\unicode[STIX]{x1D703}_{n}=1.01$ .

These features can be understood in detail. First, we compare the full numerical solution to the reduced (hydrostatic) calculation for the superhydrophobic drop, as described in § 2.2 (and in more detail in appendix B). The latter is shown as the red dashed curve in figure 9, indeed giving an excellent description of the global shape. As a second step, one can use this global shape to predict the gap thickness. Namely, the superhydrophobic drop provides $P_{v}$ assuming a negligible back influence of the vapour film profile on $P_{v}$ ; this is valid except for the relatively narrow neck and intermediate regions where the capillary (Laplace) pressure due to vapour film deformation is important. Inserting this pressure profile into the lubrication equation (2.8), one can obtain the vapour-layer profile. The result is shown as the red dashed curve in the inset of figure 9 and indeed manifests an excellent quantitative agreement, outside the neck region and in the oscillatory intermediate region.

The same asymptotic analysis as for the infinite drop can be applied. However, care must be taken that the oscillation visible in the inset of figure 9 does not extend all the way to the centre of the drop; otherwise there would be no flat ‘outer region’ below the drop. Hence, we need the width of the bump, $\hat{\ell }_{b}\sim {\mathcal{E}}^{3/40}$ to remain smaller than ${\mathcal{R}}$ . We therefore postulate a new hierarchy of length scales in the case of finite drop sizes, namely

(4.1) $$\begin{eqnarray}t_{n}\ll t_{0}\ll \ell _{b}\ll R,\end{eqnarray}$$

which is the same as $\hat{t}_{n}\ll \hat{t}_{0}\ll \hat{\ell }_{b}\ll {\mathcal{R}}$ , resulting in

(4.2) $$\begin{eqnarray}{\mathcal{E}}^{3/10}\ll {\mathcal{E}}^{1/4}\ll {\mathcal{E}}^{3/40}\ll {\mathcal{R}}.\end{eqnarray}$$

Based on these observations we can now revisit the analysis for the vapour layer. For equal material properties and small evaporation numbers, equation (3.2) is still valid so that the immersed part of the drop has a constant curvature. For the numerical example in figure 9 we find $\unicode[STIX]{x1D706}_{c}\unicode[STIX]{x1D705}_{h}=2\times 0.29=2/{\mathcal{R}}_{c}$ . Also, the lubrication equation (3.7) is still valid. However, since the expression for $P_{v}$ involves ${\mathcal{R}}_{c}$ rather than ${\mathcal{R}}$ , we need to adapt the expression for $t_{\ast }=t_{0}$ accordingly. With this, equation (3.5) and the first expression (3.10) simply become

(4.3) $$\begin{eqnarray}t_{\ast }=t_{0}=\unicode[STIX]{x1D706}_{c}\left(\frac{{\mathcal{R}}_{c}}{{\mathcal{R}}}\right)^{1/4}{\mathcal{E}}^{1/4},\end{eqnarray}$$

where the ratio ${\mathcal{R}}_{c}/{\mathcal{R}}$ can be calculated from the corresponding superhydrophobic drops. When computing the thickness of the very thin neck, i.e. the position where the drop and pool are the closest, one should take into account two further effects due to the finite drop size. First, the neck is no longer positioned at $\unicode[STIX]{x1D703}=\unicode[STIX]{x03C0}/2$ : in the example in figure 9 we find $\unicode[STIX]{x1D703}_{n}=1.01$ , which will lead to a small change in the thickness at the ‘exit’ of the outer region, $t_{exit}$ , in view of the weak variation of $t$ with theta. Second, the matching of the neck to the upper surface of the droplet will be modified, since the droplet’s curvature will change with respect to the value for an infinitely large drop. Since all these factors have to be evaluated numerically, we here just give the scaling of the neck thickness

(4.4) $$\begin{eqnarray}t_{n}\sim \unicode[STIX]{x1D706}_{c}\left(\frac{{\mathcal{R}}_{c}}{{\mathcal{R}}}\right)^{3/10}{\mathcal{E}}^{3/10}.\end{eqnarray}$$

We also note that the prefactor in this law exhibits some dependence on ${\mathcal{R}}$ when ${\mathcal{R}}\approx 1$ , and therefore the scaling $\hat{t}_{n}\sim {\mathcal{R}}^{3/10}$ may not actually hold for ${\mathcal{R}}\approx 1$ . This explains why the apparent scaling identified by Maquet et al. (Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016) was rather $\hat{t}_{n}\sim {\mathcal{R}}^{1/4}$ for the range of radii studied there.

In summary, we conclude that the structure of the present asymptotic analysis and the resulting scaling laws remain the same for finite-sized drops, provided that the undulations near the neck do not penetrate a large fraction of the gap length (i.e. provided that the intermediate region stays significantly shorter than the outer region 1). This being satisfied, in the case of equal liquid properties one can even compute the prefactors, provided that ${\mathcal{R}}_{c}$ and $\unicode[STIX]{x1D703}_{n}$ are determined by considering the corresponding superhydrophobic drop. Note that the (dimensional) drop size $R$ appears both in ${\mathcal{E}}$ and in the prefactors of (4.3) and (4.4). Hence, as already mentioned, one observes a pure scaling relation in terms of $R$ only in the large drop limit, although this is limited to the case of equal liquid properties.

We close the discussion by considering the case when $\unicode[STIX]{x1D6E4}=\unicode[STIX]{x1D6FE}_{p}/\unicode[STIX]{x1D6FE}_{d}\neq 1$ and $P=\unicode[STIX]{x1D70C}_{p}/\unicode[STIX]{x1D70C}_{d}\neq 1$ , i.e. when the drop and pool consist of different liquids. This is for example the case for the ethanol drops on a silicone oil pool studied by Maquet et al. (Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016). Note that the immersed shape is now no longer expected to be a spherical cap due to the generally different densities of the two liquids. As a consequence, we will no longer be able to proceed in fully analytical terms as before. However, asymptotic analyses can still be carried out if we rely on the numerical solution for the equilibrium (static) shape of the associated superhydrophobic drop, which is expected to constitute the leading-order approximation for the Leidenfrost drop shape. (That is possessing the same size $R$ and liquid properties as our Leidenfrost drop, the liquid–liquid interfacial tension being equal to $\unicode[STIX]{x1D6FE}_{d}+\unicode[STIX]{x1D6FE}_{p}$ .) The scaling laws $t_{0}\sim \unicode[STIX]{x1D706}_{c}\tilde{{\mathcal{E}}}^{1/4}$ and $t_{n}\sim \unicode[STIX]{x1D706}_{c}\tilde{{\mathcal{E}}}^{3/10}$ will eventually be recovered, the prefactors being determined numerically through the associated superhydrophobic drop characteristics. We formalise these points below.

We use $\unicode[STIX]{x1D706}_{c}$ as the length scale and $\unicode[STIX]{x1D70C}_{d}g\unicode[STIX]{x1D706}_{c}=\unicode[STIX]{x1D6FE}_{d}/\unicode[STIX]{x1D706}_{c}$ as the pressure scale to introduce dimensionless variables, marked by a hat,

(4.5a-d ) $$\begin{eqnarray}{\hat{s}}=\frac{s}{\unicode[STIX]{x1D706}_{c}},\quad \hat{r}=\frac{r}{\unicode[STIX]{x1D706}_{c}},\quad \hat{z}=\frac{z}{\unicode[STIX]{x1D706}_{c}},\quad \hat{P}_{v}=\frac{P_{v}}{\unicode[STIX]{x1D70C}_{d}g\unicode[STIX]{x1D706}_{c}},\end{eqnarray}$$

similar to earlier used $\hat{t}=t/\unicode[STIX]{x1D706}_{c}$ . Here $r$ is the cylindrical radial coordinate (distance to the symmetry axis), $s$ the arc length (counting from the symmetry axis) along the liquid–liquid interface of the associated superhydrophobic drop in the meridional cross-section, while $z$ is the vertical Cartesian coordinate (cf. figure 3). In the outer region 1 considered in the framework of our present asymptotic scheme (cf. figure 3 and § 3), equation (2.8) for the vapour gap thickness then rewrites to leading order as

(4.6) $$\begin{eqnarray}-\frac{1}{12\hat{r}}\unicode[STIX]{x2202}_{{\hat{s}}}\left(\hat{r}\hat{t}^{3}\unicode[STIX]{x2202}_{{\hat{s}}}\hat{P}_{v}\right)=\frac{\tilde{{\mathcal{E}}}}{\hat{t}},\end{eqnarray}$$

where the pressure in the vapour gap $\hat{P}_{v}({\hat{s}})$ and the geometric characteristics $\hat{r}({\hat{s}})$ are a priori given functions, known from the associated superhydrophobic drop consideration (cf. appendix B). The solution to (4.6), non-singular at the symmetry axis ${\hat{s}}=0$ , can be written as

(4.7) $$\begin{eqnarray}\hat{t}^{4}=\frac{16\tilde{{\mathcal{E}}}\displaystyle \int _{0}^{{\hat{s}}}\hat{r}^{4/3}(-\hat{P}_{v}^{\prime })^{1/3}\,\text{d}{\hat{s}}}{(-\hat{r}\,\hat{P}_{v}^{\prime })^{4/3}},\end{eqnarray}$$

the prime denoting a derivative with respect to ${\hat{s}}$ . The thickness at the symmetry axis, $\hat{t}_{0}=\hat{t}(0)$ , and at the exit, $\hat{t}_{exit}=\hat{t}({\hat{s}}_{CL})$ , can then be inferred as

(4.8a,b ) $$\begin{eqnarray}\hat{t}_{0}=\left(-\frac{6\,\tilde{{\mathcal{E}}}}{\hat{P}_{v}^{\prime \prime }(0)}\right)^{1/4},\quad \hat{t}_{exit}=\frac{2\,\tilde{{\mathcal{E}}}^{1/4}\left(\displaystyle \int _{0}^{{\hat{s}}_{CL}}\hat{r}^{4/3}(-\hat{P}_{v}^{\prime })^{1/3}\,\text{d}{\hat{s}}\right)^{1/4}}{[-\hat{r}({\hat{s}}_{CL})\hat{P}_{v}^{\prime }({\hat{s}}_{CL})]^{1/3}},\end{eqnarray}$$

where ${\hat{s}}_{CL}$ is the value of the arc length at the contact line of the associated superhydrophobic drop (known a priori, cf. appendix B). We note that the consideration only makes sense provided that $\hat{P}_{v}^{\prime }<0$ for all $0<{\hat{s}}<{\hat{s}}_{CL}$ and $\hat{P}_{v}^{\prime \prime }(0)<0$ , which turns out to be indeed the case for a superhydrophobic drop. We also note that the results of § 3 with a hemispherical shape and of § 4.1 with a spherical cap shape are recovered from here with $\text{d}{\hat{s}}={\mathcal{R}}\,\text{d}\unicode[STIX]{x1D703}$ , $\hat{P}_{v}^{\prime }=-\text{sin}\,\unicode[STIX]{x1D703}$ , $\hat{r}={\mathcal{R}}\sin \unicode[STIX]{x1D703}$ and ${\hat{s}}_{CL}={\mathcal{R}}\,\unicode[STIX]{x1D703}_{CL}$ . Equations (4.7) and (4.8) confirm once again that the scaling in terms of ${\mathcal{E}}$ established in § 3 for the vapour gap thickness in this outer region 1, namely $\hat{t}=O(\tilde{{\mathcal{E}}}^{1/4})$ including $\hat{t}_{0}=O(\tilde{{\mathcal{E}}}^{1/4})$ and $\hat{t}_{exit}=O(\tilde{{\mathcal{E}}}^{1/4})$ , is indeed robust.

We next turn to the inner region (cf. figure 3), also referred to as the neck region, the consideration of which follows the same asymptotic scheme as § 3. We introduce a local Cartesian coordinate $x$ (and its dimensionless version $\hat{x}=x/\unicode[STIX]{x1D706}_{c}$ ) parallel to the slope at the contact line of the associated superhydrophobic drop and pointing away from the vapour film. In this local Cartesian system, the drop and pool surfaces are described by $\hat{d}(\hat{x})$ and $\hat{p}(\hat{x})$ , respectively, and $\hat{t}=\hat{d}-\hat{p}$ and $\text{d}\hat{x}\approx \text{d}{\hat{s}}$ . Similar to § 3, the vapour pressure $\hat{P}_{v}$ in the neck region (unlike the earlier considered outer region 1) is no longer given by the associated superhydrophobic drop but is rather coupled to the local vapour gap profile. Owing to the expected small size of the neck region, the leading-order contribution in $\unicode[STIX]{x2202}_{\hat{x}}\hat{P}_{v}$ will be due to the capillary (Laplace) pressure associated with the first curvature of the drop and pool surfaces, i.e.  $\hat{P}_{v}^{\prime }\approx -\hat{d}^{\prime \prime \prime }$ and $\hat{P}_{v}^{\prime }\approx \unicode[STIX]{x1D6E4}\hat{p}^{\prime \prime \prime }$ . The latter two expressions must be equal, hence $\hat{d}^{\prime \prime \prime }\approx -\unicode[STIX]{x1D6E4}\hat{p}^{\prime \prime \prime }$ . Using this fact, as well as $\hat{t}=\hat{d}-\hat{p}$ , we express $\hat{P}_{v}^{\prime }\approx -(\unicode[STIX]{x1D6E4}/(1+\unicode[STIX]{x1D6E4}))\hat{t}^{\prime \prime \prime }$ . Using this in (4.6) and recalling, on the one hand, that it is planar geometry that holds to leading order in the neck region, and on the other hand, that the local evaporation flux $\tilde{E}/\hat{t}$ is negligible relative to the flux from the remainder of the vapour gap passing through the neck region (cf. § 3.3), one obtains

(4.9) $$\begin{eqnarray}\frac{1}{12}\,\frac{\unicode[STIX]{x1D6E4}}{1+\unicode[STIX]{x1D6E4}}\unicode[STIX]{x2202}_{\hat{x}}\left(\hat{t}^{3}\unicode[STIX]{x2202}_{\hat{x}\hat{x}\hat{x}}\hat{t}\right)=0\,,\end{eqnarray}$$

where the prefactor is kept for later convenience.

As in § 3.3, we shall look for solutions of this equation subject to boundary conditions $\hat{t}^{\prime \prime }(-\infty )=0$ whilst $\hat{t}^{\prime \prime }(+\infty )=\hat{\unicode[STIX]{x1D705}}_{1h,CL}-\hat{\unicode[STIX]{x1D705}}_{1e,CL}$ , where $\hat{\unicode[STIX]{x1D705}}_{1h,CL}$ and $\hat{\unicode[STIX]{x1D705}}_{1e,CL}$ are the (known) first curvatures of the upper drop and pool surfaces at the contact line of the associated superhydrophobic drop (appendix B). Recall that in the particular case of large drops with the same liquid properties (cf. § 3.3), we have $\hat{\unicode[STIX]{x1D705}}_{1h,CL}=\sqrt{2}$ and $\hat{\unicode[STIX]{x1D705}}_{1e,CL}=-\sqrt{2}$ resulting from the puddle solution, and giving rise to $\hat{t}^{\prime \prime }(+\infty )=2\sqrt{2}$ in present terms.

To account for the flux coming from the interior of the vapour gap, against which the local flux $\tilde{E}/\hat{t}$ was neglected when writing (4.9), we integrate (4.9) from $\hat{x}=-\infty$ to a finite value of $\hat{x}$ . In doing so, we take into account that the quantity $(1/12)(\unicode[STIX]{x1D6E4}/(1+\unicode[STIX]{x1D6E4}))\hat{t}^{3}\unicode[STIX]{x2202}_{\hat{x}\hat{x}\hat{x}}\hat{t}|_{\hat{x}=-\infty }$ , which is actually the dimensionless volume flux per unit length at the entrance to the neck region, must match the corresponding flux from the outer region 1 (the contribution from the intermediate region being negligible to leading order similar to § 3). Thus, it must be equal to the dimensionless volume flux per unit length at the exit from the outer region 1:

(4.10) $$\begin{eqnarray}\frac{1}{\hat{r}({\hat{s}}_{CL})}\int _{0}^{{\hat{s}}_{CL}}\hat{r}\frac{\tilde{{\mathcal{E}}}}{\hat{t}}\,\text{d}{\hat{s}}=\frac{1}{12}\,\hat{t}_{exit}^{3}[-\hat{P}_{v}^{\prime }({\hat{s}}_{CL})],\end{eqnarray}$$

the latter equality being written on account of (4.6) integrated over the outer region 1. Here recall that $\hat{t}_{exit}$ is given by (4.8), while $\hat{r}({\hat{s}}_{CL})$ and $\hat{P}_{v}^{\prime }({\hat{s}}_{CL})$ are values known from the associated superhydrophobic drop consideration (appendix B). We thereby finally arrive at the following equation for the vapour gap thickness in the inner (neck) region:

(4.11) $$\begin{eqnarray}\hat{t}^{3}\hat{t}^{\prime \prime \prime }=\frac{1+\unicode[STIX]{x1D6E4}}{\unicode[STIX]{x1D6E4}}\hat{t}_{exit}^{3}[-\hat{P}_{v}^{\prime }({\hat{s}}_{CL})],\end{eqnarray}$$

which is a first integral of (4.9) accounting for the mentioned flux condition. A rescaling

(4.12a-d ) $$\begin{eqnarray}\hat{t}=A^{2/5}B^{-3/5}\,T,\quad \hat{x}=A^{1/5}B^{-4/5}\,\unicode[STIX]{x1D701},\quad A\equiv \frac{1+\unicode[STIX]{x1D6E4}}{\unicode[STIX]{x1D6E4}}\hat{t}_{exit}^{3}[-\hat{P}_{v}^{\prime }({\hat{s}}_{CL})],\quad B\equiv \frac{\hat{\unicode[STIX]{x1D705}}_{1h,CL}-\hat{\unicode[STIX]{x1D705}}_{1e,CL}}{\sqrt{2}}\end{eqnarray}$$

reduces equation (3.17) with the earlier mentioned boundary conditions to the problem $T^{3}T^{\prime \prime \prime }=1$ with $T^{\prime \prime }(-\infty )=0$ and $T^{\prime \prime }(+\infty )=\sqrt{2}$ already considered in § 3.3. In particular, for the minimum neck thickness, $T_{n}=1.147$ was obtained, which here yields

(4.13) $$\begin{eqnarray}\hat{t}_{n}=1.147\,\left(\frac{1+\unicode[STIX]{x1D6E4}}{\unicode[STIX]{x1D6E4}}\hat{t}_{exit}^{3}[-\hat{P}_{v}^{\prime }({\hat{s}}_{CL})]\right)^{2/5}\left(\frac{\hat{\unicode[STIX]{x1D705}}_{1h,CL}-\hat{\unicode[STIX]{x1D705}}_{1e,CL}}{\sqrt{2}}\right)^{-3/5}.\end{eqnarray}$$

As $\hat{t}_{exit}=O(\tilde{{\mathcal{E}}}^{1/4})$ in accordance with (4.8), whereas the other quantities in (4.13) are just $O(1)$ , we see that $\hat{t}_{n}=O(\tilde{{\mathcal{E}}}^{3/10})$ , which confirms the robustness of the earlier established scaling law for the neck thickness (cf. § 3).

With the $\tilde{{\mathcal{E}}}$ scaling (power) laws themselves confirmed, we recall that the prefactors at the asymptotic results such as (4.7), (4.8) and (4.13) depend exclusively on characteristics of the associated superhydrophobic drop. The latter are computed numerically as described in appendix B and subsequently used in (4.7), (4.8) and (4.13) to complete the present asymptotic consideration. The results are illustrated below together with their comparison with the full Leidenfrost numerics (the latter realised as described in appendix A).

Figure 10.

Global drop shapes (a,b) and vapour gap thicknesses (c distributions along the arc length of the pool surface; d values in the centre and at the neck as functions of $\tilde{{\mathcal{E}}}$ ). Results for ${\mathcal{R}}=3$ and the material properties resembling those for an ethanol drop on a silicone oil pool (Maquet et al. Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016). In particular, ${\mathcal{P}}=1.244$ and $\unicode[STIX]{x1D6E4}=1.156$ . The (a,b) are for $\tilde{{\mathcal{E}}}=4.8\times 10^{-9}$ ( $\unicode[STIX]{x0394}T=1~\text{K}$ ) and $\tilde{{\mathcal{E}}}=2.3\times 10^{-7}$ ( $\unicode[STIX]{x0394}T=40~\text{K}$ ), respectively. And so are the lower and upper curves in (c). The arc length ${\hat{s}}$ is along the pool surface in the full numerics, while along the superhydrophobic drop–pool interface in the outer region 1 asymptotics.

Figure 10 shows results for a drop of ${\mathcal{R}}=3$ with non-equal material properties inspired from Maquet et al. (Reference Maquet, Sobac, Darbois-Texier, Duchesne, Brandenbourger, Rednikov, Colinet and Dorbolo2016). We see that the global Leidenfrost drop and pool shapes are still close to those of the associated superhydrophobic drop, as expected. The morphological structure of the vapour gap is still the same as noted earlier in the case of equal material properties. The asymptotic results for the outer region 1 capture well the film thickness distribution in the central part, although at larger $\tilde{{\mathcal{E}}}$ the waviness from the intermediate region penetrates closer to the symmetry axis. For the thickness values in the centre and at the neck, we once again obtain a good agreement between the asymptotic and the full numerical approaches, although the agreement slightly deteriorates at larger $\tilde{{\mathcal{E}}}$ (especially for $\hat{t}_{n}$ ). Importantly, the asymptotic scalings $\hat{t}_{0}\sim \tilde{{\mathcal{E}}}^{1/4}$ and $\hat{t}_{n}\sim \tilde{{\mathcal{E}}}^{3/10}$ are seen to still be well reproduced by the full numerics. We note that the straight lines in figure 10(d) are the asymptotic predictions with no fitting involved: the prefactors were determined directly from the associated superhydrophobic drop analysis.

Figure 11.

Extension of the part of the results of figure 10 pertaining to $\tilde{{\mathcal{E}}}=2.3\times 10^{-7}$ (still with ${\mathcal{P}}=1.244$ , $\unicode[STIX]{x1D6E4}=1.156$ ) to a number of drop radii, ${\mathcal{R}}=1.5,2,3,10$ . In (b), the correspondence between each curve and the ${\mathcal{R}}$ value can reasonably be guessed from the right ending of the former.

Figure 12.

Extension of the results of figure 9 to a number of pool-to-drop density ratios ${\mathcal{P}}=0.8,\,2,\,40$ (otherwise still for ${\mathcal{R}}=3$ , $\unicode[STIX]{x1D6E4}=1$ and $\tilde{{\mathcal{E}}}=4.8\times 10^{-9}$ , which corresponds to ${\mathcal{E}}=8.64\times 10^{-8}$ ). As ${\mathcal{P}}$ is increased, the drop mounts in (a), while the curves in (b) get shorter from the right (the overall arc length of the vapour gap decreases).

Some of the cases shown in figures 9 and 10 are taken up for a further parametric study in figures 11 and 12, partly aimed at testing the limits of the applicability of the present asymptotic scheme. In particular, the results of figure 10 corresponding to the larger evaporation number value ( $\tilde{{\mathcal{E}}}=2.3\times 10^{-7}$ ) are extended in figure 11 to some other drop radius values. While the Leidenfrost drops are seen to still be close to the superhydrophobic shapes in all cases shown, the present asymptotic results cease to be valid for smaller drops as far as the outer region 1 and $\hat{t}_{0}$ are concerned. This is especially true for the smallest drop displayed, with ${\mathcal{R}}=1.5$ . It can clearly be observed from figure 11(b) that such a change in the vapour gap morphology is related first of all with the violation of the part $\hat{l}_{n}\ll {\mathcal{R}}$ of the presumed hierarchy of length scales (4.1). This violation occurs for larger $\tilde{{\mathcal{E}}}$ as ${\mathcal{R}}$ is decreased, when the wavelength of the intermediate region undulations becomes comparable with the size of the drop, as already discussed at the end of § 4.1. At smaller $\tilde{{\mathcal{E}}}$ however (e.g. at $\tilde{{\mathcal{E}}}=4.8\times 10^{-9}$ used earlier in figure 10), the present asymptotic scheme is still found to work rather satisfactorily in the central part of the drop even for ${\mathcal{R}}$ as low as ${\mathcal{R}}=1.5$ (the result not shown).

A no less remarkable result of figure 11 is some deterioration of the agreement between asymptotics and full numerics observed for large ${\mathcal{R}}$ (viz.  ${\mathcal{R}}=10$ ) as compared to ${\mathcal{R}}=3$ as far as the gap thickness in the centre (i.e.  $\hat{t}_{0}$ ) is concerned. There is a good reason for that. Indeed, it is clear that, quite unlike a superhydrophobic drop over a pool with equal liquid properties, a drop of a differing liquid will tend to adopt a puddle-like shape as ${\mathcal{R}}$ is increased (here limiting consideration to the case ${\mathcal{P}}>1$ , of a lighter drop; a heavier one will merely sink for sufficiently large ${\mathcal{R}}$ ). For such a puddle, which the drop with ${\mathcal{R}}=10$ of figure 11 already much resembles, it is not only the upper surface that flattens, but also the immersed one. The present asymptotic scheme breaks down in the presence of a flattened part of the immersed surface, for which the $\hat{P}_{v}^{\prime }$ and $\hat{P}_{v}^{\prime \prime }$ values to be used in (4.7) and (4.8) vanish and the driving force of the flow $\hat{P}_{v}^{\prime }$ is no longer accurately estimated by the superhydrophobic drop. The length scale at which such flattening occurs is the (dimensionless) capillary length of the immersed surface $\sqrt{(1+\unicode[STIX]{x1D6E4})/({\mathcal{P}}-1)}$ . Hence the present asymptotic scheme is expected to work in an optimal way when ${\mathcal{R}}\lesssim \sqrt{(1+\unicode[STIX]{x1D6E4})/({\mathcal{P}}-1)}$ , i.e. for sufficiently small drops. The drop with ${\mathcal{R}}=10$ of figure 11 is already relatively large in this regard, hence the mentioned agreement deterioration. Note that this concerns a relatively larger value $\tilde{{\mathcal{E}}}=2.3\times 10^{-7}$ . For a smaller value $\tilde{{\mathcal{E}}}=4.8\times 10^{-9}$ , the agreement still proves to be excellent even for ${\mathcal{R}}=10$ (the result not shown). Note also that for a system with ${\mathcal{P}}=1$ , the capillary length of the immersed surface goes to infinity (the surface itself assuming the form of a spherical cap), and hence such a limitation on the maximum drop radius is lifted.

In figure 12, we take up the case of figure 9 (with ${\mathcal{R}}=3$ , $\unicode[STIX]{x1D6E4}=1$ and $\tilde{{\mathcal{E}}}=4.8\times 10^{-9}$ ) and explore how the phenomenon is affected by the variation of the density ratio ${\mathcal{P}}$ . We see that, as long as the pool surface deformation remains appreciable (e.g. for ${\mathcal{P}}=0.8,\,2$ ), the expected morphological features remain in place. In particular, this is still the case at ${\mathcal{P}}=0.8$ , for nearly the maximum possible immersed-surface deformation: we are then on the verge of the disappearance of a floating drop configuration for ${\mathcal{P}}$ slightly below ${\mathcal{P}}=0.8$ , when a drop with ${\mathcal{R}}=3$ and $\unicode[STIX]{x1D6E4}=1$ becomes too heavy to remain on the pool surface. The fact that such disappearance happens practically simultaneously (in terms of ${\mathcal{P}}$ ) for the Leidenfrost and superhydrophobic drops can serve as yet another confirmation of a close relationship between these two configurations. On the other hand, while perhaps not physically relevant, the interest of the case ${\mathcal{P}}=40$ is that the pool surface becomes essentially flat: hence we should thereby approach the case of a Leidenfrost drop above a (flat) solid. Indeed, the vapour film profile for ${\mathcal{P}}=40$ is seen (cf. figure 12 b) to more closely resemble that typical for a flat solid substrate (Snoeijer et al. Reference Snoeijer, Ziegler, Andreotti, Fermigier and Eggers2008; Burton et al. Reference Burton, Sharpe, van der Veen, Franco and Nagel2012; Sobac et al. Reference Sobac, Rednikov, Dorbolo and Colinet2014), with the present asymptotic scheme yielding an appreciable error with respect to the full numerics. The reason for such an error can be traced back to the fact that, under the conditions when the vapour gap thickness becomes comparable to (or even larger than) the deviation of the immersed surface from the horizontal, the pressure distribution $\hat{P}_{v}({\hat{s}})$ can no longer be taken as $\hat{t}$ -independent as assumed from the superhydrophobic drop considerations. There must rather be a feedback between $\hat{P}_{v}({\hat{s}})$ and  $\hat{t}({\hat{s}})$ such as that which exists in the case of a flat solid substrate (Snoeijer et al. Reference Snoeijer, Ziegler, Andreotti, Fermigier and Eggers2008; Sobac et al. Reference Sobac, Rednikov, Dorbolo and Colinet2014). Note also that a similar observation can actually be attributed to the flattened parts (if any) of the immersed surface even if the latter is not flattened overall (cf. the above discussion of the drop with ${\mathcal{R}}=10$ of figure 11). Finally, an increase of the pool-to-drop surface tension ratio $\unicode[STIX]{x1D6E4}$ will lead to similar effects of pool surface flattening as those due to an increase of ${\mathcal{P}}$ .

Thus, for differing liquids too, the scalings $\hat{t}_{0}\sim \tilde{{\mathcal{E}}}^{1/4}$ and $\hat{t}_{n}\sim \tilde{{\mathcal{E}}}^{3/10}$ are still robust and work in a reasonable interval of small $\tilde{{\mathcal{E}}}$ values for sufficiently large drops ( ${\mathcal{R}}\gg \hat{l}_{n}$ ) in the general case of significantly curved pool surfaces. However, the particular cases when the immersed superhydrophobic drop surface undergoes a strong overall (for too large ${\mathcal{P}}$ and/or $\unicode[STIX]{x1D6E4}$ ) or partial (for too large ${\mathcal{R}}$ ) flattening must realistically be excluded from the applicability domain of the present asymptotic scheme. Indeed, such applicability would then just be expected for extremely small values of $\tilde{{\mathcal{E}}}$ , which are of no practical interest. In contrast, the pure scaling in terms of ${\mathcal{R}}$ underscored in § 4.1 makes actually no sense here (for differing liquids) due to a morphological difference between the superhydrophobic drop shapes in the limit of large ${\mathcal{R}}$ : a hemisphere for equal liquid properties, and a puddle for differing ones (assuming a lighter drop, ${\mathcal{P}}>1$ ) with further adverse consequences due to the mentioned partial flattening of the immersed surface.