2.1. VOF formulation

Since fluids are assumed to be immiscible, the advection of the material interface is carried out by means of an algebraic VOF method. The numerical scheme for the advection is based on a novel Courant–Friedrichs–Lewy-dependent flux limiter whereby the classical total-variation-diminishing (TVD) bounds are exceeded, thus enabling efficient and improved representation of binary functions (Pirozzoli, Di Giorgio & Iafrati Reference Pirozzoli, Di Giorgio and Iafrati2019). The method yields perfectly crisp interfaces with very limited numerical atomization (flotsam and jetsam). Let $\chi$ be a passive tracer advected by a continuous divergence-free velocity field $\boldsymbol {u}$, which satisfies the passive transport equation

(2.18)\begin{equation} \frac{\partial \chi}{\partial t} + \boldsymbol{\nabla}\boldsymbol{\cdot} (\chi {\boldsymbol{u}}) = 0. \end{equation}

For the problem under scrutiny here, $\chi$ is either $1$ or $0$, which is the case of two immiscible fluids. In the VOF method, a colour function is introduced to approximate the cell average of $\chi$, which in the illustrative case of one space dimension is defined as

(2.19)\begin{equation} C_i = \frac 1{\Delta x_i} \int_{x_{i-1/2}}^{x_{i+1/2}} \chi (x,t^n)\, \mathrm{d} x , \end{equation}

where $\Delta x_i = x_{i+1/2}-x_{i-1/2}$ is the cell size. Equation (2.18) is then discretized in time yielding

(2.20)\begin{equation} C_i^{n+1/2} = C_i^{n- 1/2} - \frac{1}{\Delta x_i} \left( \hat{f}_{i+1/2} - \hat{f}_{i-1/2} \right) , \end{equation}

where the numerical flux $\hat {f}_{i+1/2}$ is an approximation for the amount of $\chi$ transported through the cell interface $x_{i+1/2}$ during the time interval $(t^{n-1/2}, t^{n+1/2})$. This is determined by assuming piecewise linear reconstruction within each cell, namely

(2.21)\begin{equation} C_{i}(x) = C^n_{i} + s_{i} (x-x_{i}), \end{equation}

with slope $s_i$ selected so as to prevent the occurrence of overshoots/undershoots by enforcing the TVD constraints (Sweby Reference Sweby1984)

(2.22)\begin{equation} s_i = \frac{1}{\Delta x_{i}}\,\varphi(\theta_{i+1/2})\,\delta C_{i+1/2} , \end{equation}

where $\delta C_{i+1/2} = C_{i+1}-C_i$, $\theta _{i+1/2}=\delta C_{i-1/2}/\delta C_{i+1/2}$. Suitable choice of the slope limiter function $\varphi$ is found to provide crisp resolution of contact discontinuities (with 2–3 grid points), and absence of spurious flotsam–jetsam as in early implementations of the TVD idea (Noh & Woodward Reference Noh and Woodward1976; Hirt & Nichols Reference Hirt and Nichols1981). Details of the algorithm are provided in the original reference, Pirozzoli et al. (Reference Pirozzoli, Di Giorgio and Iafrati2019). After computing the colour function $C$, density and viscosity are determined from

(2.23a,b)\begin{equation} \rho = \tilde{C} + \frac{\rho_2}{\rho_1} \left( 1 - \tilde{C} \right), \quad \mu = \tilde{C} + \frac{\mu_2}{\mu_1} \left( 1 - \tilde{C} \right) , \end{equation}

where $\tilde {C}$ is a smoothed version of the colour function, evaluated by averaging $C$ over 27 neighbouring cells (Popinet Reference Popinet2009; Tryggvason et al. Reference Tryggvason, Scardovelli and Zaleski2011).

2.2. Spatial discretization

The momentum equations are discretized in the finite-difference framework with a staggered grid layout, where the pressure, the colour function and the material properties are defined at the cell centres, whereas the velocity components are stored at the middle of the cell faces (Harlow & Welch Reference Harlow and Welch1965). The right-hand side of (2.13) is rewritten in order to cast convective and diffusive terms in a more canonical form:

(2.24)\begin{align} {\rm RHS} & ={-}\left( \frac{3}{2}\, \boldsymbol{H}^n_h-\frac{1}{2}\,\boldsymbol{H}^{n-1}_h \right) + \frac{1}{\rho^{n+{1}/{2}}\,{\textit{Re}} } \left[ \boldsymbol{\varSigma}_h^n + \frac{1}{2} \left( \boldsymbol{\nabla}_h \boldsymbol{u}^{{\rm T},n} - \boldsymbol{\nabla}_h \boldsymbol{u}^{{\rm T},n-1} \right) \boldsymbol{\nabla}_h \mu^{n+{1}/{2}} \right] \nonumber\\ &\quad + \frac{1}{ \rho^{n+{1}/{2}}\,{\textit{We}}}\,\boldsymbol{f}_{\sigma}^n - \frac{1}{ \rho^{n+{1}/{2}}\,{\textit{Fr}}}\,\boldsymbol{j} , \end{align}

where $\boldsymbol {H}_h$ and $\boldsymbol {\varSigma }_h$ denote, respectively, convective and viscous terms. Terms associated with variation of viscosity appear in this case, which are rearranged as

(2.25)\begin{align} &\frac{1}{\rho^{n+{1}/{2}}\,{\textit{Re}}} \left[ \frac{3}{2}\, \boldsymbol{\nabla}_h \boldsymbol{\cdot} \left( \mu^{n+{1}/{2}}\,\boldsymbol{\nabla} {\boldsymbol{u}}^{{\rm T},n} \right) - \frac{1}{2}\,\boldsymbol{\nabla}_h \left( \mu^{n+{1}/{2}}\,\boldsymbol{\nabla} {\boldsymbol{u}}^{{\rm T},n-1} \right) \right] \nonumber\\ &\quad = \frac{1}{\rho^{n+{1}/{2}}\,{\textit{Re}}} \left[ \boldsymbol{\nabla}_h \boldsymbol{\cdot} \left( \mu^{n+{1}/{2}}\,\boldsymbol{\nabla}{\boldsymbol{u}}^{{\rm T},n} \right) + \frac{1}{2} \left( \boldsymbol{\nabla}_h \boldsymbol{\cdot} \left( \mu^{n+{1}/{2}}\,\boldsymbol{\nabla} {\boldsymbol{u}}^{{\rm T},n} \right) - \boldsymbol{\nabla}_h \boldsymbol{\cdot} \left(\mu^{n+{1}/{2}}\,\boldsymbol{\nabla} {\boldsymbol{u}}^{{\rm T},n-1}\right)\right)\right] , \end{align}

and exploiting incompressibility, one has

(2.26)\begin{align} \boldsymbol{\nabla}_h \boldsymbol{\cdot} \left( \mu^{n+{1}/{2}}\,\boldsymbol{\nabla} {\boldsymbol{u}}^{{\rm T},n} \right) &= \boldsymbol{\nabla}_h \boldsymbol{u}^{{\rm T},n}\,\boldsymbol{\nabla}_h \mu^{n+{1}/{2}} + \mu^{n+{1}/{2}}\,\boldsymbol{\nabla}_h \boldsymbol{\cdot} \boldsymbol{\nabla}_h {\boldsymbol{u}}^{{\rm T},n} \nonumber\\ &= \boldsymbol{\nabla}_h {\boldsymbol{u}}^{{\rm T},n}\,\boldsymbol{\nabla}_h \mu^{n+{1}/{2}} + \mu^{n+{1}/{2}}\,\boldsymbol{\nabla}_h \left( \boldsymbol{\nabla}_h \boldsymbol{\cdot} {\boldsymbol{u}} \right) \nonumber\\ &= \boldsymbol{\nabla}_h {\boldsymbol{u}}^{{\rm T},n}\,\boldsymbol{\nabla}_h \mu^{n+{1}/{2}} . \end{align}

For the convective terms, defined as

(2.27a,b)\begin{equation} \boldsymbol{H}^n_h = \boldsymbol{\nabla}_h \boldsymbol{\cdot} ( \boldsymbol{u}^n \boldsymbol{u}^n ) , \quad \boldsymbol{H}^{n-1}_h = \boldsymbol{\nabla}_h \boldsymbol{\cdot} ( \boldsymbol{u}^{n-1} \boldsymbol{u}^{n-1} ) , \end{equation}

a centred second-order discretization is used (e.g. Harlow & Welch Reference Harlow and Welch1965; Orlandi Reference Orlandi2012), which is generally best suitable for fully resolved flows, yielding discrete preservation of the total kinetic energy in the case of uniform density. For the diffusive terms, which are written as

(2.28)\begin{equation} \boldsymbol{\varSigma}_h^n = \boldsymbol{\nabla}_h \boldsymbol{\cdot} \mu^{n+{1}/{2}} \left( \boldsymbol{\nabla}_h \boldsymbol{u}^{n} + \boldsymbol{\nabla}_h \boldsymbol{u}^{{\rm T},n} \right), \end{equation}

a standard second-order central discretization is used (Tryggvason et al. Reference Tryggvason, Scardovelli and Zaleski2011).

The last step concerns the solution of the Poisson equation (2.9) for the corrective pressure, which is also the most expensive part in multiphase flow solvers in terms of computational effort. The Poisson equation is discretized by a finite-difference scheme with a staggered Cartesian mesh. The resulting sparse linear system is solved by iterative methods. In particular, the HYPRE library (Falgout & Yang Reference Falgout and Yang2002) is found to be very efficient in massively parallel computations. Both geometric multigrids and the Krylov methods have been tested, the latter proving to be more robust in the presence of complicated flow topologies.

2.3. Surface tension

The modelling of surface tension effects is the most peculiar and critical aspect when developing a multiphase flow solver. Use of the VOF method, which has advantages in terms of mass conservation, has some drawbacks when the curvature on the interface has to be estimated, which is necessary for the determination of surface tension. In this work, the continuum surface force method (Brackbill, Kothe & Zemach Reference Brackbill, Kothe and Zemach1992) is used to determine the equivalent local body force, whereas the interface curvature is evaluated through the height function technique (Cummins, Francois & Kothe Reference Cummins, Francois and Kothe2005; Francois et al. Reference Francois, Cummins, Dendy, Kothe, Sicilian and Williams2006; Hernández et al. Reference Hernández, López, Gómez, Zanzi and Faura2008; López & Hernández Reference López and Hernández2010; Popinet Reference Popinet2009; Aniszewski et al. Reference Aniszewski2021)). The height function method is known to work well as long as the height function is within the cell dimension (Cummins et al. Reference Cummins, Francois and Kothe2005). At points where this condition is not met, the interface curvature is estimated based on the gradient of the interface normal vector (Goldman Reference Goldman2005):

(2.29)\begin{equation} k = \frac{\boldsymbol{\nabla} \tilde{C} \ast H ( \tilde{C} ) \ast \boldsymbol{\nabla} \tilde{C}^{\rm T} - | \boldsymbol{\nabla} \tilde{C} |^2 \,{\rm Tr}\bigl(H ( \tilde{C} ) \bigr)} {2 | \boldsymbol{\nabla} \tilde{C} |^3 }, \end{equation}

where $\boldsymbol {\nabla } \tilde {C}$ and $H( \tilde {C} )$ are, respectively, the gradient and the Hessian of the smoothed colour function. The first- and second-order derivatives of the colour function field (${\partial \tilde {C}}/{\partial x_i}$ and ${\partial ^2 \tilde {C}}/{\partial x_i\, \partial x_j }$) are approximated using the least-squares method (Ding et al. Reference Ding, Shu, Yeo and Xu2004). A detailed verification and validation study of the solver is reported in Appendix A.

3.1. Flow cases

Results of numerical simulations of wave breaking are hereafter reported for the idealized case of a wave train with assumed periodicity in the streamwise and spanwise directions (see figure 2). The initial free-surface elevation $\eta (x,z)$ is assigned as in Iafrati (Reference Iafrati2009), Chen et al. (Reference Chen, Kharif, Zaleski and Li1999), Deike et al. (Reference Deike, Popinet and Melville2015, Reference Deike, Melville and Popinet2016) and Wang et al. (Reference Wang, Yang and Stern2016), that is,

(3.1)\begin{equation} \eta (x,z) = \frac{\epsilon}{2 {\rm \pi}} \left( \cos ( k \left(x - r(z)\,\Delta x \right) ) + \frac{1}{2} \epsilon \cos ( 2 k \left(x - r(z)\,\Delta x \right) ) + \frac{3}{8} \epsilon^2 \cos ( 3 k \left(x - r(z)\,\Delta x \right) ) \right), \end{equation}

where $\epsilon = a k$ is the initial wave steepness, $a$ is the wave amplitude, $k = 2 {\rm \pi}$ is the fundamental wavenumber, and the period of the fundamental wave component is $T = \sqrt {2 {\rm \pi}} \approx 2.5$. A small perturbation is introduced in the initial wave profile in the form of a random shift by a fraction ($0 \leqslant r(z) \leqslant 1$) of the grid cell size. The corresponding initial velocity field in water is derived from potential flow theory:

(3.2)$$\begin{gather} u(x,y,z) = \varOmega\,\frac{\epsilon}{k} \exp ( k y ) \cos ( k \left(x - r(z)\,\Delta x \right) ), \quad \forall \, y < \eta(x,z), \end{gather}$$

(3.3)$$\begin{gather}v(x,y,z)= \varOmega\,\frac{\epsilon}{k} \exp ( k y ) \sin ( k \left(x - r(z)\, \Delta x \right) ), \quad \forall \, y < \eta(x,z), \end{gather}$$

where $\varOmega = \sqrt {k / {\textit {Fr}}\,( 1 + \epsilon ^2 ) }$ accounts for nonlinear corrections (Whitham Reference Whitham1974). No-slip boundary conditions are assigned at the top and bottom boundaries. At the beginning of the simulation, the fluid in the air domain, i.e. $y > \eta (x,z)$, is assumed to be at rest. As soon as the simulation starts, the solution of the Poisson equation enforces the continuity of the velocity field, therefore the velocity in air is initialized as a divergence-free velocity field satisfying the continuity of the normal velocity at the interface. Later on, motion in air is induced by momentum exchange occurring at the interface due to the normal and tangential stresses. As the water depth is of the same order as the fundamental wavelength, wave propagation can be regarded to be of deep-water type, and the presence of the bottom does not affect the evolution of the breaking process substantially (Chen et al. Reference Chen, Kharif, Zaleski and Li1999). For similar reasons, at such a wavelength/depth ratio, the energy loss by bottom friction is essentially negligible (Lighthill Reference Lighthill1978). Two- and three-dimensional numerical simulations have been carried out for different Reynolds numbers, but in all cases it is assumed that

(3.4)\begin{equation} {\textit{We}} = \frac{\rho_1 \tilde{U}^2 \lambda}{\sigma} = \frac{\rho_1 g \lambda^2}{\sigma} = 12\,262.5 . \end{equation}

Assuming the surface tension coefficient to be $0.072\ \textrm {N}\ \textrm {m}^{-1}$, the chosen Weber number corresponds to water waves with about $30$ cm fundamental wavelength. At such a wavelength, the Reynolds number is

(3.5)\begin{equation} {\textit{Re}} = \frac{\rho_1 \tilde{U} \lambda}{\mu_1}= \frac{\rho_1 g^{1/2} \lambda^{3/2}}{\mu_1} \approx 5.1 \times 10^5 . \end{equation}

Numerical simulations at such a Reynolds number would require a considerable computational effort for all the relevant scales of the flow to be fully resolved. In order to minimize artefacts due to lack of sufficient resolution, simulations have been conducted at $ {\textit {Re}}=10\,000$ and $40\,000$. Despite this limitation, viscous effects may be regarded as representative of full-scale conditions, while providing accurate and energy-preserving solutions. In all cases, the density and viscosity ratios are assumed to be $\rho _1/\rho _2 = 800$ and $\mu _1/\mu _2 = 55$, hence representative of the real air–water system. The flow parameters for the various simulations performed are listed in table 1. The computational domain is one fundamental wavelength long (streamwise direction), two fundamental wavelengths high (vertical direction), and for 3-D simulations, one-half fundamental wavelength wide (spanwise direction), namely $x \in [-0.5 , 0.5 ]$, $y \in [-1, 1 ]$, $z \in [-0.25 , 0.25 ]$. Each 3-D simulation has been carried out at two grid resolutions, in order to gain information about grid sensitivity. In all cases, the grid cells are uniformly spaced in the $x$- and $z$-directions, whereas in the vertical direction, cells are clustered about the still-water level in order to achieve better resolution around the interface. In particular, the grid size is kept uniform for $-0.25 \leqslant y \leqslant 0.25$, and progressively increased moving away from the centre of the domain (Orlandi Reference Orlandi2012, § 2.2.3c). Assuming $\lambda =30$ cm, the resulting grid spacing in the well-resolved zone is about $0.6$ mm in the coarse-mesh simulations (as in Chen et al. Reference Chen, Kharif, Zaleski and Li1999), and $0.3$ mm in the fine-mesh simulations.

Figure 2.

Sketch of the computational set-up for the study of wave breaking: no-slip boundary conditions are assigned at the top and bottom boundaries, whereas periodic boundary conditions are assigned in the streamwise ($x$) and spanwise ($z$) directions.

Table 1.

List of simulations performed. For all cases, $ {\textit {We}} = 12\,262.5$. Columns show the simulation identifier, the number of cells used, the domain size in the streamwise, vertical and spanwise directions, the initial steepness parameter, and the Reynolds number of the liquid phase.

Particularly at the shortest scales, the dynamics of the breaking is strongly affected by surface tension (Duncan Reference Duncan2001). An illustration of the various stages of the breaking process is provided in figure 3, where kinetic energy and instantaneous streamtraces are shown. Starting from the initial conditions (figure 3a), the onset of the breaking occurs at the time instant at which for the first time a portion of the air–water interface becomes vertical (figure 3b). Next, curling of the crest and plunging onto the forward face are displayed in figure 3(c), which shows the impact of the water jet and subsequent air entrainment. Finally, figure 3(d) shows the splash-up and successive impacts on the free surface, and resulting air entrainment (Kiger & Duncan Reference Kiger and Duncan2012). The simulations are advanced in time up to $t/T=2.8$, at which time most energy has been dissipated, and effects of spurious streamwise periodicity are still small.

Figure 3.

Air entrainment in a plunging breaker: slices of the 3D1E4c flow case are reported, showing contours of kinetic energy, and instantaneous streamtraces: (a) initial condition, $t/T = 0.0$; (b) breaking inception, $t/T = 0.26$; (c) initial jet impact, $t/T = 0.38$; (d) backward-splash entrainment, $t/T = 0.84$.

3.2. Influence of initial conditions and grid size

In order to derive a quantitative estimate of the uncertainty in the numerical results, for the 2-D case, five repetitions of the same simulation have been carried out by imparting small random perturbations of the initial wave profile (3.1). This is to mimic what usually happens in experiments where, due to the residual turbulence level and/or small perturbations in the initial free-surface profile, differences in the breaking dynamics occur, although the main features are quite repeatable. In figure 4, the time histories of the total mechanical energy for the various simulations are reported. Up to onset of breaking, the results are perfectly overlapping. However, when breaking initiates, minor changes in the air entrainment and in the bubble fragmentation process caused by the different initial shifts lead to progressive divergence in the behaviour of the total energy. At the end of the simulation, the maximum scatter across cases is about $10-15\,\%$ of the initial energy content. This issue should be kept in mind when comparing different simulations. The results of 2-D simulations with initially perturbed state are then used to extract an ensemble average of the volume fraction and associated density and viscosity fields. For that purpose, an intermittency coefficient (Brocchini & Peregrine Reference Brocchini and Peregrine2001)

(3.6)\begin{equation} \bar{C}( \boldsymbol{x},t ) = \frac{ \sum^N_i C_i ( \boldsymbol{x}, t ) }{ N } \end{equation}

is determined as an average of the local volume fraction over $N= 5$ simulations with different initial conditions, as shown in figure 5. The time evolution confirms that all computed solutions are well overlapping up to the breaking onset, also in terms of the free-surface profile. As soon as the water jet plunges onto the free surface, larger differences emerge in the size and distributions of the entrapped bubbles, thus leading to much wider scatter. Differences are originated by strong nonlinearities in the flow triggered by changes associated with use of a discrete grid to describe the fragmentation and reconnection processes of the interface. At a later stage, the large air cavity that forms breaks down into smaller cavities that subsequently rise up and emerge from the water, thus the intermittency region shrinks, while remaining larger than the grid cell.

Figure 4.

Time histories of total energy for 2-D simulations with initial steepness $\epsilon = 0.5$, with different initial perturbations.

Figure 5.

Contours of ensemble-averaged volume fraction of 2-D simulations with perturbed initial conditions at different times, (a) $t/T = 0.4$, (b) $t/T = 0.8$, (c) $t/T = 1.2$, (d) $t/T = 1.6$, (e) $t/T = 2.0$, and (f) $t/T = 2.4$.

The effect of the grid resolution is analysed in the 3-D flow cases. In order to test the capability of the computational model to resolve all the relevant scales responsible for energy dissipation, a comparison between the time history of the total energy ($E_{tot}$) obtained from the simulations on coarse and fine meshes is displayed in figure 6. The total energy is here defined as

(3.7)\begin{align} E_{tot} = \underbrace{ \int_{V} \frac{1}{2}\,\rho ( u^2 + v^2 +w ^2 )\,\mathrm{d} V }_{\text{kinetic energy}} + \underbrace{\int_{V} \rho\,g (y + d/2) \,\mathrm{d} V }_{\text{potential energy}} + \underbrace{\frac{1} {We}\, ( \mathcal{S} -1 ) }_{\text{surface tension potential energy}} , \end{align}

where the first term on the right-hand side is the total kinetic energy, the second term is the potential energy, with $d$ the water depth, and the last term is the surface tension potential energy, with $\mathcal {S}$ the surface area of the interface. No significant difference is observed between coarse and fine simulations during the pre-breaking phase. Once the breaking starts, small differences develop, which, nevertheless, are within the inherent uncertainty of the simulations as discussed previously in the 2-D case.

Figure 6.

Evolution of total energy as obtained from 3-D simulations of wave breaking with $\epsilon = 0.5$. Results are shown for (a) $ {\textit {Re}}=10\,000$, and (b) $ {\textit {Re}}=40\,000$.

3.3. Energy budgets

Starting from the momentum and continuity equations, the following integral budget equation can be derived:

(3.8)\begin{align} \frac{{\rm d}}{{\rm d}t} \underbrace{ \int_V \left(\rho\,\frac{u^2}{2} + \rho g y\right) \mathrm{d} V}_{\text{total energy}} &={-} \underbrace{ \oint_{\partial V} \left( p + \rho\,\frac{u^2}{2} + \rho g y \right) \boldsymbol{u} \boldsymbol{\cdot} \boldsymbol{n} \, \mathrm{d} S }_{\text{boundary energy flux}} + \underbrace{ \oint_{\partial V} \left( \varSigma \boldsymbol{\cdot} \boldsymbol{u} \right) \boldsymbol{\cdot} \boldsymbol{n} \, \mathrm{d} S }_{\text{work of surface tension forces}} \nonumber\\ &\quad - \underbrace{ \int_V \boldsymbol{\varSigma} : \boldsymbol{\nabla} \boldsymbol{u} \, \mathrm{d} V }_{ \text{viscous dissipation} } + \underbrace{ \int_V \boldsymbol{u} \boldsymbol{\cdot} \boldsymbol{f}_{\sigma} \, \mathrm{d} V }_{\text{ work of tension forces} }, \end{align}

where surface integrals over the domain boundaries vanish due to the periodicity in the streamwise and spanwise directions, and to the no-slip boundary condition at the bottom and top walls. It is important to note that the above equations apply in continuous form, but they are not valid rigorously in discrete form, depending on the numerical scheme and grid size. The discretization scheme adopted in the present model for the momentum equation conserves the total energy also in discrete form in the case of a single fluid (Orlandi Reference Orlandi2012). However, the conservation properties are not guaranteed in case of multiphase flows due to the variation of the fluid properties, and of the density in particular. In figure 7, the time histories of the total mechanical energy for the various simulations are compared with the time integrals of the sum of the viscous dissipation and surface tension work terms. The results highlight satisfactory agreement between the energy decay and the total dissipation, which, as expected, improves for the case of fine grid computations. Differences are minor prior to breaking, and become more significant once breaking starts. After the start of the breaking occurring at about $t/T \approx 0.5$, the air–water interface increases in size owing to air entrainment and bubble fragmentation, but in spite of that, the energy conservation properties of the discrete form of the convective terms and of the approximate representation of the surface tension are confirmed.

Figure 7.

Time histories of total mechanical energy (purple line with solid square symbols) and of the time integral of the sum of viscous dissipation and surface tension work (green line with open circles) for 3-D simulations of wave breaking with initial steepness $\epsilon = 0.5$: (a) $ {\textit {Re}}=10\,000$, coarse grid (3D1E4c); (b) $ {\textit {Re}}=10\,000$, fine grid (3D1E4f); (c) $ {\textit {Re}}=40\,000$, coarse grid (3D4E4c); (d) $ {\textit {Re}}=40\,000$, fine grid (3D4E4f).

3.4. Role of breaking in energy dissipation

The time histories of kinetic, potential, surface tension and total energies during the breaking process are shown in figure 8 for $ {\textit {Re}}=10\,000$ and $40\,000$, limited to fine grid cases. In the early stages, the total energy follows the theoretical decay rate estimated by Landau & Lifschitz (Reference Landau and Lifshitz1987), whereas a sharp increase of energy dissipation occurs shortly after the onset of breaking. The time histories of the kinetic and potential energy contributions are characterized by oscillatory behaviours with opposite phases, associated with the bound wave component. As long as the wave is regular, the two contributions are balanced, and their sum remains constant. During the breaking stage, owing to plunging of the water jet with subsequent air entrainment and bubble fragmentation, large vortical structures develop that yield an increase of kinetic energy as compared to potential energy. The time history of the total energy shows that most dissipation occurs within about one wave period, in agreement with results of previous authors (Chen et al. Reference Chen, Kharif, Zaleski and Li1999; Iafrati Reference Iafrati2009; Deike et al. Reference Deike, Popinet and Melville2015, Reference Deike, Melville and Popinet2016; Wang et al. Reference Wang, Yang and Stern2016). As discussed by Iafrati (Reference Iafrati2011), most dissipation is associated with the formation of small-scale bubbles, which increase the size of the air–water interface and thus the surface tension contribution, and is accompanied with severe velocity gradients, mainly concentrated into vortex sheets (see below). The results of simulations at the two Reynolds numbers are quite similar, except for small differences in the dissipated energy fraction. Besides uncertainties discussed previously, part of this difference is associated with the different amount of the energy fraction that would be dissipated in the absence of breaking, as suggested by the theoretical estimates (thin black lines in figure 8). The above results corroborate findings made in previous studies (e.g. Lubin et al. Reference Lubin, Vincent, Abadie and Caltagirone2006; Iafrati Reference Iafrati2009; Deike et al. Reference Deike, Popinet and Melville2015), which showed that the dissipated energy fraction does not depend much on the Reynolds number, or on dimensionality.

Figure 8.

Time histories of kinetic energy ($E_k$), potential energy ($E_p$), surface tension energy ($E_s$) and total energy ($E_{tot}$) of water for 3-D wave breaking with initial steepness $\epsilon = 0.5$. Here, $E_0$ is the initial total energy, and $T$ is the wave period. The solid black line represents the theoretical linear viscous dissipation $E/E_0 = \exp (-4 \nu k^2 t)$, where $k=2 {\rm \pi}$ is the fundamental wavenumber (Landau & Lifschitz Reference Landau and Lifshitz1987). Plots are for: (a) $ {\textit {Re}}=10\,000$, fine grid (3D1E4f); (b) $ {\textit {Re}}=40\,000$, fine grid (3D4E4f).

With this background, it becomes interesting to investigate the dissipation process more deeply, by looking for possible differences in the basic mechanisms characterizing wave breaking at different Reynolds numbers. For that purpose, the time histories of viscous dissipation are compared in figure 9. At the beginning of the simulations, differences are just due to use of different Reynolds numbers. Dissipation increases sharply soon after the breaking starts, and it decays as $t^{-2}$ afterwards. It is worth noticing that in the late stage of the breaking process, the solutions at the two Reynolds numbers are nearly overlapped, implying that increased $ {\textit {Re}}$ is accompanied by increased velocity gradients, thus representing a special case of the general principle of dissipation anomaly (Onsager Reference Onsager1949). In order to identify better the zones where it is mostly concentrated, spanwise averages of the viscous dissipation have been computed at different times and shown in figure 10, at time instants corresponding to the vertical dashed lines in figure 9. The time evolution indicates that in the early stages of the breaking process, viscous dissipation is quite vigorous, and mostly localized about the plunging point and around the entrained air cavity. In the next stage, when the air cavity is pushed downwards, the viscous dissipation region broadens and propagates more in depth. Next, as the large air cavity fragments into smaller bubbles, the viscous dissipation decreases in amplitude but spreads behind the breaker, continuing to propagate in depth. By comparing the results obtained at the two Reynolds numbers, it is seen that that in the higher-$ {\textit {Re}}$ simulation, the region with high viscous dissipation displays sharper variations in space and a deeper penetration.

Figure 9.

Time histories of total viscous dissipation in 3-D wave breaking with initial steepness $\epsilon = 0.5$, for fine simulations at $ {\textit {Re}}=10\,000$ and $40\,000$. The green dash-dotted and purple dotted vertical lines indicate the time of the onset of breaking, whereas the black dashed lines represent the time instants shown in figure 10.

Figure 10.

Spanwise averages of viscous dissipation in 3-D simulation of wave breaking at (a) $ {\textit {Re}}=10\,000$ (3D1E4f), and (b) $ {\textit {Re}}= 40\,000$ (3D4E4f), in logarithmic scale. The white line marks the $0.5$ volume fraction iso-line.

3.5. Air entrainment and bubbles distribution

Whereas the above discussion is focused on global quantities, a more quantitative analysis of bubbles and vortical structures generated by the breaking process is presented herein. A rendering of the computed air–water interface is provided in figure 11 (more frames are provided in movie 1 and 2 in the online supplementary materials). As expected, the simulation at $ {\textit {Re}} = 40\,000$ includes smaller bubbles, which are grouped into larger clusters. In the simulation at $ {\textit {Re}} = 10\,000$, the air cavity entrained at the onset of the breaking retains its tubular shape for a longer time interval, and it takes some time before destabilizing and breaking into smaller bubbles. Conversely, at $ {\textit {Re}} = 40\,000$, the air cavity displays large perturbation in the spanwise direction already at the time when the jet touches the free surface ahead, thus it fragments rather quickly into smaller bubbles, meaning that the 3-D instability mechanisms become effective in play much earlier.

Figure 11.

Evolution of the breaking event all sequences are provided respectively in movie 1 and 2 ($Re= 10\,000$ and $Re=40\,000$) in the online supplementary materials for (a) $ {\textit {Re}}=10\,000$ (3D1E4f), and (b) $ {\textit {Re}}=40\,000$ (3D4E4f).

Because of its longer stability, the entrained air cavity at $ {\textit {Re}} = 10\,000$ can propagate deeper before fragmenting into smaller bubbles. A detailed illustration of the instability mechanism leading to fragmentation of the tubular air cavity for the case $ {\textit {Re}} = 10\,000$ is provided in figure 12. Here, the air cavity develops first modulations of the radius in the spanwise direction, which lead to the formation of large air bubbles connected by thin air filaments. As time elapses, the large bubbles move upwards under the action of the buoyancy, whereas the air filaments become thinner and longer. Finally, the air bubbles reach the upper water surface and degas, whereas the thin filaments break into tiny bubbles. This is a clear manifestation of the Rayleigh–Taylor instability mechanism involving gravity and surface tension (Gao, Deane & Shen Reference Gao, Deane and Shen2021b).

Figure 12.

Details of the fragmentation of the cylindrical air cavity in numerical simulation of wave breaking at $ {\textit {Re}}=10\,000$ (3D1E4f).

A quantitative analysis of the bubble size distribution generated during the breaking process is provided in figure 13. The theoretical distribution proposed by Deane & Stokes (Reference Deane and Stokes2002) is also shown for comparison. For bubble size larger than the Hinze scale (Hinze Reference Hinze1955), the bubble size distribution is the result of balance between turbulent velocity fluctuations and surface tension effects; it is characterized by a $-10/3$ power-law probability density function. As discussed by Soloviev & Lukas (Reference Soloviev and Lukas2014), large bubbles fragment due to both the instability of the air cavities and the detachment of small bubbles during the rising process associated with the buoyancy. Bubbles smaller than the Hinze scale are not prone to fragment owing to the stabilizing effect of surface tension, and are instead generated by jet/wave-face interaction throughout the active phase, and exhibit a $-3/2$ power-law probability density function (Deane & Stokes Reference Deane and Stokes2002). The bubble size distributions shown in figure 13 have been evaluated from flow samples stored at intervals $\Delta t/T \approx 0.02$ apart, from $t/T \approx 0.8$ to $t/T \approx 2.8$. The equivalent bubble radius is evaluated by using the algorithm developed by Herrmann (Reference Herrmann2010) to identify connected domains with the volume fraction field. The volumes of the domains thus identified are evaluated, and their equivalent radii are determined assuming a spherical shape, namely $R_{eq} = ( 3 {V} / (4 {\rm \pi}) )^{1/3}$. For the smaller bubbles, the $-3/2$ power law is observed for the finest grid only, as the limitations of the discrete model adopted for surface tension prevent a correct description of the interface dynamics for bubble with radius comparable to the cell size (Gao et al. Reference Gao, Deane, Liu and Shen2021a). This limitation is indeed confirmed by the change in the slope of the probability density functions occurring for bubbles with radius smaller than $2.5$ grid lengths.

Figure 13.

Probability density functions of bubble size, including all bubbles from $t/T = 0.8$ to $t/T=2.8$: (a) wave breaking at $ {\textit {Re}}=10\,000$; (b) wave breaking at $ {\textit {Re}}=40\,000$.

In addition to the global statistics of the bubble size, in figure 14, information concerning the number of the bubbles, their average size, the trapped air volume and the vertical position of their centre of mass is provided. As shown in figure 11, regardless of the grid resolution, at $ {\textit {Re}} = 10\,000$, larger air cavities are entrained at the onset of the breaking compared to the $ {\textit {Re}} = 40\,000$ case. As can be deduced from figure 14, shortly after the onset of the breaking, the large air cavity breaks into smaller bubbles (figure 12), thus leading to an increase in the bubble number and in a corresponding reduction of the average size. As anticipated previously, at $ {\textit {Re}} = 40\,000$, the interface is already strongly perturbed and a large cluster of bubbles is entrained at the onset of the breaking instead of a single large air cavity. At later stages, the bubble size remains almost constant, whereas the number of bubbles decreases owing to the degassing process. Comparison of data shows fewer, larger bubbles at $ {\textit {Re}} = 10\,000$ for $t/T < 1.4$, whereas for $t/T > 1.4$, the average bubble size is about the same, but more bubbles are found at $ {\textit {Re}} = 40\,000$. In both cases, the average bubble size approaches $1$ mm. It is worth noticing that also coarse grid results are very close each other, although far from the fine grid ones. Figure 14(b) also shows differences in the surface tension energy at the two Reynolds numbers, which might result from approximate estimation of the bubbles surface area, and because of the contribution of the free surface of the wave, which is not accounted for.

Figure 14.

Time histories of: (a) number of bubbles; (b) average equivalent bubbles radius and surface tension energy; (c) volume of trapped air; and (d) averaged depth of bubble centres.

In terms of the total entrained air volume (figure 14c), significant differences occur for $t/T < 1.4$, whereas the decay rate is rather similar for $t/T > 1.4$. As found through acoustic measurements by Eric & Melville (Reference Eric and Melville1991), after the initial air entrainment, the total air volume decays exponentially with coefficient $-3.9$, whereas the present results fit better with a $-2.9$ coefficient. In the late stages, the coarse simulations display a reduced decay rate, which is presumably associated with limitation of the post-processing in resolving the dynamics of the smallest bubbles.

The time histories of the vertical position of the centre of mass show that at the onset of breaking, the bubbles are mostly located above the still-water level, and as time progresses, they are dragged down to depths of the order of the initial wave amplitude. At $ {\textit {Re}} = 40\,000$ the position of the centre of mass exhibits large oscillations, presumably due to the large coherent structures formed during the breaking, whereas, presumably due to the higher viscosity, at $ {\textit {Re}} = 10\,000$ the descent of the position of the centre of mass is much more gentle.

In order to get a better understanding of the bubble size distribution at different stages of the breaking process, the statistics of the equivalent bubble radius versus time are provided in figure 15 for the fine-grid simulations. In the graphs, the average equivalent radius is also shown as a solid line. The data again confirm that at $ {\textit {Re}} = 10\,000$, a few larger and more persistent bubbles are formed at the onset of the breaking, whereas at $ {\textit {Re}} = 40\,000$, the air cavity is already fragmented into smaller bubbles. Furthermore, the maximum number of bubbles is achieved at different times, namely $t/T \approx 2$ for $ {\textit {Re}}=10\,000$, and $t/T \approx 1.45$ for $ {\textit {Re}}=40\,000$. Figure 16 provides information about the vertical distribution of the bubbles. In particular, the figure shows the number of bubbles lying in a horizontal slab with thickness $\Delta y\,\lambda = 0.6$ mm, as a function of time. No substantial effect of the Reynolds number is observed in terms of the maximum depth reached by the bubbles, although the concentration of bubbles in the deepest layers is higher for $ {\textit {Re}} = 40\,000$. Furthermore, for $ {\textit {Re}} =40\,000$, the bubbles are spread out in a wider region, whereas at $ {\textit {Re}} = 10\,000$, bubbles are preferentially concentrated around $y \lambda = -10$ mm.

Figure 15.

Bubble size distribution over time, for flow cases (a) 3D1E4f and (b) 3D4E4f. The vertical axis is in logarithmic scale, the colour map indicates the number of the bubbles, and the line with symbols denotes the average equivalent radius $\langle R_{eq}\rangle$.

Figure 16.

Bubble depth distribution over time, for flow cases (a) 3D1E4f and (b) 3D4E4f. The colour map indicates the number of bubbles, and the line with symbols denotes the average depth of the bubbles.

Figure 17 shows the distribution of the depth of the bubbles as a function of the respective size. Close to the free surface ($-20\ \textrm {mm} \leqslant y \lambda \leqslant 5\ \textrm {mm}$), bubbles with a wide range of sizes are present, the largest with radius about 10 mm. Moving deeper, only relatively small bubbles are present, with typical radius about 1 mm. As already observed, more bubbles penetrate deeply at higher Reynolds numbers. It is noteworthy that the above results cannot be extrapolated directly to the case of ocean waves, as fresh water is herein assumed. In fact, there is experimental evidence that salinity affects the process of micro-bubble formation, hence the overall number of bubbles that form in salt water is about an order of magnitude higher than in fresh water (Cartmill & Yang Su Reference Cartmill and Yang Su1993).

Figure 17.

Bubble depth distribution as a function of bubble size, for flow cases (a) 3D1E4f and (b) 3D4E4f. The colour map indicates the number of bubbles.

3.6. Coherent vortical structures

The results presented in the previous subsections have shown that air entrainment and bubble dynamics occurring at different Reynolds numbers are remarkably different, although the total energy dissipated during the breaking is essentially the same. It is therefore interesting to investigate in more depth the mechanisms governing the energy dissipation, and their connection with air entrainment and bubble fragmentation processes. This can be done by analysing the coherent vortical structures generated during the breaking phenomenon. Several types of vortical structures can be recognized in turbulence, which can be categorized roughly into vortex tubes and vortex sheets (She, Jackson & Orszag Reference She, Jackson and Orszag1990; Douady, Couder & Brachet Reference Douady, Couder and Brachet1991; Ruetsch & Maxey Reference Ruetsch and Maxey1992). Vortex tubes (the so-called worms) drew most of the attention in early numerical simulations and experiments (Vincent & Meneguzzi Reference Vincent and Meneguzzi1991; Cadot, Douady & Couder Reference Cadot, Douady and Couder1995), being the most prominent observed features. However, deeper analyses showed that vortex sheets, i.e. zones of locally nearly 2-D shearing motion, provide a dominant contribution to enstrophy production through vortex stretching and, in turn, to energy dissipation (Tsinober Reference Tsinober1998). Vortex sheets are often disregarded since they exhibit a strong tendency to roll up as a consequence of the Kelvin–Helmholtz instability mechanisms, leading to the formation of vortex tubes, hence their lifetimes are relatively short (Passot et al. Reference Passot, Politano, Sulem, Angilella and Meneguzzi1995). This is also the reason why intense vortical structures in turbulence come in the form of vortex tubes surrounded by vortex sheets spiralling around them (Horiuti & Takagi Reference Horiuti and Takagi2005).

In order to identify vortex tubes and vortex sheets, Pirozzoli, Bernardini & Grasso (Reference Pirozzoli, Bernardini and Grasso2008) introduced distinct vorticity-like variables, one more suitable to identify tube-like structures ($\omega _t$), and the other more appropriate to identify sheet-like vorticity distributions ($\omega _s$). After Zhou et al. (Reference Zhou, Adrian, Balachandar and Kendall1999), vortex tubes are identified as the connected regions where the velocity gradient tensor has one real eigenvalue ($\lambda _r$) and two complex conjugate eigenvalues ($\lambda _c = \lambda _{cr} \pm \mathrm {i} \lambda _{ci}$). In those regions, the discriminant of $u_{i,j}$ satisfies the condition

(3.9)\begin{equation} \varDelta = Q^{*3} + \tfrac{27}{4} R^{*2} > 0, \end{equation}

where $Q = - 1/2 u_{i,j} u_{j,i}$ and $R = -1/3 u_{i,j} u_{j,k} u_{k,i}$ are the second and third invariants of $u_{i,j}$ (the first being identically zero). Within the core of vortex tubes, the flow is then a combination of a straining motion with intensity $\lambda _r$, and a spiralling motion with angular velocity $\lambda _{ci}$. It can be shown readily that in the case of 2-D solid-body rotation, the imaginary part of the complex eigenvalue pair is proportional to the vorticity modulus ($\lambda _{ci} = \omega / 2$), hence a vorticity-like variable can be introduced to characterize vortex tubes:

(3.10)\begin{equation} \omega_t = 2 \lambda_{ci}. \end{equation}

Tubes are defined as regions where $\omega _t$ exceeds a physically relevant threshold value.

The identification of the vortex sheets relies on the work of Horiuti & Takagi (Reference Horiuti and Takagi2005). Let $S_{i,j}$ and $W_{i,j}$ be the symmetric and antisymmetric parts of the velocity gradient tensor. Then vortex sheets are identified as the regions where the largest eigenvalue ($\lambda _L$) of the tensor $L_{i,j} = S_{i,k} W_{k,j} + S_{j,k} W_{k,i}$ is positive, after discarding the eigenvector that is most aligned with the vorticity vector. In the case of a pure 2-D parallel shear flow, by its definition, $\lambda _L$ turns out to be proportional to the square of the vorticity modulus ($\lambda _L = \omega ^2 / 2$), hence a vorticity-like variable can be introduced to characterize vortex sheets:

(3.11)\begin{equation} \omega_s = \sqrt{2 \lambda_L}. \end{equation}

Sheets are defined as regions where $\omega _s$ exceeds a physically relevant threshold value.

Iso-surfaces of the vortex tube and vortex sheet indicators at various times during the breaking process from data for $ {\textit {Re}} = 10\,000$ and $40\,000$ are shown in figure 18. The plots show that a strong shear layer is formed at the onset of breaking, which becomes quite strong once the jet plunges onto the free surface and entrains the large air cavity (see figures 18a–d). Hence smaller structures develop as a consequence of the bubble fragmentation process and of the large velocity gradients developing inside the bubble clouds (see figures 18d–g). In the simulation at $ {\textit {Re}} = 10\,000$, a vortex sheet initially develops around the entrained air column, and it retains a 2-D shape for a long time interval. Next, when the air column collapses, the vortex sheets develop thinner and more irregular shapes (see figure 18g). In the case at $ {\textit {Re}} = 40\,000$, the air cavity is already disrupted at the onset of breaking, therefore vortex sheets exhibit a 3-D irregular pattern from the very beginning. Owing to severe stretching, the structures become elongated along the streamwise direction shortly after the first plunging event (see figure 18b). Coherent tubular structures develop progressively inside the vortex sheets, initially with shape similar to the parent vortex sheets. The latter then roll up around the tubes as a result of Kelvin–Helmholtz instability, which is very similar to that observed in isotropic turbulence (Horiuti & Takagi Reference Horiuti and Takagi2005). Three types of tubular structures can be identified. The first is obviously the hollow cylinder extending spanwise, associated with entrainment of the large air cavity during the initial plunging event. The second type includes the streamwise vortices formed around the air tubes in a periodic series (see Lubin & Glockner Reference Lubin and Glockner2015). A third type includes hairpin-like vortices resembling those generated in boundary layers (Wu & Moin Reference Wu and Moin2009; Schlatter & Örlü Reference Schlatter and Örlü2012; Pierce, Moin & Sayadi Reference Pierce, Moin and Sayadi2013), which emerge in the last stages of the breaking event, as shown in figures 19(c,d).

Figure 18.

View from under the water level of vortex tubes and vortex sheets in a plunging breaking event at (a,c,e,g) $ {\textit {Re}} = 10\,000$(3D1E4f), and (b,d,f,h) $ {\textit {Re}} = 40\,000$ (3D4E4f), in their evolution from $t/T \approx 0.8$ to $t/T \approx 1.4$. Vortex tubes are rendered as yellow iso-surfaces of $\omega _t = 20$, and vortex sheet are rendered as grey iso-surfaces of $\omega _s = 20$.

Figure 19.

View from under the water level of vortex tubes in a plunging breaking event at (a,c) $ {\textit {Re}} = 10\,000$ (3D1E4f) and (b,d) $Re=40\ 000$ (3D4E4f). Vortex tubes are rendered as yellow iso-surfaces of $\omega _t = 20$.

The first type of tube is particularly evident in the simulation at $ {\textit {Re}} = 10\,000$ soon after the plunging process. Streamwise tubes are more evident in the simulation at $ {\textit {Re}} = 40\,000$, whereas they are much less evident at $ {\textit {Re}} = 10\,000$, despite the presence of some streamwise air filaments. This is presumably a consequence of the weak vorticity generated at the lower Reynolds number, or the relatively large value of $\omega _t$ chosen for their identification. Hairpin-like vortices occur starting from $t / T \approx 1.0$ (see figures 19c,d), and considering their resemblance to the structures developing in turbulent boundary layers, they seem to be a consequence of the surface current underneath the air–water interface (Iafrati Reference Iafrati2009). As expected, the simulations show that filamentary vortex structures at the higher Reynolds numbers are smaller and more numerous. In fact, although vortex tubes are mostly responsible for intermittency (Douady et al. Reference Douady, Couder and Brachet1991; Sreenivasan & Antonia Reference Sreenivasan and Antonia1997; Moisy & Jiménez Reference Moisy and Jiménez2004), evidence shows that intense dissipation takes place mainly within vortex sheets that emanate from, and are spiralling around, the core region of vortex tubes (Kawahara Reference Kawahara2005).

In order to better understand the connections between air entrainment and viscous dissipation with vortical structures, in figures 20 and 21, slices taken in the longitudinal symmetry plane, in a horizontal plane, and in two cross-stream planes are drawn. Note that different time instants are considered for the two Reynolds numbers, in order to capture the most relevant configurations of each case. For clarity, the analysis is limited to the water phase ($C \geqslant 0.5$). The results display clearly close correlation between viscous dissipation and the vortex sheet indicator, at both Reynolds numbers. It is also worth noticing that viscous dissipation is not confined around the free surface, but is also high around the entrained bubbles, being a likely consequence of the bubble fragmentation process. Within the high-dissipation regions marked by the vortex sheet indicator, vortex tubes also form in zones with high vorticity. Due to entrainment of the elongated air cavity, at $ {\textit {Re}}=10\,000$, vortex tubes are correlated mainly with spanwise vorticity (see figure 20f), whereas at $ {\textit {Re}}=40\,000$, due to fragmentation of the air cavity, vorticity is more isotropic, and vortex tubes are well correlated with all vorticity components.

Figure 20.

Instantaneous visualizations in two cross-stream planes (b–e), in the longitudinal symmetry plane (f,g), and in a horizontal plane (h,i), for wave breaking at $ {\textit {Re}}=10\,000$ (3D1E4f). See panel (a) for the precise location of the planes. Coloured contours denote the local values of the normal-to-plane vorticity components (b,d,f,h), and the local dissipation rate (c,e,g,i). The black solid lines in (b,d,f,h) denote the $\omega _t=20$ iso-line, and in (c,e,g,i) the $\omega _s=20$ iso-line. Only points belonging to the water phase are shown ($C \geqslant 0.5$).

Figure 21.

Instantaneous visualizations in two cross-stream planes (b–e), in the longitudinal symmetry plane (f,g), and in a horizontal plane (h,i), for wave breaking at $ {\textit {Re}}=40\,000$ (3D4E4f). See panel (a) for the precise location of the planes. Coloured contours denote the local values of the normal-to-plane vorticity components (b,d,f,h), and the local dissipation rate (right). The black solid lines in (b,d,f,h) denote the $\omega _t=20$ iso-line, and in (c,e,g,i) the $\omega _s=20$ iso-line. Only points belonging to the water phase are shown ($C \geqslant 0.5$).

In order to retrieve more quantitative information about the statistics among the various indicators, vertical profiles of their averages in the longitudinal and spanwise directions are shown in figure 22. Figures 22(a,b) refer to the same time instants as figures 20 and 21, whereas figures 22(c,d) refer to a later time, $t/T = 1.6$. Figures 22(a,b) show that for both Reynolds numbers, the vorticity is mainly concentrated in the region $y \approx -0.08 {-}0.08$, and the dissipation also attain its maximum in the same zone. In fact, that is the zone where the horizontal average density is between $0.001$ and $0.999$, i.e. where the average density takes intermediate values between pure air and pure water. It is clear that the concentration of high vorticity, vortical structures and dissipation happens where the fragmentation and bubbles productions phenomena take place. Moreover, the spanwise vorticity component very nearly coincides with its modulus at $ {\textit {Re}} = 10\,000$, whereas the vorticity is more isotropic at $ {\textit {Re}} = 40\,000$ as a result of fragmentation of the entrapped air cavity.

Figure 22.

Vertical profiles of horizontal (spanwise and streamwise) averages in the water phase of viscous dissipation ($\epsilon$), vorticity modulus ($| \omega |$), streamwise vorticity ($| \omega _x |$), vertical vorticity ($| \omega _y |$), spanwise vorticity ($| \omega _z |$), vorticity-like variable for vortex tubes ($\omega _t$), vorticity-like variable for vortex sheet ($\omega _s$), and mean volume fraction ($\bar {C}$), for: (a) $ {\textit {Re}}=10\,000$ (3D1E4f) at $t/T=0.938$; (b) $ {\textit {Re}}=40\,000$ (3D4E4f) at $t/T=0.878$; (c) $ {\textit {Re}}=10\,000$ (3D1E4f) at $t/T=1.6$; (d) $ {\textit {Re}}=40\,000$ (3D4E4f) at $t/T=1.6$. The shaded area denotes the mixing region ($0.001 < \bar {C} < 0.999$).

At later stages, i.e. figures 22(c,d), the vorticity propagates deeper, but at $ {\textit {Re}} = 10\,000$ it decreases sharply at $y \lesssim -0.20$, whereas at $ {\textit {Re}} = 40\,000$ the decay is milder. It is interesting to note that at that depth, the total dissipation at $ {\textit {Re}} = 40\,000$ is two orders of magnitude higher. In all cases, it should be noted that dissipation is larger wherever vortex sheets, namely $\omega _s$, are intense. Vortical structures are generated in the mixing zone due mainly to air entrainment and bubble fragmentation, and in the next stage, they are entrained downwards, where most viscous dissipation takes place.

In order to highlight how and to what extent vortical structures are linked to viscous dissipation, the correlation coefficients between vorticity-like variables for vortex sheets and vortex tubes, and viscous dissipation, have been evaluated, as shown in figure 23. Inside the water phase, association between vortex sheets and dissipation is nearly perfect, becoming a little less in the mixing region, where, however, the correlation coefficient is still around $0.8$. Association between tubes and dissipation is, on the other hand, negligible in water, becoming about $0.4$ in the mixing region. Whereas the same trend is observed at the two Reynolds numbers, it is interesting that at the higher $ {\textit {Re}}$, the region with significant vortical activity extends well under the mixing region.

Figure 23.

Vertical profiles in the water phase of the correlation coefficient between the vorticity-like variable for vortex tubes and vorticity-like variable for vortex sheets ($R( \omega _t, \omega _s )$), vorticity-like variable for vortex tubes and viscous dissipation ($R( \omega _t, \epsilon )$), vorticity-like variable for vortex sheet and viscous dissipation ($R( \omega _s, \epsilon )$), and mean volume fraction ($\bar {C}$), for: (a) $ {\textit {Re}}=10\,000$ (3D1E4f) at $t/T=0.938$; (b) $ {\textit {Re}}=40\,000$ (3D4E4f) at $t/T=0.878$; (c) $ {\textit {Re}}=10\,000$ (3D1E4f) at $t/T=1.6$; (d) $ {\textit {Re}}=40\,000$ (3D4E4f) at $t/T=1.6$. The shaded area denotes the mixing region ($0.001 < \bar {C} < 0.999$).