2.1. Free-surface hydraulic jumps

For single-layer flow in a horizontal channel of constant width, $W$, the basic parameters are the flow depth, $y$, the volumetric flow rate per unit width, $q$, the fluid density, $\rho$, and the gravitational acceleration, $g$. It is customary in open channel hydraulics (see Henderson (Reference Henderson1966), § 2.3) to evaluate (2.1) using the standard hydraulic assumptions, and then non-dimensionalise by $\rho g W y_{c}^{2}$, where the critical depth, $y_{c} = (q^{2}/g)^{1/3}$, to obtain the non-dimensional, single-layer momentum function

(2.3a)\begin{equation} M_{S} = \frac{{y^{\prime}}^{2}}{2} + \frac{1}{y^{\prime}} = {y^{\prime}}^{2} \left( \frac{1}{2} + {\textit{Fr}}^{2} \right), \end{equation}

where $y^{\prime } = y/y_{c}$, and the Froude number for single-layer flow

(2.3b)\begin{equation} {\textit{Fr}}^{2} \equiv \left( \frac{q^{2}}{gy^{3}} \right) = {y^{\prime}}^{- 3}. \end{equation}

Note that, whenever we refer to a Froude number, we refer to the squared quantity, as in (2.3).

A free-surface hydraulic jump is a rapid transition from supercritical upstream flow, ${\textit {Fr}}_{U}^{2} > 1$, to subcritical downstream flow, ${\textit {Fr}}_{D}^{2} < 1$, where the subscripts $_{U}$ and $_{D}$ refer to the conjugate conditions immediately upstream and downstream of the jump.

Assuming negligible friction losses over the length of the jump, and equating the momentum function upstream and downstream of the jump, yields (see Henderson Reference Henderson1966)

(2.4)\begin{equation} \frac{y_D}{y_U}=\frac{1}{2}\left(\sqrt{1+8{Fr}_U^{2}}-1)\right). \end{equation}

The dimensionless specific energy (Bernoulli constant) for a single-layer flow is given by

(2.5)\begin{equation} E_{S} = y^{\prime}\left( 1 + \frac{{\textit{Fr}}^{2}}{2} \right). \end{equation}

The loss of specific energy across a free-surface hydraulic jump (see Henderson Reference Henderson1966) is

(2.6)\begin{equation} \Delta E_{J} \equiv E_{{SU}} - E_{{SD}} = \frac{(y_{D}^{\prime} - y_{U}^{\prime})^{3}}{4y_{D}^{\prime}y_{U}^{\prime}}. \end{equation}

Upstream and downstream of a free-surface hydraulic jump (2.1)–(2.3) give

(2.7)\begin{equation} \frac{{\rm d} M_{S}}{{\rm d} x^{\prime}} ={-} \frac{f}{8} \frac{y}{R_h} {\textit{Fr}}^{2} y^{\prime}, \end{equation}

where $x^{\prime } = x / y_{c}$, the hydraulic radius, $R_h \equiv A/P = Wy / (W + 2y)$, where $A$ is the cross-sectional area of the channel and $P$ is its wetted perimeter. Methods for determining the Darcy–Weisbach friction factor, $f$, are given in Chow (Reference Chow1959) and Finnemore & Franzini (Reference Finnemore and Franzini2002).

The above concepts are illustrated in figure 2(b) by plotting $M_{S}$ and $E_{S}$ vs ${\textit {Fr}}^{2}$ for the flow depicted in figure 2(a). In this flow $y_{D} / y_{U} \approx 2$, and (2.3a) and (2.4) give the conjugate states ${\textit {Fr}}_{U}^{2} = 3$ and ${\textit {Fr}}_{D}^{2} = 3/8$. Across the jump momentum is assumed constant, and (2.6) gives $\Delta E_{J}=0.087$. Downstream of the jump, between D and F, friction results in a gradual decrease in $M_{S}$, in accordance with (2.7).

While (2.4) allows us to calculate the relationship between upstream and downstream conditions, we must emphasise a point made by Henderson (Reference Henderson1966, p. 69) that is central to the present study:

Consider the flow depicted in figure 2(a) where the jump is located at a transition in bed slope (a transitional jump). If the height of a downstream weir (not visible) were lowered, so that the flow depth and momentum function at $D$ were reduced, then the momentum function at $D$ would be less than that at $U$. To redress this imbalance the position of the jump would move downstream (a free jump), exposing a reach of supercritical flow that, due to friction, would reduce the momentum so that that the flow conditions upstream and downstream of the jump were again conjugate to each other. On the other hand, if the downstream depth were increased the position of the jump would move upstream, creating a drowned hydraulic jump (see Chow Reference Chow1959), and the analysis would need to be modified to account for the sloping bed upstream of $U$.

2.2. Momentum and energy functions for two-layer flows

Now we follow the procedure presented above to derive momentum and energy functions for two-layer flows. The experiment depicted in figure 3, will be used to provide context. For two-layer flow in a channel of constant width, $W$, the basic flow parameters are: the layer depths, $y_{i}$, where the subscripts $i = 1, 2$ refer to the upper and lower layers, respectively; the volumetric flow rate per unit width of each layer, $q_{i}$; the flow rate ratio, $r=q_2/q$, where $q = q_1+q_2$; and the reduced gravitational acceleration, $g^{\prime } = \varepsilon g$, where $\varepsilon = \left (\rho _{2} - \rho _{1} \right )/\rho _{2}$. In the present study we assume $\varepsilon \ll 1$. The total flow depth, $Y = y_{1} +$ $y_{2} + h$, where $h$ is the local height of the sill.

For two-layer flows in a horizontal channel of constant width (2.1) becomes

(2.8) \begin{equation} S = \int_{0}^{y_2} ( P_2 + \rho_2 u_2^{2} ) W \,{\rm d} z + \int_{y_2}^{Y} (P_1 + \rho_1 u_1^{2}) W \,{\rm d} z. \end{equation}

To evaluate (2.8), Chu & Baddour (Reference Chu and Baddour1977) and Wood & Simpson (Reference Wood and Simpson1984) assumed that the pressure is hydrostatic, and that within each layer the density is constant and the velocity is cross-sectionally uniform. After dividing by $\rho g^{\prime } W Y^{2}$, they obtained to $O(\varepsilon )$

(2.9)\begin{equation} S_{T} = \frac{1}{2\varepsilon} + {y^{\prime}_2}^{2} \left(\frac{1}{2}+F_2^{2}\right) + {y_1^{\prime}}^{2} F_1^{2}, \end{equation}

where $y_i^{\prime }=y_i/Y$. For single-layer flows there exists a critical depth, $y_c$, which we used for non-dimensionalisation in § 2.1. No simple critical depth exists for two-layer flows, and we use the total depth, $Y$, for the non-dimensionalisation. The densimetric Froude number

(2.10)\begin{equation} F_{i}^{2} = \frac{q_{i}^{2}}{g^{\prime}y_{i}^{3}}. \end{equation}

Note again, that whenever we refer to a Froude number, we refer to the squared quantity. Note also, that the composite Froude number (Armi Reference Armi1986),

(2.11)\begin{equation} G^{2} = F_{1}^{2} + F_{2}^{2} - \varepsilon F_{1}^{2}F_{2}^{2}, \end{equation}

rather than the densimetric Froude number, is commonly used to describe the criticality of two-layer flows (see Appendix A for details).

In density jumps the assumptions of constant density and uniform velocity within each layer are not satisfied. Wilkinson & Wood (Reference Wilkinson and Wood1971) and others have relaxed these assumptions by using correction factors in their analyses of density jumps. However, the internal hydraulic jumps that we investigate in the present paper cause far less disruption to the flow than density jumps, and we do not incorporate correction factors into our analysis of the hydraulics of two-layer flows. This allows us to focus on understanding the processes that govern the entrainment and mixing associated with internal hydraulic jumps.

As it stands (2.9) is not particularly useful, since the first term on the right-hand side is $O(\varepsilon ^{-1})$ times as large as the other terms. Following Chu & Baddour (Reference Chu and Baddour1977) and Wood & Simpson (Reference Wood and Simpson1984), we eliminate this term by assuming that the upper layer energy, $E_{1} = \rho _{1}gY + \rho _{1} u_{1}^{2} / 2$, is constant. The resulting non-dimensional momentum function for two-layer flows to $O\left (\varepsilon \right )$ is

(2.12)\begin{equation} M_{T} \equiv S_{T} - {\frac{1}{2\varepsilon}\left( \frac{E_{1}}{\rho_{1}{gY}}\right)}^{2} = {y_{2}^{\prime}}^{2}\left( \frac{1}{2} + F_{2}^{2} \right) + \frac{1}{2}(y_{1}^{\prime} - y_{2}^{\prime})y_{1}^{\prime}F_{1}^{2}. \end{equation}

To $O\left ( \varepsilon \right )$ (2.12) is the same as those obtained by Chu & Baddour (Reference Chu and Baddour1977) and Wood & Simpson (Reference Wood and Simpson1984). Note that if the upper layer is passive, i.e. if $F_{1}^{2} \ll F_{2}^{2}$, (2.12) has the same form as (2.3a), its single-layer counterpart.

While our focus is on variations in the momentum function, since they determine the position of internal hydraulic jumps, it is also informative to consider variations in the two-layer energy function, defined by Baddour & Abbink (Reference Baddour and Abbink1983) and others, as

(2.13)\begin{equation} E_{T} \equiv \frac{E_{2} - E_{1}}{\rho_{2}g^{\prime}Y} = y_{2}^{\prime} \left( 1 + \frac{1}{2}F_{2}^{2} \right) - \frac{1}{2}{y_{1}^{\prime}F}_{1}^{2}. \end{equation}

As in the case of the momentum function, if the upper layer is passive, i.e. when $F_{1}^{2} \ll F_{2}^{2}$, (2.13) has the same form as (2.5), its single-layer counterpart.

2.3. Internal hydraulic jumps in barotropically driven two-layer flows

We study two-layer flow in a horizontal, rectangular channel, as depicted in figure 3. An internally supercritical flow downstream of the crest of a sill is followed by an internal hydraulic jump that transitions to an internally subcritical flow. We model a barotropically driven two-layer flow by installing a downstream width contraction, which imposes an approximately uniform velocity profile at the downstream end of the channel (see Appendix A for details). The uniform downstream velocity profile eliminates the closure problem recognised by Yih & Guha (Reference Yih and Guha1955), and allows us to refine the theory of internal hydraulic jumps.

Here, we derive the appropriate momentum and energy functions needed to analyse this configuration. Wood (Reference Wood1968) and Armi (Reference Armi1986) show that, to $O\left ( \varepsilon \right )$

(2.14)\begin{equation} u_{1o} = u_{2o} = \frac{q}{Y_{o}}, \end{equation}

where the subscript ‘$o$’ designates conditions at the end of the test section; i.e. at the start of the downstream contraction. Substituting (2.14) into (2.11), yields

(2.15)\begin{equation} G_{o}^{2} = \frac{q^{2}}{g^{\prime}r(1 - r)Y_{o}^{3}}, \end{equation}

where the two-dimensional flow rate, $q = q_{1} + q_{2}$; the total depth, $Y_{0} = y_{1o} + y_{2o}$, and the flow rate ratio

(2.16)\begin{equation} r = \frac{q_{2}}{q}. \end{equation}

The present study investigates flows with $G_{0}^{2} < 1$. At low flow rates, the flow is internally subcritical throughout the channel with only a slight depression in the interface level over the sill. This case is not of interest in the present study, since there is no internal hydraulic jump. At sufficiently higher flow rates the flow will become internally supercritical on the lee face of the sill; in such flows an internal hydraulic jump will form between the crest of the sill and the downstream contraction. Lawrence (Reference Lawrence1993) has shown that $G_{0}^{2}$ and $r$, in conjunction with the non-dimensional obstacle height, $\beta _m = h_m/Y_{0}$, where $h_m$ is the maximum height of the obstacle, determine which of these cases occurs. The values of $G_{0}^{2},\ r\ \text {and} \beta _m$ for the experiments performed in the present study are given in table 1.

Table 1.

Experimental data. Note that all dimensional quantities are in cgs units. The values given for drowned jumps at the end of the sill (subscript ‘$E$’) are calculated assuming there is no drowned jump and written in italics; $M_{E}$ was not calculated for Exps. 12 and 13 because the flow over the sill was subject to substantial non-hydrostatic effects (Zhu & Lawrence Reference Zhu and Lawrence1998).

Under the assumption of uniform flow at the downstream end of the channel, $y_{2o} = r$, and (2.12) simplifies to

(2.17)\begin{equation} M_{To} = \tfrac{1}{2}\{ r^{2} + r(1 - r)G_{0}^{2} \}. \end{equation}

To best illustrate the properties of internal hydraulic jumps, we define the non-dimensional two-layer momentum function

(2.18)\begin{align} M \equiv M_{T} - M_{To} = \frac{1}{2}\eta\left( 2r + \eta \right) + r(1 - r)G_{0}^{2} \left\{ \frac{r^{2}}{r + \eta} + \frac{{\left( \dfrac{1}{2} - r - \eta \right) \left( 1 - r \right)}^{2}}{\left( 1 - r - \eta \right)^{2}} - \frac{1}{2} \right\}, \end{align}

where $\eta = y^{\prime }_{2} - r$.

Applying (2.2) to gradually varying two-layer flow in a horizontal channel yields

(2.19)\begin{equation} \frac{{\rm d} M}{{\rm d} x^{\prime}} ={-} \frac{f_{1}}{8} \left( \frac{y_1}{R_{h_1}} \right) F_{1}^{2} y_1^{\prime} - \frac{f_{2}}{8} \left( \frac{y_2}{R_{h_2}} \right) F_{2}^{2} y_2^{\prime}, \end{equation}

where $f_{1}$ and $R_{h_1} = W/2$, and $f_{2}$ and $R_{h_2} = Wy_2 / (W + 2y_2)$, are the friction factors and hydraulic radii for the upper and lower layers, respectively. Equation (2.19) is analogous to (2.7), the corresponding single-layer result. In our experiments the walls of the channel can be assumed to be smooth, in which case

(2.20)\begin{equation} f_i = 0.223 {\textit{Re}}_{h_i}^{{-}1/4}, \end{equation}

where the hydraulic Reynolds number, ${\textit {Re}}_{h_i} = u_i R_{h_i}/\nu$, $i = 1, 2$ (see Chow Reference Chow1959). Note that $f_1$ and $f_2$ are the friction factors due to shear on the bed and sidewalls of the channel; they are not interfacial friction factors. Interfacial friction does not play a role in the calculation of $M$.

Following our approach for momentum, we define the non-dimensional two-layer energy function

(2.21)\begin{equation} E \equiv E_{T} - E_{To} = \eta + \frac{1}{2}r\left( 1 - r \right)G_{0}^{2} \left\{ \left\lbrack \frac{r}{r + \eta} \right\rbrack^{2} - \left\lbrack \frac{(1 - r)}{(1 - r - \eta)} \right\rbrack^{2} \right\}, \end{equation}

see Lawrence (Reference Lawrence1993). Note that, for convenience, we have defined the two-layer momentum and energy functions so that, at the downstream end of the channel where $\eta = 0$, (2.18) and (2.21) give $M = 0$ and $E = 0$, respectively.

The above concepts are illustrated by the two-layer flow examined in figure 3. This flow has been visualised in figure 3(a) by dyeing the lower layer red and the upper layer blue, so that mixing between the layers appears purple. Note that mixed fluid is present in a shear layer upstream of the jump, as well as in the jump itself. This mixing can be ignored for the moment, but will be examined in detail in § 4. A definition sketch for the flow is presented in figure 3(b). The variation of $M$ and $E$ with $G^{2}$ is presented in figure 3(c). While there are differences, this plot is very similar to its single-layer counterpart presented in figure 2(b), as are the basic causes of variation in the momentum and energy.

Let us consider the changes in $M$ and $E$ from the end of the sill ($E$) to end of the test section ($O$). From $E$ until the start of the jump ($U$) the flow is internally supercritical with an active lower layer, i.e. $F_2^{2} \gg F_1^{2}$. The values of $M$ and $E$ gradually decrease due to friction on the bed and sidewalls of the channel. From $U$ to the downstream end of the jump ($D$) momentum loss is negligible, but there is a considerable loss of energy. In the internally subcritical reach from $D$ to $O$, $M$ and $E$ gradually decrease, as in the shear layer upstream of the jump, but the rate of decrease is less than in the shear layer, since the lower layer velocity is less, figure 3(b).

Hydraulic jumps can form: downstream of the obstacle (free jumps); between the crest and downstream end of the sill (drowned jumps); or the start of the jump may occur at the end of the sill (transitional jumps). The flow of Guglielmini (Reference Guglielmini1697), shown in figure 2, is an example of a transitional free-surface hydraulic jump. For a transitional jump to form, $M_{E}$, the flow's momentum at the end of the sill, should match $M_{f}$, the loss of momentum due to friction on the sidewalls and bed of the flume in the internally subcritical flow between the end of the sill and the end of the test section. If the hydraulic assumptions hold, $M_{E}$ can be estimated using the approach outlined in Lawrence (Reference Lawrence1993) and $M_{f}$ can be estimated using (2.19). The jump type can be predicted according to the following:

(2.22)\begin{equation} \text{If} \quad \begin{cases} M_E > M_{f} & \text{a free jump occurs,}\\ M_E \approx M_{f} & \text{a transitional jump occurs,}\\ M_E < M_{f} & \text{a drowned jump occurs.} \end{cases} \end{equation}

While $M_{E}$ and $M_{f}$ are small quantities that are difficult to evaluate experimentally, (2.22) serves as a useful guide to the location of internal hydraulic jumps.

3.1. Series of experiments to verify two-layer hydraulic theory (Exps. 1–5)

The Series A experiments were performed with $h_m = 8.0\,\mathrm {cm}$, $q_{1} = 190$, $q_{2} = 95\,{\rm cm}^{2}\,{\rm s}^{-1}$ and $g^{\prime } \approx 18\,{\rm cm}\,{\rm s}^{2}$ (see table 1) The width of the downstream contraction was set at 1.4 cm for Exp. 1 and increased to 1.6, 1.8, 2.0 and 2.2 cm for Exps. 2–5, respectively. The upstream flow rate ratio was fixed at $r = 0.33$, and the other governing non-dimensional parameters, $G_{0}^{2}$ and $\beta _m$, varied as the free surface elevation dropped (see figure 5 and table 1). We use the theory presented in Lawrence (Reference Lawrence1993) to predict the momentum at the end of the sill, $M_{E}$, and integrate (2.19) to calculate $M_{f}$. In figure 5(a) the $M$ vs $G^{2}$ curves for $r=0.33$ are plotted for flows with a drowned jump (Exp. 1), a transitional jump (Exp. 3) and a free jump (Exp. 5). These curves are used in conjunction with photographs of the experiments (figure 5b–d) to explain the dynamics of the flow in each of these experiments.

Figure 5.

Momentum function plotted as a function of $G^{2}$ for Exps. 1, 3 and 5 together with photographs of these experiments. Solid circles indicate conditions at the end of the sill, open squares indicate conditions at the start of the jump, solid squares indicate conditions at the end of the jump and diamonds indicate conditions at the end of the channel. The experiments were performed on the same day and the upstream inflow rates and densities were constant (see table 1). In Exp. 1 the total depth, $Y = 44.1\,\mathrm {cm}$, the exit width of the downstream contraction, $W_{min} = 1.4\,\mathrm {cm}$ and a drowned jump formed over the lee face of the sill. In Exp. 3 $W_{min}$ was increased to 1.8 cm, causing the total depth to decrease to 38.1 cm, and a transitional jump formed at the end of the sill. In Exp. 5, $W_{min} = 2.2$, $Y = 33.7\,\mathrm {cm}$, and a free jump formed downstream of the sill. Red dye injected upstream at the density interface helps visualise the flow.

In Exp. 1 ($M_{E} = -0.003,\ M_{f} = 0.006$) a drowned internal hydraulic jump formed midway down the lee face of the sill, in accordance with (2.22). Note that in this experiment $M_{E} < 0$, indicating that a drowned jump would have formed even if there were no frictional momentum loss (see figure 5). A thin filament of red dye injected at the interface between the two layers at the entrance to the flume remained undisturbed until it reached the drowned jump. The dye was then entrained and mixed into the jump, highlighting the location of the jump, and the disturbed portion of the lower layer, which persisted until the end of the flume. A train of Kelvin–Helmholtz billows is observed underneath the nose of the jump, and the lower portion of the lower layer remained undisturbed. Experiments performed to investigate Kelvin–Helmholtz billowing and the entrainment and mixing that it causes are presented in § 4. Note that in all our experiments, the increase in the flow rate ratio caused by this entrainment and mixing is less than 10 % (see table 2), which does not warrant replotting the illustrative $M$ vs $G^{2}$ curves in figure 5. This observation is in contrast with the higher internal Froude number density jumps of Wilkinson & Wood (Reference Wilkinson and Wood1971) in which substantial mixing and entrainment occurred in the jet upstream of the jump and extended throughout the lower layer. The reasons for this difference are discussed in § 4.

Table 2.

Entrainment fluxes in Experiments 6–9.

In Exps. 2–5 both $M_{E}\ \text {and}\ M_{f}$ increased as the downstream contraction, $W_{min}$, was progressively opened decreasing the total depth of flow, $Y$ (table 1). However, $M_{E}$ increased more rapidly than $M_{f}$ and, as a consequence, the jump moved progressively further downstream. In Exp. 2 ($M_{E} = 0.007,\ M_{f} = 0.008$) the jump remained drowned, since $M_{E} < M_{f}$, but moved further down the lee face of the obstacle. Otherwise, Exp. 2 was very similar to Exp. 1. In Exp. 3 ($M_{E} = 0.011,\ M_{f} = 0.009$) a transitional jump formed at the end of the sill, since $M_{E} \approx M_{f}$. In this experiment a train of Kelvin–Helmholtz billows formed on the interface upstream of the jump (figure 5).

Free jumps formed in Exps. 4 and 5, respectively, since in both cases $M_{E}> M_{f}$ (see figure 5 and table 1). In these experiments the decrease in $M$ due to friction is greater than $M_{f}$, since $M_{f}$ is calculated assuming subcritical flow; whereas, in these experiments the rate of frictional loss in the supercritical flow between the end of the sill and the jump is greater, in accordance with (2.19). From the end of the sill until the jump, the lower layer depth increases gradually until the lower layer depth, $y_{2U}$, and the composite internal Froude number just upstream of the jump, $G_{U}^{2}$, are conjugate to the depth, $y_{2D}$, and the composite internal Froude number, $G_{D}^{2}$, downstream of the jump (figure 5). The free jumps in Exps. 5 and 6 are weaker than the drowned and transitional jumps (Exps. 2–4), because the composite Froude number downstream of the jump is higher.

In all of the Series A experiments, dye injected at the interface upstream of the sill was entrained into the jump, irrespective of the position of the jump. The jump consists of interfacial fluid mixed with lower layer fluid. No interfacial fluid made its way into the upper layer, nor did it enter the lower portion of the lower layer.

3.2. Series of experiments to investigate impact of jump position on entrainment and mixing (Exps. 6–9)

Series B was performed with $h_m = 8.0\,\mathrm {cm}$, $q_{1} = 217$, $q_{2} = 145\,{\rm cm}^{2}\,{\rm s}^{-1}$ and $g^{\prime } \approx 20\,{\rm cm}\,{\rm s}^{-2}$. The width of the downstream contraction was set at 1.2 cm for Exp. 6 and increased to 1.6, 1.8 and 2.2 cm for Exps. 7–9, respectively. In Series B, $r = 0.40$, whereas in Series A, $r = 0.33$. Otherwise, the primary difference is that in Series B velocity and density profiles were measured downstream of the jump (figure 6a–d) to quantify modifications to the flow caused by internal hydraulic jumps. The velocity profiles were not continuous, they were obtained by holding the propellor meter fixed for a period of 40 s at a series of vertical positions.

Figure 6.

(a–d) Photographs of Exps. 6–9 showing the effect of varying the total depth on the position of the jump, and the velocity and density profiles 5.5 m downstream of the crest of the sill. All the experiments were performed on the same day with the same flow rates and densities (see table 1). The conductivity probe and micro-propeller meter are visible just above the interface in (a).

In Exp. 6 a drowned jump formed just downstream of the crest of the obstacle (figure 6a), as expected since $M_{E} < M_{f}$. The density profile confirms the visual observation of entrainment of upper layer fluid into upper portion of the lower layer (figure 6a). The velocity profile is almost uniform, although a velocity deficit (wake), due to the stationary jump and the divergence of the upper layer over the lee face of the sill, is still evident 5.4 m downstream of the nose of the jump. This wake is likely to be less pronounced, but still present, in the downstream contraction which starts 7.7 m downstream of the nose of the jump. Similar wakes were observed in Exps. 7–9 (figure 6b–d).

As in the Series A experiments, when the downstream contraction was opened the water level dropped, and the jump moved progressively further downstream (figure 6a–d). In each case a different downstream density profile resulted. In the experiments with drowned jumps (Exps. 6–8, figure 6a–c) the only deviation from a two-layer downstream density profile was an approximately linear reduction in density in the upper portion of the lower layer. The reduction in density across this linear region increased as the jump moved downstream, consistent with the hypothesis that as the jump moves downstream more upper layer fluid is entrained into it. The density profile downstream of the free jump (Exp. 9, figure 6d) had a different form; it was broader and more symmetric, more like the hyperbolic tangent profiles characteristic of mixing layers. This suggests that most of the mixing occurs in the shear layer upstream of the free jump. These observations are consistent with those of Wilkinson & Wood (Reference Wilkinson and Wood1971), where the amount of entrainment and mixing was strongly impacted by jump position.

In all of the Series A and Series B experiments the jump location is consistent with the predictions of (2.22): i.e. when $M_{E} < M_{f}$, a drowned jump forms; when $M_{E} > M_{f}$ a free jump forms; and when $M_{E} \approx M_{f}$ a transitional jump forms near the end of the sill (figure 7). The sensitivity of the jump location to the value of $M_{E} - M_{f}$ is greater for free jumps than for drowned jumps as anticipated.

Figure 7.

Value of $M_{f} - M_{E}$ plotted as a function of the normalised position of our internal hydraulic jumps, $x_j/L_S$, where $x_j$ is the distance from the sill crest to the nose of the jump, and $L_S$ is the half-width of the sill. The square symbols represent flows with $r = 0.33$; the circular symbols represent flows with $r = 0.4$; the solid symbols represent drowned jumps; the grey symbol represents a transitional jump; and the open symbols represent free jumps.

4.1. Shear instabilities

Experiments 10 and 11 were performed to visualise the growth and fate of shear instabilities, and the turbulence and mixing associated with them, see figures 8 and 9. The parameters of Exp. 10 $(r = 0.33,\ G_{0}^{2} = 0.39$ and $\beta _m = 0.21)$ were intermediate between those of Exps. 3 and 4 (closer to Exp. 3), and a free jump formed downstream of the end of the sill. The parameters of Exp. 11 $(r = 0.40, G_{0}^{2} = 0.36$ and $\beta _m = 0.19)$ were intermediate between those of Exps. 8 and 9 (closer to Exp. 8), and a drowned jump formed near the end of the sill.

Figure 8.

(a) Photographs of Exp. 10 showing the growth of Kelvin–Helmholtz instabilities on the interface as the lower layer accelerates down the lee slope of the obstacle. The flow was illuminated with a sheet of laser light aligned with the centre of the flume. The laser light causes sodium fluorescein dissolved in the lower layer to fluoresce. (b) The longitudinal variation in the interfacial Richardson number (${\textit {Ri}}_{I}$) based on an estimated upstream vorticity thickness of 0.6 cm and density interface thickness of 0.3 cm. Downstream of the crest the lower layer accelerates, ${\textit {Ri}}_{I}$ drops below 0.25, and the interface becomes unstable to Kelvin–Helmholtz instabilities.

Figure 9.

(a–c) Photographs of Exp. 11 demonstrating the formation and fate of Kelvin–Helmholtz billows. The flow was illuminated with a sheet of laser light aligned along the centreline of the flume. The laser light causes a dye dissolved in the lower layer to fluoresce. The region outlined in (a) is expanded in (b,c), which are successive photographs, taken 0.29 seconds apart. The growth and advection of a series of Kelvin–Helmholtz billows originating on the density interface in the supercritical flow upstream of the jump (denoted 1–4) is shown. These billows entrain fluid from the upper layer into the lower layer as they are advected beneath the jump. Billows (2) and (3) are in the process of pairing. An additional, weaker series of billows forms on the interface between the jump face and the upper layer (inside red box). Features in the red box are compared with (d), which is a radar image of the upper portion of an atmospheric internal hydraulic jump in the lee of the Sierra Nevada mountain range. Shear instabilities that form on the jump face, grow, pair and collapse as they are advected downstream. Adapted from Armi & Mayr (Reference Armi and Mayr2011).

The laser imaging of Exp. 10 shows the growth of Kelvin–Helmholtz instabilities on the interface as the lower layer accelerates down the lee slope of the obstacle (figure 8a). Wavelike disturbances precede the appearance of two isolated billows and two billows in the process of pairing (figure 8a). These observations are consistent with the theory of the hydrodynamic stability of stratified shear flows. In this experiment, the velocity shear is centred about the density interface, so the gradient Richardson number at the density interface is given by

(4.1)\begin{equation} {\textit{Ri}}_{I} = \frac{g^{\prime}\delta_{V}^{2}}{\left({\Delta}u \right)^{2}\delta_{\rho}}, \end{equation}

where the vorticity thickness, $\delta _{V} = {{\Delta }U}/{\left (\partial u / \partial z \right )_{I}}$, the density interface thickness, $\delta _{\rho } = - {{\Delta }\rho }/{\left (\partial \rho /\partial z \right )_{I}}$, where ${\Delta }u = u_{2} - u_{1}$ and ${\Delta }\rho = \rho _{2} - \rho _{1}$. The longitudinal variation of ${\textit {Ri}}_{I}$ is plotted in figure 8(b), using $\delta _{V} = 0.6$ and $\delta _{\rho } = 0.3\,\text {cm}$, which are the values obtained from upstream velocity and density profiles. The variation of ${\Delta }U$ is calculated using the observed layer thicknesses and measured flow rates. Upstream of the obstacle ${\textit {Ri}}_{I} > 0.25$ and the interface is stable, as predicted (Miles Reference Miles1961; Corcos & Sherman Reference Corcos and Sherman1976). As the flow passes over the obstacle ${\Delta }U$ initially decreases, until close to the crest both layers have the same flow speed, and ${\textit {Ri}}_{I} \rightarrow \infty$. On the lee face of the obstacle the lower layer accelerates and ${\textit {Ri}}_{I}$ decreases until at about $x = 0.25$ m, ${\textit {Ri}}_{I}$ drops below 0.25. From this point, until the end of the sill, the flow becomes increasingly unstable and Kelvin–Helmholtz billows begin to grow. By the end of the sill, ${\textit {Ri}}_{I}$ is sufficiently low for the billows to pair (Koop & Browand Reference Koop and Browand1979). An example of leapfrog pairing (Pawlak & Armi Reference Pawlak and Armi1998; Thorpe Reference Thorpe2007) is visible at $x \approx 0.5$ m in figure 8(a). After pairing, ${\textit {Ri}}_{I}$ increases to approximately 0.25 and further pairing is not observed.

4.2. Structure of internal hydraulic jumps

In Exp. 11 a drowned jump formed near the end of the sill (figure 9a), and the interaction of the flow upstream of the jump with the jump is captured in two photographs taken 0.29 s apart (figure 9b,c). In figure 9(b), billow ‘1’ is located just upstream of the nose of the jump. Immediately, downstream of this billow is a parcel of upper layer fluid that has been drawn underneath the nose of the jump by the strain field of the previous billow ‘0’. As billow ‘1’ advects beneath the nose of the jump, the parcel of upper layer fluid between ‘0’ and ‘1’ is fully entrained beneath the jump (figure 9c). Subsequently, this entrained fluid mixes with the jump fluid sitting above it. Similarly, we see that the parcel of upper layer fluid between billows ‘1’ and ‘2’ is drawn into the jump (figure 9c). Billows ‘2’ and ‘3’ grow between figures 9(b) and 9(c) and are in the process of pairing. Billow ‘4’ is just starting to form in figure 9(b), but 0.29 seconds later, in figure 9(c), it is clearly visible. Billow ‘5’ is starting to form in figure 9(c). Thus, there is a continuous train of billows that results in the entrainment of successive pulses of upper layer fluid into the jump. This is the primary source of entrainment and mixing associated with the jump.

Another potential source of mixing is a second set of billows that forms on the interface between the jump and the upper layer – the jump face, starting at the ruler in figure 9(b,c). These billows are subject to much less shear than the billows advecting beneath the jump, and do not cause as much entrainment and mixing. An atmospheric analogue of these billows has been observed on the face of the jump that forms in the lee of the Sierra Nevada mountain range shown in figure 9(d) (Armi & Mayr Reference Armi and Mayr2011). Although the shear Reynolds number, ${\textit {Re}}^{*} \equiv \Delta u \delta _V / \nu \approx 1100$, is relatively high for a laboratory experiment, it dwarfs in comparison with the estimate of $O\left ( 10^{9} \right )$, for the case shown in figure 9(d). The observations are remarkably similar; in each case the billows grow, pair and collapse as they are advected downstream.

The unprecedented detail in figure 9(d) was captured by the University of Wyoming King Air research aircraft flying at 3.1 km with the radar looking upward beneath the internal hydraulic jump. Upstream is to the left, and the start of the cloud on the jump face is only visible when the streamlines rise to the lifted condensation level. The distance scale is centred in the valley at the town of Independence, California ($x = 0\,\text {km}$). At the start of the jump face ($x \approx - 2.7\,\mathrm {km}$), ${\textit {Ri}} < 0.25$ and the flow is subject to instabilities that grow into vortices. The vortex at $x \approx - 1.5$ km has entrained high-reflectivity (4 dBZ) moist air from below and wrapped it around its core. The next core centred at $x \approx - 0.5$ km is less distinct, but the vortex centred at $x \approx 0.5$ km east has a clear mass of high reflectivity (5 dBZ) mixed throughout its core. The next two vortices downstream at $x \approx 1.5$ and $x \approx 2.5$ km east appear to be pairing, a process first clearly identified for unstratified flows by Winant & Browand (Reference Winant and Browand1974) and Brown & Roshko (Reference Brown and Roshko1974), as the mechanism for growth of a shear layer. Note that in stratified flows the pairing doubles the Richardson number, as recognised by Koop & Browand (Reference Koop and Browand1979). When the ${\textit {Ri}} \gtrsim 0.25$ pairing is no longer possible and the coherent structures collapse, as can be seen in figure 9(b–d). The above observations are also consistent with data obtained from a balloon sounding that was launched from the ground at Independence and crossed the shear region at an altitude of 4.9 km (blue line in figure 9d). The Richardson number computed from the sounding was ${\textit {Ri}} \approx 0.5$, therefore, downstream of the sounding no further growth of the shear layer is possible and the coherent structures collapse.

Experiments 12 and 13 were performed to further illustrate the dynamics of internal hydraulic jumps. In these experiments a higher flow rate ratio, $r = 0.50,$ and a larger sill, $h_m = 15\,\mathrm {cm}$, were used to generate bigger jumps that could be measured in more detail. In Exp. 12 $(r = 0.50,\ G_{0}^{2} = 0.31$ and $\beta _m= 0.37),$ a drowned internal hydraulic jump formed approximately mid-way down the lee face of the sill (figure 10a). A series of vertical conductivity profiles were taken at $x = -1.0$, 1.0 and 3.0 m (figure 10b–d). The upstream profile shows the strongly two-layered upstream flow, where the density interface is about 3 mm thick (figure 10b). The profile at $x = 1.0$ m (just beyond the end of the sill) illustrates the vertical structure of the jump (figure 10c). For the purpose of discussion we identify five regions at this location, descending from the free surface:

1. (A) The upper layer in which the density remains constant at $\rho _{1}$.

2. (B) The shear layer on the jump face.

3. (C) The internal hydraulic jump, characterised by small amplitude fluctuations of variable frequency. This portion of the jump is buffeted by the shear layers above and below it.

4. (D) The shear layer at the base of the jump, consisting of a series of billows that were initiated upstream of the jump and advected beneath it. At $x = 1\,\mathrm {m}$ this shear layer exhibits rapid and large fluctuations in conductivity, reflective of the passage of Kelvin–Helmholtz billows that have begun to break down. Here, the conductivity fluctuations are larger than those seen in the shear layer on the jump face (Region B), since the velocity shear and resultant instabilities are stronger.

5. (E) An undisturbed region of the lower layer into which shear instabilities do not penetrate. In this region the density remains constant at $\rho _{2}$.

Figure 10.

(a) Photograph of Exp. 12, (b) density profile at $x = -1$ m, (c) density profile at $x = 1$ m, (d) density profile at $x = 3$ m. Each profile took approximately 60 s to complete.

Downstream of the jump, at $x = 3.0$ m, the flow has returned to being almost two-layered (figure 10d). The upper layer and the lower portion of the lower layer remain undisturbed. The billows on the jump face have broken down and collapsed leaving a sharp density interface approximately 1 cm thick. The shear layer at the base of the jump has merged with the jump to form a region of almost linear density gradient (figure 10d), and almost constant shear (not shown, but similar to figure 6b); we shall refer to this region as the jump wake. The average gradient Richardson number in this linearly stratified region is approximately 1.0, and there is no longer any shear instability, or active mixing. There are, however, still small density fluctuations that reflect incomplete mixing in the jump.

4.3. Quantitative analysis of entrainment into internal hydraulic jumps

In Exp. 13 $(r = 0.50,\ G_{0}^{2} = 0.45$ and $\beta _m = 0.32)$ a drowned jump formed near the end of the sill ($x = 0.9\,\mathrm {m}$). In this experiment we collected times series of conductivity (converted to density) at 23 vertical elevations at $x = 1.5$ m; 0.6 m downstream of the nose of the jump. Each time series consisted of 1024 measurements taken at 25 Hz. The non-dimensional density

(4.2)\begin{equation} \rho^{\prime}(z^{\prime}) = \frac{\rho(z^{\prime}) - \rho_{1}}{\Delta \rho}, \end{equation}

where $z^{\prime } = z / Y_0$, is plotted as a function of elevation in figure 11(b) for each of the 23 time series. This plot illustrates both the mean vertical density profile and the fluctuations about it. Five time series, representative of each of the five regions, are presented in figure 11(a). In the upper layer (Region A, e.g. $z^{\prime } = 0.60)$ the density is constant, except for instrumental noise, and equal to the density of the inflowing fresh water, $\rho ^{\prime } = 0$. In the upper shear layer (Region B, e.g. $z^{\prime } = 0.48)$, the density fluctuates in the range $0 \leq \rho ^{\prime } \leq ~0.32$ due to the passage of pulses of entrained fluid that have been partially mixed into the shear layer. At this location billows are in the process of merging and this is reflected in the variable time scales of the density fluctuations. In the internal hydraulic jump (Region C, e.g. $z^{\prime } = 0.42$), the density fluctuates slowly in the range $0.32 \leq \rho ^{\prime } \leq 0.64$: the passage of billows in both the upper and lower shear layers forcing the jump fluid up and down. In the lower shear layer (Region D, e.g. $z^{\prime } = 0.22$) the density fluctuates in the range $0.64 \leq \rho ^{\prime } \leq 1$: these fluctuations are larger, and fluctuate more rapidly, than those in the upper shear layer, reflecting the more active mixing in the lower shear layer. In the lower layer (Region E, e.g. $z^{\prime } = 0.06)$ the density is constant, except for instrumental noise, and equal to the density of the inflowing saline water, $\rho ^{\prime } = 1$.

Figure 11.

(a) Time series of density in Exp. 13 at $z = 0.06$, 0.22, 0.42, 0.48 and 0.60. (b) Compilations of density measurements at each location. Each time series consists of 1024 measurements taken at 25 Hz.

The density profiles presented in figure 10 show that the sharp two-layer flow observed upstream of the sill is substantially modified as it passes over the sill and through the jump. However, these profiles alone do not allow us to make quantitative estimates of the amount of entrainment and mixing that has occurred, because the velocity profiles have also changed. Both the velocity and density profiles need to be taken into account, and the appropriate way to do so is to compare normalised profiles of density as a function of streamfunction,

(4.3)\begin{equation} \psi(z^{\prime}) = \left\{\int_{0}^{z^{\prime}} u \,{\rm d} z^{\prime}\right\}\frac{Y_0}{q}. \end{equation}

Here, we examine the profiles of $\rho ^{\prime }$ vs $\psi$ for experiments 6–9, see figure 12. The upstream ($x = -1.5\,\mathrm {m}$) profile for Exp. 6 is indistinguishable from the upstream profiles for Exps. 7–9 (not shown), demonstrating the two-layer nature of the upstream flow. For each experiment, profiles were taken sufficiently far downstream of the jump ($x = 4.5$ m) for active mixing to have ceased. The gradient Richardson number in the wake of the jump is of $O(1)$ in each case.

Figure 12.

(a) Profile of $\rho ^{\prime }$ vs $\psi$ upstream $(x = -1.5\,\textit {m})$ of the sill in Exp. 6 (red), and profiles of $\rho ^{\prime }$ vs $\psi$ downstream $(x = 4.5\,\mathrm {m})$ of the drowned jumps in Exps. 6–8 (black). (b) Profile of $\rho ^{\prime }$ vs $\psi$ upstream $(x = -1.5\,\mathrm {m})$ of the sill in Exp. 9 (red), and profiles of $\rho ^{\prime }$ vs $\psi$ downstream $(x = 4.5\,\mathrm {m})$ of the free jump in Exps. 9 (black).

The density-streamfunction profiles highlight the differences between free jumps and drowned jumps with respect to entrainment and mixing. In the drowned jumps (Exps. 6–8), a considerable amount of upper layer fluid is entrained and mixed into the lower layer, but almost no fluid from the lower layer is mixed into the upper layer (figure 12a). In the free jump (Exp. 9), mixing occurs almost symmetrically about the interface (figure 12b). To quantify entrainment rates we define the flux of upper layer fluid entrained into the lower layer as

(4.4)\begin{equation} q_{12} = \int_{0}^{\psi_{\tiny{{\textit{INT}}}}}\left(1 - \rho^{\prime}\right) {\rm d} \psi, \end{equation}

and the flux of lower layer fluid entrained into the upper layer as

(4.5)\begin{equation} q_{21} = \int_{\psi_{\tiny{{\textit{INT}}}}}^{1}{\rho^{\prime}}{\rm d} \psi, \end{equation}

where we define $\psi _{\tiny {{\textit {INT}}}}$ is the value of the streamfunction when $\rho ^{\prime } = r$. The net entrainment flux

(4.6)\begin{equation} q_{\tiny{{\textit{ENT}}}} = q_{12} - q_{21}. \end{equation}

Note that combining (4.4) and (4.5), and recognising that $\int _{0}^{1}\rho ^{\prime }\,{\rm d} \psi = r$, gives

(4.7)\begin{equation} q_{\tiny{{\textit{ENT}}}} = \psi_{\tiny{{\textit{INT}}}} - r. \end{equation}

The values of $q_{12}$, $q_{21}$, $q_{\tiny {{\textit {ENT}}}}$ and $\psi _{\tiny {{\textit {INT}}}}$ for each of the profiles are given in table 2.

The profile obtained at $x = -1.5\,\mathrm {m}$ in Exp. 6, is typical of the upstream profile in all experiments, and shows an almost perfectly two-layered flow (figure 12a): very little fluid has been entrained across the interface in either direction, see table 2. The lack of entrainment reflects the care taken to minimise mixing upstream: in the channel upstream of the sill the interfacial Richardson number, ${\textit {Ri}}_{I} = O(0.5)$, see figure 8(b). The distinctly two-layer flow upstream of the sill allows us to focus on the mixing and entrainment associated with the jump, and their impact on the downstream flow. We discuss the experiments with drowned jumps first (Exps. 6–8), and then the experiment with a free jump (Exp. 9).

In the case of drowned jumps (Exps. 6–8), far more fluid is entrained from the upper layer into the lower layer, than vice versa, i.e. $q_{12} \gg q_{21}$ (table 2). In fact, within the accuracy of our experiments, $q_{21}=0.004$ is the same as it was upstream of the sill, indicating that there is a negligible amount of mixing caused by the upper shear layer in drowned jumps, consistent with figure 6(a–c). The amount of fluid entrained and mixed by the lower shear layer increases as a drowned jump moves down the lee face of the sill, see figure 13 and table 2. The further downstream that a jump forms, the greater the length of the shear layer that is exposed upstream of the jump, and the more entrainment into the jump. This increasing entrainment is reflected in the increasing density deficit downstream of the jump (figure 12a). Beneath the jump the shear layer is subject to pairing, and continues to grow until it occupies the full depth of the wake of the jump. Downstream $(x = 4.5\,\mathrm {m})$ of a drowned jump there is an almost linear decrease in $\rho ^{\prime }$ with increasing $\psi$ in the wake of the jump (figure 12a). The interface between the upper layer and the lower layer downstream of the jump remains sharp, confirming that the shear instabilities on the upper face of the jump do not result in a significant amount of mixing. Even though the lower shear layer is relatively strong, it is not strong enough to penetrate the bottom boundary layer, and the lower portion of the lower layer remains undisturbed.

Figure 13.

Entrainment fluxes downstream $(x = 4.5\,\mathrm {m})$ of the jump in Exps. 6–9 plotted against the normalised jump location, $x_j/L_{S}$. The open triangles represent, $q_{12},$ the flux of fresh fluid in the lower layer; the open squares represent, $-q_{21}$, and the closed circles represent the net entrainment flux, $q_{\tiny {{\textit {ENT}}}} = q_{12} - q_{21}$. The grey symbols are from measurements taken upstream $(x = -1.5\,\mathrm {m})$ of the sill.

In Exp. 9, in which a free jump forms far downstream of the sill, the behaviour is quite different. Immediately downstream of the sill ${\textit {Ri}} \ll 0.25$ and billows pair: further downstream ${\textit {Ri}} \gtrsim 0.25$, and they collapse and breakdown due to secondary three-dimensional instabilities. In the resulting mixed layer, the velocity and density profiles vary relatively smoothly. The jump that forms downstream of this mixed layer is more of a gradual expansion with no roller region (see figures 2(a), 5 and 6(d)), in contrast with the drowned jumps described above. Downstream of the free jump the $\psi (\rho ^{\prime })$ plot is almost symmetric about the interface, see figure 12(b). Thus, there is a dramatic difference between drowned jumps and free jumps, both in the structure of the jump and the entrainment and mixing associated with it.

In developing the theory presented in § 2 we assumed that the change in $r$ due to entrainment into the jump was small. This assumption is satisfied in our experiments where the maximum value of $q_{\tiny {{\textit {ENT}}}} \approx 0.031$ (Exp. 8), which is indeed small compared with r = 0.4. To achieve much greater entrainment, the velocity shear between the two layers upstream of the jump would have had to have been much greater, but this is not achievable in two-layer flow over a sill, where the driving force is the pressure difference due to a higher interface level upstream of the sill than downstream.

However, much higher velocity shears can be achieved in flows of the type studied by Wilkinson & Wood (Reference Wilkinson and Wood1971), where the upstream flow was a strong boundary jet injected through a small (1 cm high) duct under high pressure. In the strong internal jumps of Wilkinson & Wood (Reference Wilkinson and Wood1971), the shear internal Froude number (see Appendix A) at location E, $F_{\Delta E}^{2} = 50$–270; and the flux of ambient fluid entrained into the jet was up to 200 % of the initial jet flux.

While Wilkinson and Wood achieved high shear internal Froude numbers by discharging under pressure, consistent with engineering applications, the Froude numbers achieved in our experiments were limited by the difference in interface height upstream and downstream of the sill, as is also the case in geophysical flows (e.g. Mayr & Armi Reference Mayr and Armi2008). In our experiments $F_{2 E}^{2} = 2.9$–4.0, see table 1. Even though the density and velocity profiles were modified upstream and downstream of the jump, a sharp density interface persisted downstream of the jump. In Exp. 9 the flux of upper layer fluid entrained into the lower layer, $q_{12} = 0.04$ (table 2) was 10 % of the initial lower layer flux; i.e. $q_{12} / r = 0.1$, see table 2. This value, the highest achieved in our experiments, is more than an order of magnitude less than the entrainment rates of Wilkinson & Wood (Reference Wilkinson and Wood1971).