3.1. Flow regimes

As a representative example, figure 5 shows the evolution of the two-layer gravity current for run 10, with $R_{\rho }=2$ and $R_h=1$. Upon removal of the gate, the lower layer (in blue) develops a distinct head, whereas the upper layer (in red) forms a wedge-like intrusion behind the lower-layer head, cf. figure 5(a). The shear along the interface between the ambient and dense fluids results in the formation of strong Kelvin–Helmholtz vortices. As the current propagates further, we can distinguish a dense head of lower-layer fluid and a more dilute wake containing both upper and lower-layer fluid (figure 5b). These findings are similar to previous experimental observations (Gladstone et al. Reference Gladstone, Ritchie, Sparks and Woods2004; Dai Reference Dai2017; Wu & Dai Reference Wu and Dai2020; He et al. Reference He, Zhu, Zhao, Chen, Lin and Yuan2021). The wake region immediately behind the head is characterised by strong turbulent mixing of the lock fluid layers, whereas further back, the two dense layers remain more distinct, as seen in figure 5(c). The mixed region gradually expands, as dense fluid from the head is transported into the turbulent wake (figure 5d).

Figure 5.

Instantaneous concentration isosurfaces $c_U=0.1$ and $c_L=0.1$, along with the concentration field for both upper and lower layers for run 10 ($R_{\rho }=2$ and $R_h=1$), (a) $t=5$, (b) $t=10$, (c) $t=15$ and (d) $t=20$.

Figure 6 compares three cases with identical thickness ratio $R_h=1$, but different density ratios $R_{\rho }$, i.e. runs 2–4. For a moderate density ratio $R_{\rho }=1.25$, the fronts emerging from the upper and lower lock layers initially have comparable velocities, and significant mixing occurs near the head of the current (figure 6a). For larger density ratios ($R_{\rho }=2$ and 4), on the other hand, the lower layer front propagates much faster than the upper layer front, so that the current head consists nearly entirely of lower-layer fluid, which was also observed by Wu & Dai (Reference Wu and Dai2020). The upper, red layer advances much more slowly, giving rise to much weaker Kelvin–Helmholtz vortices along its interface with the ambient fluid, along with much less-vigorous mixing (figure 6b,c).

Figure 6.

Instantaneous concentration isosurfaces $c_U=0.1$ and $c_L=0.1$, along with the concentration field for both upper and lower layers at $t=20$ for $R_h=1$: (a) run 2 for $R_{\rho }=1.25$, (b) run 3 for $R_{\rho }=2$ and (c) run 4 for $R_{\rho }=4$.

Figure 7 focuses on flows with constant density ratio $R_{\rho }=4$ and different thickness ratios $R_h$, i.e. runs 1, 4, 7 and 14. For $R_h=0$, the lower layer is absent and the upper layer propagates as a single-layer gravity current (figure 7a). For the small but finite value $R_h=0.1$, the thin lower layer lubricates the much thicker upper layer, so that the upper layer advances faster than for $R_h=0$. Note that the head of the upper layer outruns the lower layer front (figure 7b). A similar trend was also observed by Gladstone et al. (Reference Gladstone, Ritchie, Sparks and Woods2004), Dai (Reference Dai2017), Wu & Dai (Reference Wu and Dai2020) and He et al. (Reference He, Zhu, Zhao, Chen, Lin and Yuan2021). The conditions under which this can occur are discussed in more detail in the following section. For $R_h=0.25$ the two front velocities are similar, and significant mixing occurs in the head region (figure 7c). For $R_h=1.5$, on the other hand, the lower layer front propagates faster than the upper layer, so that the current head consists mostly of lower-layer fluid (figure 7d). We now proceed to a more quantitative analysis of the dependence of the front velocity, energy budget, mixing and entrainment on $R_{\rho }$ and $R_h$.

Figure 7.

Instantaneous concentration isosurfaces $c_U=0.1$ and $c_L=0.1$, along with the concentration field for both upper and lower layers for $R_{\rho }=4$: (a) run 1 for $R_h=0$ at $t=30$, (b) run 4 for $R_h=0.1$ at $t=30$, (c) run 7 for $R_h=0.25$ at $t=30$ and (d) run 14 for $R_h=1.5$ at $t=18$.

3.2. Front velocity

We define the front positions $X_{f,U}$ and $X_{f,L}$ of the upper and lower layers as the rightmost locations in the flow field with $c_U=0.5$ and $c_L=0.5$, respectively. This large threshold value is selected so that small amounts of fluid from one layer that have become entrained into the other layer do not result in a spurious front location value. The respective front velocities are then obtained as $U_{f,U} = {\rm {d}} X_{f,U} / {\rm {d}} t$ and $U_{f,L}={\rm {d}} X_{f,L}/{\rm {d}} t$.

Figure 8 displays the front velocities as functions of time for runs 4 and 10. For single-layer currents, it is well known that they proceed through a short acceleration phase into a constant-velocity slumping phase that can last for an extended period of time and typically extends over approximately four lock lengths (Rottman & Simpson Reference Rottman and Simpson1983). Figure 8 indicates that the two-layer gravity currents of the present study stay within the slumping phase throughout the entire simulation, as their front velocity, which is determined by the rate at which the more advanced layer propagates, remains approximately constant. The slower layer, on the other hand, displays a highly unsteady front velocity, as it is strongly affected by the turbulent wake of the current head.

Figure 8.

Upper and lower layer front velocities $U_f$ as a function of time for different density ratios $R_{\rho }$ and height ratios $R_h$. (a) The lower layer moves ahead of the upper layer for run 10 ($R_{\rho }=2$, $R_h=1$). (b) The upper layer overtakes the lower layer for run 4 ($R_{\rho }=4$, $R_h=0.1$).

Figure 8(a) shows that for run 10 the velocity of the lower, faster layer remains approximately constant, whereas that of the upper, slower layer fluctuates with time. Figure 8(b), on the other hand, indicates that for run 4 the upper, faster layer propagates at an approximately constant velocity, whereas the lower, slower layer decelerates and does not develop a quasi-steady front velocity.

We now proceed to employ the conservation of mass and vorticity to develop a circulation model for the case of a faster lower layer, by building on the earlier work by Borden & Meiburg (Reference Borden and Meiburg2013). Figure 9 presents the schematic flow field. After removal of the gate, the lower-layer lock fluid forms a right-propagating gravity current front of height $h_{gc,L}$ with velocity $U_{f,L}$. Far behind the front, a discontinuity propagates with velocity $U_{r,L}$ to the left. Simultaneously, a counter current of velocity $U_0$ emerges in the ambient fluid above the gravity current. Subsequently, the upper-layer lock fluid also forms a gravity current of height $h_{gc,U}$ and velocity $U_{f,U}$ that propagates on top of the lower layer fluid. The flow is fully described by eight dimensionless unknowns: $U_{f,L}$, $U_0$, $U_{r,L}$, $U_{f,U}$, $U_U$, $U_{r,U}$, $h_{gc,L}$ and $h_{gc,U}$.

Figure 9.

Model flow for predicting the upper and lower layer front velocities $U_{f,U}$ and $U_{f,L}$.

Within control volume EFGI, and in the reference frame moving with the lower layer fluid, mass conservation for the ambient fluid gives

(3.1)\begin{equation} U_{f,L}h_{gc,L}=U_0(H-h_{gc,L}). \end{equation}

Because no vorticity enters the control volume, and vorticity flows out of the control volume confined to a thin vortex sheet between the lower layer and the ambient fluid, the vorticity flux is equal to the vortex sheet strength $U_0+U_{f,L}$, multiplied by the sheet's principal velocity $(U_0+U_{f,L})/2$. The vorticity conservation at the interface gives

(3.2)\begin{equation} R_{\rho}h_{gc,L}=\tfrac{1}{2}(U_0+U_{f,L})^2. \end{equation}

In control volume DEIJ, in the reference frame moving with the upper layer, the mass conservation for the ambient fluid, along with vorticity conservation at the upper surface of the upper layer can be written as

(3.3)\begin{gather} U_0(H-h_{gc,L})+U_{f,U}h_{gc,U}=U_{r,U}(H-h_{gc,L}-h_{gc,U}), \end{gather}

(3.4)\begin{gather}h_{gc,U}=\tfrac{1}{2}(U_{r,U}+U_{f,U})^2. \end{gather}

For control volume CDJK, in the frame moving with the disturbance of the upper layer, mass and vorticity conservation yields

(3.5)\begin{gather} U_{r,U}(H-h_{gc,L}-h_{gc,U})=U_U(H-h_{gc,L})+U_{f,U}h_{gc,U}, \end{gather}

(3.6)\begin{gather}H-h_{gc,L}-h_{gc,U}=\tfrac{1}{2}(U_{f,U}+U_{r,U})^2. \end{gather}

Similarly in control volume BCKM, in the frame moving with the disturbance of the lower layer, mass and vorticity conservation leads to

(3.7)\begin{gather} U_U(H-h_{gc,L})=U_{r,L}(H-h_{gc,L}-h_U), \end{gather}

(3.8)\begin{gather}(R_{\rho}-1)(h_L-h^L_{gc})=(U_{f,L}+U_U)\left(\frac{U_{f,L}-U_U}{2}+U_{r,L}\right). \end{gather}

By combining these equations, we obtain for the dimensionless front velocity and height of the upper and lower layer gravity currents

(3.9a,b)\begin{gather} U_{f,L}= \frac{(2+2R_h-h_{gc,L})\sqrt{2R_{\rho}h_{gc,L}}}{2(1+R_h)},\quad U_{f,U} = \frac{\sqrt{2h_{gc,U}}}{2}-\frac{h_{gc,L}\sqrt{2R_{\rho}h_{gc,L}}}{2(1+R_h)}. \end{gather}

(3.10)\begin{gather}h_{gc,L}=\frac{R_h(1+R_h)(3R_{\rho}-2)-R_h\sqrt{R_{\rho}(1+R_h)[R_{\rho}(9+R_h)-8]}}{R_h(2R_{\rho}-1)-1}, \end{gather}

(3.11)\begin{gather}h_{gc,U}=\frac{(1+R_h)(R_{\rho}R_h-2)+R_h\sqrt{R_{\rho}(1+R_h)[R_{\rho}(9+R_h)-8]}}{2R_h(2R_{\rho}-1)-2}. \end{gather}

Figure 10 compares simulation results for the upper and lower layer front velocities with corresponding experimental data of He et al. (Reference He, Zhu, Zhao, Chen, Lin and Yuan2021), and with predictions by (3.9a,b). We observe generally good agreement, as reflected by the coefficient of determination $R^2=0.814$. We note that for $R_h=0$, i.e. in the absence of a lower layer, (3.9a,b) yields the correct solution $U_{f,U}=\sqrt {2}/2$ for single-layer currents (Borden & Meiburg Reference Borden and Meiburg2013). In the limit of $R_\rho =1$, the two layers have identical density and form a single-layer current with $U_{f,U}=\sqrt {2(R_h+1)}/2$, which is again consistent with Borden & Meiburg (Reference Borden and Meiburg2013). If we mix the two lock layers initially so as to form a homogeneous lock fluid, a single-layer current forms with front velocity $\sqrt {2(1+R_hR_{\rho })}/2$, based on the circulation model and the half-depth assumption. Corresponding data, indicated in figure 10, suggest that the front velocity of a two-layer current is quantitatively similar to that of an equivalent, initially well-mixed single-layer current.

Figure 10.

The black and blue symbols compare simulation results for the upper and lower layer front velocities, along with experimental data by He et al. (Reference He, Zhu, Zhao, Chen, Lin and Yuan2021), to corresponding predictions by (3.9a,b). The experimental data are for cases with $R_{\rho }=5$ for $R_h=0.34$ and 0.13. For all cases the lower layer moves faster than the upper layer. Also shown by red symbols are the corresponding simulation results for single-layer currents and predictions by $\sqrt {2(1+R_hR_{\rho })}/2$.

Figure 11 shows predictions for the front velocities by (3.9a,b) as functions of $R_h$, for different values of $R_{\rho }$. Here $U_{f,L}$ increases with $R_h$ and $R_{\rho }$. When $R_{\rho }$ is small, $U_{f,U}$ increases slightly for all $R_h$. For larger $R_{\rho }$, on the other hand, $U_{f,U}$ decreases for all $R_h$ values. This illustrates the competing effects of increased potential energy conversion and larger ambient counter-current velocity. We furthermore note that as $R_{\rho }$ increases, a smaller value of $R_h$ will suffice to ensure that the lower layer propagates faster than the upper layer.

Figure 11.

Predictions by (3.9a,b) for the upper and lower layer front velocities, $U_{f,U}$ and $U_{f,L}$, as functions of $R_h$, for different values of $R_{\rho }$.

3.3. Energy budget

The initial potential energy stored in the upper and lower dense fluid layers acts as the source that drives the flow. Once the gate opens, this potential energy is partially converted into kinetic energy, which is subsequently dissipated by the action of viscosity. In the following, we analyse these energy conversion processes quantitatively, along with the energy transfer between the different fluid layers. Towards this end, we define the potential energy $E_p$, kinetic energy $E_k$ and dissipated energy $E_d$, respectively, as

(3.12)\begin{gather} E_p(t)=\int^W_0\int^{H}_0\int^L_0 (c_U+R_{\rho}c_L)(y-h_L)\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.13)\begin{gather}E_k(t)=\int^W_0\int^{H}_0\int^L_0 \tfrac{1}{2}(u^2+v^2+w^2)\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.14)\begin{gather}E_d(t)=\int^t_0\varepsilon(\tau)\,\mathrm{d}\tau, \end{gather}

where $u$, $v$ and $w$ indicate the fluid velocity components in the $x$, $y$ and $z$ directions. Note that we focus on the potential energy relative to the situation with ambient fluid everywhere. We choose the initial top boundary of the lower dense layer $y=h_L$ as our reference level, so that the initial potential energy contained in the upper lock layer is constant for all cases. Here $\varepsilon$ indicates the instantaneous viscous dissipation rate

(3.15)\begin{equation} \varepsilon(t) = \int^W_0\int^{H}_0\int^L_0 \frac{2}{Re}s_{ij}s_{ij}\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{equation}

with $s_{ij}$ denoting the rate-of-strain tensor

(3.16)\begin{equation} s_{ij} = \frac{1}{2}\left(\frac{\partial u_i}{\partial x_j}+\frac{\partial u_j}{\partial x_i}\right). \end{equation}

As the fluid is at rest initially, the overall energy budget of the flow takes the form

(3.17)\begin{equation} E_{total}=E_p+E_k+E_d=\mathrm{const.}=E_{p,init}, \end{equation}

where $E_{p,init}$ represents the initial potential energy. To analyse the time-dependent conversion of potential, kinetic and dissipated energy, and the energy transfer among the different layers, we consider the respective contributions of the individual layers to the overall energy budget:

(3.18)\begin{gather} E_k=E_{kU}+E_{kL}+E_{k0}, \end{gather}

(3.19)\begin{gather}E_p=E_{pU}+E_{pL}, \end{gather}

(3.20)\begin{gather}E_d=E_{dU}+E_{dL}+E_{d0}, \end{gather}

(3.21)\begin{gather}\varepsilon=\varepsilon_U+\varepsilon_L+\varepsilon_0, \end{gather}

where the subscripts $U$, $L$ and $0$ again refer to the upper layer, lower layer and ambient fluid, respectively. These contributions take the form

(3.22)\begin{gather} E_{kU}(t)=\int^W_0\int^{H}_0\int^L_0 c_U\tfrac{1}{2}(u^2+v^2+w^2)\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.23)\begin{gather}E_{kL}(t)=\int^W_0\int^{H}_0\int^L_0 c_L\tfrac{1}{2}(u^2+v^2+w^2)\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.24)\begin{gather}E_{k0}(t)=\int^W_0\int^{H}_0\int^L_0 (1-c_U-c_L)\tfrac{1}{2}(u^2+v^2+w^2)\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.25)\begin{gather}E_{pU}(t)=\int^W_0\int^{H}_0\int^L_0c_U(y-h_L)\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.26)\begin{gather}E_{pL}(t)=\int^W_0\int^{H}_0\int^L_0R_{\rho}c_L(y-h_L)\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.27)\begin{gather}\varepsilon_U(t)=\int^W_0\int^{H}_0\int^L_0c_U\frac{2}{Re}s_{ij}s_{ij}\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.28)\begin{gather}\varepsilon_L(t)=\int^W_0\int^{H}_0\int^L_0c_L\frac{2}{Re}s_{ij}s_{ij}\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.29)\begin{gather}\varepsilon_0(t)=\int^W_0\int^{H}_0\int^L_0(1-c_U-c_L)\frac{2}{Re}s_{ij}s_{ij}\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z. \end{gather}

Figure 12 shows the time evolution of all energy components for the representative example of run 9 with $R_{\rho }=1.25$ and $R_h=1$. Note that all energy components are normalised by the initial potential energy of the upper dense layer $E_{pU,init}$. The total energy $E_{total}$ varies by around $1.5\,\%$ of $E_{pU,init}$ over the course of the simulation, which suggests that energy is conserved with good accuracy throughout the simulation.

Figure 12.

Time history of the various energy budget components for run 9 with $R_{\rho }=1.25$ and $R_h=1$.

For the first 10 time units the potential energy of the upper and lower dense layers rapidly decreases as the lock fluid collapses, whereas the kinetic energy of all three layers increases. Around $t \approx 10$, the collapse of the lower layer is nearly complete and its potential energy levels off. For late times, its potential energy even increases slightly due to mixing processes that tend to lift up parcels of dense fluid. On the other hand, the upper dense fluid layer continues to lose potential energy. The kinetic energy of all three layers levels off after $t \approx 10$. For late times $E_{kU}$ and $E_{kL}$ gradually decrease due to the effects of dissipation. The dissipated energy grows slowly with time for all three layers.

Figure 13 shows the influence of the density ratio $R_{\rho }$ and the height ratio $R_h$ on the evolution of the different energy components. Figure 13(a) indicates that the kinetic energy and dissipation of the upper layer do not vary significantly with the lower layer density, even though the upper layer loses potential energy faster in the presence of a denser lower layer that collapses more quickly. Figure 13(b) shows that the energetics of the lower layer are affected more strongly by an increase in $R_{\rho }$. As the density of the lower layer increases, it converts potential energy into kinetic energy more quickly, and it dissipates energy at a faster rate. As a larger height ratio $R_h$ also causes the lower layer to propagate faster, $R_h$ has a similar influence on the lower layer energy components as $R_{\rho }$, cf. figure 13(d). On the other hand, the dynamics of the upper layer are affected more strongly by $R_h$ than by $R_{\rho }$, cf. figure 13(c). Here $E_{kU}$ and $E_{dU}$ increase with $R_h$, because for larger $R_h$, the upper layer can descend to a lower vertical level, which enables it to convert more potential energy into kinetic energy.

Figure 13.

The evolution of the various energy budget components for different $R_{\rho }$ and $R_h$: (a) upper layer energy components for $R_h=1$ and different $R_{\rho }$ values, i.e. runs 9–11; (b) lower layer energy components for $R_h=1$ and different $R_{\rho }$ values; (c) upper layer energy components for $R_{\rho }=1.25$ and different $R_h$, i.e. runs 5, 9 and 12; and (d) lower layer energy components for $R_{\rho }=1.25$ and different $R_h$.

For a single-layer gravity current, the dense fluid always transfers energy to the ambient fluid, e.g. Necker et al. (Reference Necker, Härtel, Kleiser and Meiburg2002) and He et al. (Reference He, Zhao, Hu, Yu and Lin2018). For a two-layer gravity current the situation becomes more complex, as shown in figure 14. In this figure we analyse the change in total energy for each individual fluid layer, ${\rm \Delta} E_U$, ${\rm \Delta} E_L$ and ${\rm \Delta} E_0$, in order to obtain insight into the energy transfer between the different layers. Although the ambient fluid gains energy for all values of $R_{\rho }$ and $R_h$, and the upper dense layer always loses energy, the lower dense layer can gain or lose energy, depending on the specific values of the governing dimensionless parameters. This net energy gain of the lower dense layer, as a result of energy transfer from the upper layer, is perhaps somewhat unexpected. To quantify this effect as function of $R_\rho$ and $R_h$, we focus on the normalised ${\rm \Delta} E_U$ and ${\rm \Delta} E_L$ at the representative time $t=20$. Figure 15(a) presents ${\rm \Delta} E_U$ as a function of $R_h$ for different values of $R_\rho$. We find that to a good approximation ${\rm \Delta} E_U$ varies linearly with $R_h$. Thus, we look for a scaling parameter of the form $R^{\lambda _1}_{\rho } R_h$. Figure 15(b) shows that the raw data are well fitted ($R^2=0.997$) by a straight line of the form

(3.30)\begin{equation} \frac{{\rm \Delta} E_U}{E_{pU,init}}={-}0.2-1.1R^{0.2}_{\rho}R_h. \end{equation}

The intersect with the vertical axis at $-$0.2 indicates that the upper layer loses about $20\,\%$ of its initial energy when $R_h=0$. This suggests that a single-layer gravity current with a small aspect ratio will transfer approximately $20\,\%$ of its initial energy to the ambient fluid, as the lock fluid collapses and forms the gravity current. A similar conclusion can also be found from Zhu, He & Meiburg (Reference Zhu, He and Meiburg2021). On the other hand, the energy variation of the upper layer mainly comes from the decrease of the potential energy $E_{pU}$, which is shown in figure 13. $E_{pU}$ changes approximately linearly with $R_h$. However, a larger $R_\rho$ results in a faster lower layer, which enhances the loss of $E_{pU}$ indirectly. Equation (3.30) captures the linear and nonlinear dependence of $E_{pU}$ on $R_h$ and $R_\rho$, respectively, and it reflects that the decrease of $E_U$ depends more strongly on $R_h$ than on $R_\rho$.

Figure 14.

Time history of the variation of the total energy of the upper layer fluid ${\rm \Delta} E_U$, the lower layer fluid ${\rm \Delta} E_L$ and the ambient fluid ${\rm \Delta} E_0$ for the cases with (a) $R_h=1$ and different $R_{\rho }$, i.e. runs 9–11, and (b) $R_{\rho }=1.25$ and different $R_h$, i.e. runs 5, 9 and 12.

Figure 15.

Variation of the total energy of the upper layer fluid ${\rm \Delta} E_U$, and of the lower layer fluid ${\rm \Delta} E_L$, for different values of $R_{\rho }$ and $R_h$.

Figure 15(c) shows the normalised ${\rm \Delta} E_L$ as a function of the height ratio $R_h$ for different density ratios $R_\rho$. As $R_h$ increases, ${\rm \Delta} E_L$ initially increases as well, but it subsequently reaches a maximum and then decreases. This suggests that for small $R_h$ the lower layer gains more energy from the upper layer than it transfers to the ambient fluid, whereas for large $R_h$ this situation is reversed. We find that the raw data depend parabolically on $R^{0.8}_{\rho } R_h$, as seen in figure 15(d). A good fit ($R^2=0.999$) is achieved by

(3.31)\begin{equation} \frac{{\rm \Delta} E_L}{E_{pU,init}}={-}0.1(R^{0.8}_{\rho} R_h-1)^2+0.1. \end{equation}

When $R_h=0$, the lower layer does not exist and ${\rm \Delta} E_L$ is zero. Equation (3.31) also indicates that the lower layer gains a maximum of $10\,\%$ of the initial upper layer energy, when $R^{0.8}_{\rho } R_h=1$. Here $R^{0.8}_{\rho } R_h$ can be roughly interpreted as representing the mass of the lower layer. A lower layer of larger mass obtains more energy from the upper layer, up to a threshold beyond which the effect of the upper layer on the lower layer starts to wane, and the lower layer transfers more energy to the ambient fluid.

3.4. Mixing of the upper and lower layers

We now proceed to analyse and quantify the mixing dynamics between the upper and lower dense fluid layers, which strongly affects the overall propagation rate of the two-layer current. In order to obtain insight into the Lagrangian mixing behaviour, we mark individual fluid patches by passive tracers of different colours, so that we can easily track them throughout the evolution of the flow, cf. figure 16. Depending on whether the lower dense layer advances faster or more slowly than the upper layer, we observe different mixing patterns.

Figure 16.

Temporal evolution of Lagrangian mixing between upper and lower layer fluids. (a) Run 9 ($R_{\rho }=1.25$, $R_h=1$): the lower layer fluid propagates faster and forms the head of the current. Significant mixing occurs in the wake of the head. (b) Run 2 ($R_{\rho }=1.25$, $R_h=0.1$): the upper layer fluid propagates faster and forms the current head. Relatively little mixing occurs between upper and lower layer fluids.

When the lower layer propagates faster, it rapidly forms a head after the gate is removed. The fluid in the head is carried upward by the ambient counterflow, so that it mixes with both the upper dense layer and the ambient fluid through the action of the interfacial Kelvin–Helmholtz vortices. The fluid within the head is constantly being replenished by the near-wall layer of the current, which moves faster than the head itself. It also entrains upper-layer fluid in a wedge-like shape behind the head, so that the entire head region becomes vigorously mixed, as shown in figure 16(a).

When the upper dense layer advances more rapidly than the lower layer, it surges ahead of the lower layer and forms the head of the current, cf. figure 16(b). Very little lower layer fluid enters the head under these conditions, and the two layers mix much less than in the flow of figure 16(a).

Previous studies have shown that the interfacial instabilities in stratified flow can help to predict the mixing properties between different layers (Balasubramanian & Zhong Reference Balasubramanian and Zhong2018; Martin, Negretti & Hopfinger Reference Martin, Negretti and Hopfinger2019). Holmboe (Reference Holmboe1962) predicted Kelvin–Helmholtz instability and Holmboe instability at small and large Richardson numbers, respectively. The bulk Richardson number $J=g'\delta /({\rm \Delta} U)^2$ is defined, whereas Kelvin–Helmholtz instabilities can only occur when $J<0.07$. Here, $g'$ is the reduced gravity, $\delta ={\rm \Delta} U/(\partial U/\partial y)_{max}$ is the shear layer thickness and ${\rm \Delta} U$ is the velocity difference between the two layers or the current and the ambient fluid. Hazel (Reference Hazel1972) found that Holmboe instabilities exist when $\delta /\eta >2$, where $\eta ={\rm \Delta} \rho /(\partial \rho /\partial y)_{max}$ is the density layer thickness, and ${\rm \Delta} \rho$ is the density difference. We have measured $J$ and $\delta /\eta$ from several profiles in different cases, which are presented in table 3.

Table 3.

Parameters $J$ and $\delta /\eta$ for different cases.

Table 3 shows that the bulk Richardson numbers at the interface of the upper or lower layer and ambient fluid $J_{U0}$ or $J_{L0}$ are less than 0.07 for all cases. Kelvin–Helmholtz instability is observed, as shown in figures 6 and 7. Note that for run 6, the upper and lower layers have similar front velocity, so a clear interface of the lower layer and ambient fluid does not exist. However, for the interface of the upper and lower layers, the bulk Richardson number $J_{UL}$ is always larger than 0.07. In most of the cases $\delta _{UL}/\eta _{UL}$ is higher than 2, so that Holmboe instability occurs. In run 11, the large density ratio decreases the shear layer thickness, resulting in a small value of $\delta _{UL}/\eta _{UL}$, which suppresses the Holmboe instability.

In order to quantify the mixing of upper and lower layer fluids as a function of $R_{\rho }$ and $R_h$, we follow a computational approach similar to that of Tokyay, Constantinescu & Meiburg (Reference Tokyay, Constantinescu and Meiburg2011), and evaluate the normalised volume $V_m$ within which the concentrations of the upper and lower layer fluids both exceed a threshold value $c_t$:

(3.32)\begin{gather} V_m=\frac{1}{L_s\times h_U\times W}\int^H_0\int^L_0 \int^W_0\gamma_{UL}\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.33)\begin{gather}\gamma_{UL}=\left\{\begin{array}{@{}ll} 1 & c_U>c_t\ {\rm and}\ c_L>c_t,\\ 0 & {\rm otherwise.} \end{array}\right. \end{gather}

Figure 17 shows the temporal evolution of $V_m$ for different values of $R_{\rho }$, $R_h$ and $c_t=0.02$. It demonstrates that $R_{\rho }$ has a non-monotonic influence on the time history of $V_m$, so that at least during some flow stages mixing is most pronounced for intermediate values of $R_{\rho }$. These complex dynamics result from the competing effects of density stratification: on the one hand, strong stratification tends to suppress mixing; on the other hand, it increases the velocity difference between the layers, and thereby enhances the interfacial shear, which tends to promote mixing. At the same time, a larger velocity difference between the layers results in a head region that contains very little upper layer fluid, which in turn reduces mixing.

Figure 17.

Time development of the mixed volume $V_m$ for the height ratio $R_h=1$ with different density ratios $R_{\rho }$ (i.e. runs 9–11); and for the density ratio $R_{\rho }=1.25$ with different height ratios $R_h$ (i.e. runs 2, 5 and 9).

Figure 17 also indicates that a larger height ratio $R_h$ uniformly tends to promote mixing, as it allows the dense fluid layers to release more potential energy, and to generate a more vigorous flow.

Similar to our approach in § 3.3, we evaluate the mixed volume $V_m$ at $t=20$ for different cases to show the quantitative dependence on the density ratio $R_{\rho }$ and height ratio $R_h$. Figure 18(a) presents $V_m$ as a function of $R_h$ for different $R_{\rho }$. Here $V_m$ increases with $R_h$, but is significantly reduced for large values of $R_{\rho }$. Figure 18(b) shows that for $R^{-0.25}_{\rho } R^{0.5}_h$ as the scaling parameter, the raw data can be well fitted ($R^2=0.962$) by a straight line of the form

(3.34)\begin{equation} V_m=1.3R^{{-}0.25}_{\rho} R^{0.5}_h. \end{equation}

This equation is consistent with the fact that for $R_h=0$ no mixed fluid is being generated. Although a larger $R_h$ results in more mixing, an increase in $R_{\rho }$ reduces the mixed volume $V_m$.

Figure 18.

The mixed volume $V_m$ for different $R_{\rho }$ and $R_h$.

As the approach of Tokyay et al. (Reference Tokyay, Constantinescu and Meiburg2011) is affected by the concentration threshold, we also present and compare the results of two alternate approaches for quantifying the mixing of the upper and lower layers. The first is based on the framework of Winters et al. (Reference Winters, Lombard, Riley and D'Asaro1995). In the closed system of our configuration, the increase in the background potential energy $E_b$ results only from mixing, so that the evolution of $E_b$ is a direct measure of the mixing. The background potential energy $E_b$ is defined as

(3.35)\begin{equation} E_b = \int^W_0\int^{H}_0\int^L_0 (c_U+R_Lc_L)(y_*-h_L)\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{equation}

where $y_*$ is the vertical position in the state of the minimum potential energy. Note that here we also choose the initial top boundary of the lower dense layer $y = h_L$ as our reference level.

Figure 19 shows the time history of the normalised background potential energy $(E_b-E_{b,init})/E_{pU,init}$ for different cases. Here $E_{b,init}$ is the initial background potential energy. The energy $E_b$ increases with time, which implies the presence of the irreversible mixing. However, different from the conclusion presented by figure 17, $E_b$ monotonically increases with the density ratio $R_{\rho }$. This may be due to the fact that the density of the lower layer directly affects the calculation of the background potential energy. On the other hand, the evolution of $E_b$ quantitatively presents the mixing not only between the upper and lower layers but also between the two layers and ambient fluid.

Figure 19.

Time history of the normalised background potential energy $(E_b-E_{b,init})/E_{pU,init}$ for the height ratio $R_h=1$ with different density ratios $R_{\rho }$ (i.e. runs 9–11); and for the density ratio $R_{\rho }=1.25$ with different height ratios $R_h$ (i.e. runs 2, 5 and 9).

As a second approach, we first calculate the volumes that the upper layer, lower layer and the two-layer current occupy (García Reference García1993). They are defined as $V_U$, $V_L$ and $V_{UL}$:

(3.36)\begin{gather} V_U=\frac{\left(\displaystyle\int^W_0\int^{H}_0 \int^L_0 c_U\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z\right)^2}{\displaystyle\int^W_0\int^{H}_0 \int^L_0 c_U^2\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z}, \end{gather}

(3.37)\begin{gather}V_L=\frac{\left(\displaystyle\int^W_0\int^{H}_0\int^L_0 c_L\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z\right)^2}{\displaystyle\int^W_0\int^{H}_0 \int^L_0 c_L^2\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z}, \end{gather}

(3.38)\begin{gather}V_{UL}=\frac{\left(\displaystyle\int^W_0\int^{H}_0\int^L_0 c_U+c_L\,\mathrm{d}x\,\mathrm{d}\,y\mathrm{d}z\right)^2}{\displaystyle\int^W_0\int^{H}_0\int^L_0 (c_U+c_L)^2\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z}. \end{gather}

Then, the normalised mixed volume $V_{m,G}$ can be obtained as

(3.39)\begin{equation} V_{m,G} = \frac{V_U+V_L-V_{UL}}{L_s\times h_U\times W} .\end{equation}

Figure 20 shows the time history of the normalised mixed volume $V_{m,G}$ for different cases. The values of $V_{m,G}$ are smaller than $V_m$ shown in figure 17, which indicates that this method has a larger concentration threshold to define the boundary of the currents. At the same time, $V_{m,G}$ exhibits a monotonic decrease with the increase of the density ratio $R_\rho$. However, the values of $V_m$ show the strongest mixing occurs for intermediate $R_\rho$, as larger values of $R_\rho$ cause more low-concentration mixing.

Figure 20.

Time evolution of the normalised mixed volume $V_{m,G}$ for the height ratio $R_h=1$ with different density ratios $R_{\rho }$ (i.e. runs 9–11); and for the density ratio $R_{\rho }=1.25$ with different height ratios $R_h$ (i.e. runs 2, 5 and 9).

3.5. Entrainment in two-layer gravity currents

As an essential feature, propagating gravity currents entrain ambient fluid, thus increasing their volume. The entrainment dynamics of two-layer currents are more complex than for single-layer currents, because they involve the interfaces of both layers with the ambient fluid. Following Ottolenghi et al. (Reference Ottolenghi, Adduce, Inghilesi, Armenio and Roman2016), we define the entrainment velocity as the volume flux per unit area of the ambient fluid across the interface with the gravity currents:

(3.40)\begin{equation} U_e(t)=\frac{Q(t)}{0.5[S(t)+S(t-{\rm \Delta} t)]}. \end{equation}

Here $S(t)=W d_e(t)$ denotes the interfacial area at time $t$, where we define $d_e(t)$ as the rightmost location in the flow field with $c_U=0.02$ or $c_L=0.02$. Before the ambient counter-current reaches the left wall, $d_e(t)$ is the distance between this location and the front of the left-propagating ambient counter-current. Here $Q(t)$ is the instantaneous volume flux across the interface:

(3.41)\begin{equation} Q(t)=\frac{V(t)-V(t-{\rm \Delta} t)}{{\rm \Delta} t}, \end{equation}

where the volume of the two-layer gravity current is obtained as

(3.42)\begin{gather} V(t)=\int^W_0\int^H_0\int^L_0\gamma\,\mathrm{d}x\,\mathrm{d}y\,\mathrm{d}z, \end{gather}

(3.43)\begin{gather}\gamma=\left\{\begin{array}{@{}ll} 1 & {c_U>c_t\ \mathrm{or}\ c_L>c_t,}\\ 0 & \mathrm{otherwise.} \end{array}\right. \end{gather}

As a threshold value we take $c_t=0.02$, consistent with Ottolenghi et al. (Reference Ottolenghi, Adduce, Inghilesi, Armenio and Roman2016). The instantaneous entrainment parameter $E(t)$ of the current is then obtained as the ratio of the entrainment velocity to the front velocity of the two-layer gravity current relative to the ambient fluid:

(3.44)\begin{equation} E(t)=\frac{U_e(t)}{2U_f(t)}. \end{equation}

Here, we assume that the ambient fluid flows to the left with approximately $U_f(t)$, so that the velocity difference between the current and the ambient is $2U_f(t)$. The time-averaged entrainment behaviour of the flow is characterised by the bulk parameters:

(3.45)$$\begin{gather} \bar{Q}(t)=\frac{V(t)-V(0)}{t}, \end{gather}$$

(3.46)$$\begin{gather}\bar{U}_e(t)=\frac{\bar{Q}(t)}{0.5[S(t)+S(0)]}, \end{gather}$$

(3.47)$$\begin{gather}\bar{U}_f(t)=\frac{X_f(t)-X_f(0)}{t}, \end{gather}$$

(3.48)$$\begin{gather}\bar{E}(t)=\frac{\bar{U}_e(t)}{2\bar{U}_f(t)}. \end{gather}$$

Figure 21 compares the entrainment dynamics of single- (run 8 for $R_{\rho }=1$ and $R_h=1$) and two-layer (run 10 for $R_{\rho }=2$ and $R_h=1$) gravity currents. Figure 21(a,b) show the bulk and instantaneous entrainment fluxes, $\bar {Q}$ and $Q$. Early on the dense fluid collapses and forms a well-defined head. Kelvin–Helmholtz billows evolve along the upper boundary and entrain ambient fluid, so that the bulk entrainment flux $\bar {Q}$ increases with time. After the ambient counter-current reaches the left wall of the tank at $t \approx 12$, $\bar {Q}$ levels off, with a larger value for the two-layer case. As compared with the bulk entrainment flux, the instantaneous flux $Q$ exhibits more complex behaviour characterised by pronounced peaks. To establish the reasons for these peaks, we turn to the streamwise vorticity field averaged over the spanwise direction, cf. figure 22. Consistent with earlier work by Ottolenghi et al. (Reference Ottolenghi, Adduce, Inghilesi, Armenio and Roman2016), we find that the Kelvin–Helmholtz billows trap the most ambient fluid when they reach their maximum size and intensity, resulting in the formation of instantaneous peaks in $Q$, cf. figure 22(a–d). The billows increase their size before the peak occurs, and they break down after that. Although the instantaneous fluxes $Q$ evolve qualitatively similarly for the single- and two-layer cases, $Q$ reaches a higher peak value for the two-layer case, cf. figure 22(e,f).

Figure 21.

The time evolution of bulk and instantaneous entrainment properties for single- (run 8 for $R_{\rho }=1$ and $R_h=1$, blue lines, right column) and two-layer (run 10 for $R_{\rho }=2$ and $R_h=1$, black lines, left column) gravity currents: (a,b) bulk and instant entrainment fluxes $\bar {Q}$ and $Q$; (c,d) bulk and instantaneous entrainment velocities $\bar {U}_e$ and $U_e$; (e,f) bulk and instantaneous entrainment parameters $\bar {E}$ and $E$.

Figure 22.

The dimensionless vorticity fields $\omega _{xy}$ of single- (run 8 for $R_{\rho }=1$ and $R_h=1$) and two-layer (run 10 for $R_{\rho }=2$ and $R_h=1$) gravity currents: (a,c,e) for the two-layer case; (b,d,f) for the single-layer case.

Figure 21(c,d) show the time evolution of the bulk and instantaneous entrainment velocities, $\bar {U}_e$ and $U_e$. The high early values are related to the initial collapse and the formation of the head (He et al. Reference He, Zhao, Hu, Yu and Lin2018). After $t \approx 12$, $\bar {U}_e$ and $U_e$ decrease, because the tail region of the currents does not give rise to significant entrainment (Bhaganagar Reference Bhaganagar2017). This is also reflected in the time evolution of the bulk and instantaneous entrainment parameters, $\bar {E}$ and $E$, cf. figure 21(e,f). For both single- and two-layer flows we observe $\bar {E}$ and $E$ of $O(10^{-2})$, which is consistent with earlier investigations (Ottolenghi et al. Reference Ottolenghi, Adduce, Inghilesi, Armenio and Roman2016; He et al. Reference He, Zhao, Hu, Yu and Lin2018, Reference He, Zhao, Zhu and Hu2019).

Figure 23 shows the influence of the density ratio $R_{\rho }$ and the height ratio $R_h$ on the evolution of the bulk entrainment parameter $\bar {E}$ for two-layer gravity currents. Figure 23(a) demonstrates that $\bar {E}$ decreases for larger $R_{\rho }$, since stronger stratification tends to dampen the Kelvin–Helmholtz instability while causing a larger front velocity. The effects of the layer height ratio $R_h$ are analysed in figure 23(b). Until the left-propagating counter-current encounters the left wall, $R_h$ has only a minor influence on $\bar {E}$, because the entrainment is dominated by the lower-layer current. After the reflection of the counter-current from the left wall, however, it is evident that larger $R_h$-values enhance entrainment, so that $\bar {E}$ increases.

Figure 23.

The evolution of bulk entrainment parameter $\bar {E}$ for two-layer gravity currents as a function of front location $X_f$ with different $R_{\rho }$ and $R_h$: (a) $R_h=1$ with different $R_{\rho }$, i.e. runs 9–11; (b) $R_{\rho }=1.25$ with different $R_h$, i.e. runs 5, 9 and 12.

3.6. Constant excess weight

As mentioned in § 2.1, so far we have employed the thickness and density of the upper layer to scale the simulations. Consequently, the total excess weight in the initial condition has not been held constant for the different cases. In this section, we keep the total excess weight constant and run several cases with different density and height ratios of the upper and lower layers.

We introduce characteristic length and velocity scales $\hat {H}/2$ and $\hat {u}_{b,A}= \sqrt {\hat {g}\hat {H}(\hat {\rho }_A-\hat {\rho }_0)/2\hat {\rho }_0}$ to non-dimensionalise the governing equations. Here $\hat {\rho }_A=(\hat {\rho }_U \hat {h}_U+\hat {\rho }_L \hat {h}_L)/\hat {H}$ is the average density of the lock fluid. The non-dimensional (2.10)–(2.12) can be rewritten as

(3.49)\begin{gather} \frac{\partial u_i}{\partial t}+u_j\frac{\partial u_i}{\partial x_j}={-}\frac{\partial p}{\partial x_i}+\frac{1}{Re_A} \frac{\partial^2 u_i}{\partial x_j\partial x_j}+(R_Uc_U+R_Lc_L)\,{\rm e}^{g}_i, \end{gather}

(3.50)\begin{gather}\frac{\partial c_U}{\partial t}+u_j\frac{\partial c_U}{\partial x_j}= \frac{1}{Pe}_A\frac{\partial^2 c_U}{\partial x_j\partial x_j}, \end{gather}

(3.51)\begin{gather}\frac{\partial c_L}{\partial t}+u_j\frac{\partial c_L}{\partial x_j}=\frac{1}{Pe}_A\frac{\partial^2 c_L}{\partial x_j\partial x_j}. \end{gather}

The dimensionless parameters are the Reynolds number ${Re}_A$,

(3.52)\begin{equation} {Re}_A=\frac{\hat{u}_{b,A}\hat{H}}{2\hat{\nu}}, \end{equation}

the Péclet number ${Pe}_A$,

(3.53)\begin{equation} {Pe}_A=\frac{\hat{u}_{b,A}\hat{H}}{2\hat{\kappa}}, \end{equation}

and the density parameters for the upper layer $R_U$ and lower layer $R_L$,

(3.54)\begin{gather} R_U=\frac{\hat{\rho}_U-\hat{\rho}_0}{\hat{\rho}_A-\hat{\rho}_0}, \end{gather}

(3.55)\begin{gather}R_L=\frac{\hat{\rho}_L-\hat{\rho}_0}{\hat{\rho}_A-\hat{\rho}_0}. \end{gather}

The initial and boundary conditions are as described in § 2.2. The parameters of the simulations are listed in table 4. All cases have the same averaged density of the two-layer lock fluids.

Table 4.

Simulation cases and parameters.

Figure 24 shows the evolution of the two-layer gravity currents with different density ratio $R_{\rho }$ and height ratio $R_h$. Although having different stratification, the two-layer currents propagate at comparable velocities, due to the identical initial averaged density $\rho _A$. Figure 24(a–c) compare three cases with constant height ratio $R_h=1$ but different density ratio $R_{\rho }$, i.e. runs 15–17. With increasing $R_{\rho }$, the upper layer slows down and the main body of the currents becomes thinner. Figure 24(d–f) present the flows with identical density ratio $R_{\rho }=1.5$ and different height ratio, i.e. runs 16, 18 and 19. When increasing $R_h$, the lower layer has a larger volume but smaller density. For a small height ratio $R_h=0.25$, the fronts of the upper and lower layers have similar velocities. For larger height ratios ($R_h=1$ and 4), the lower layer propagates faster than the upper layer.

Figure 24.

Instantaneous concentration field, along with the concentration isosurfaces $c_U=0.5$ and $c_L=0.5$ for both upper and lower layers at $t=30$: (a–c) runs 15–17 for $R_h=1$ and $R_{\rho }=1$, 1.5 and 3; (d–f) runs 18, 16 and 19 for $R_{\rho }=1.5$ and $R_h=0.25$, 1 and 4.