3.1. Droplet distribution over the breaking crest

In order to explore the relationship between events in the breaking process and the spatio-temporal distribution of droplet generation over the breaking crests, the position, time and diameter of each droplet measurement are indicated on top of the crest profiles for the weak, moderate and strong breakers in figures 3(a), 3(b) and 3(c), respectively. The profiles are ensemble averages over 10 realizations of each breaker that are taken from figure 9 of Reference Erinin, Liu, Wang and DuncanPart 1 and plotted in the laboratory reference frame. The droplet data are from three breaker realizations at each measurement location. Plotting only a subset of the droplet data was necessary because higher numbers of droplets from additional breaker realizations made the plots difficult to interpret. Further details of the plotting scheme are given in the figure caption. Since the horizontal droplet measurement plane is located slightly above the wave crest, see § 2.1, the droplet measurement times and positions are not the same as the positions and times when the droplets were generated at the water surface. The motion of a given droplet between the time it is generated and measured is influenced by the initial droplet ejection velocity, the initial vertical distance from the measurement plane, and the interaction between the droplet and the air flow field, which is created by the breaking wave. Thus, the droplets measured in this experiment were generated at times earlier than the measured times and may have been generated upstream or downstream of their plotted location. These issues will be discussed further in § 3.5. Finally, it should be kept in mind that the droplets are measured across the entire width of the tank while the individual wave profiles are measured only at the centre plane of the tank. In spite of this limitation of the profile measurements, the ensemble average profile and distributions of standard deviation should be independent of cross-tank position, except very near the tank walls.

Figure 3.

(a) The spatial distributions of droplets plotted on top of the evolution of the ensemble average surface profiles for the weak, moderate and strong breakers are presented in (a,b,c), respectively. The ensemble average surface profiles are the same as those shown in figure 9 of Reference Erinin, Liu, Wang and DuncanPart 1; however, the profiles shown here are plotted in the laboratory reference frame. A similar version of (a) was presented in Erinin et al. (Reference Erinin, Wang, Liu, Towle, Liu and Duncan2019). The profiles and droplets are plotted relative to the ensemble average position and time of jet impact, $\tilde x = 0$ and $\tilde t = 0$, respectively. The bottom-most profile in each plot is the crest shape at $\tilde t = 0$ and each successive profile (the time between profiles is $\Delta t = 12.3$ ms) is plotted $\mathrm {d} y = 20$ mm above the previous. Every tenth profile is coloured red and labelled with a lower case Roman numeral. The green squares are located at the highest point on each surface profile and the magenta upside-down triangles are located at the first three indentations, see the caption for figure 9 in Reference Erinin, Liu, Wang and DuncanPart 1 for more details. The droplets are plotted as filled circles on the profile recorded at the time closest to the time when the given droplet crosses the measurement plane and are located on that profile at the streamwise position of the droplet crossing. The vertical bands with no droplets appear at locations where droplet data were not collected, see figure 2. These bands are sometimes difficult to see in the present panels due to the crest point and indention markers and an optical illusion created by the wavy surface profiles. The colour of the droplets indicates their diameter as given by the logarithmically scaled colour bar. Regions with large numbers of droplets with similar diameters take on a generalized colour and may correspond to particular processes in the breaking events. The blue- and orange-coloured backgrounds between the profiles show the spatio-temporal limits of two droplet-producing regions, regions I-A (in orange) and I-B (in blue).

As can be seen in figure 3(a–c), the first droplets are typically measured just before or after the profiles marked (i), which corresponds to $\tilde t =110.8$ ms. Near profile (ii), a region begins where many droplets with diameters as large as approximately 1 mm cross the measurement plane. For the strong breaker, this region is sharply defined (measuring approximately 150 mm by 98 ms) and begins at approximately profile (ii). The string of inverted magenta triangles marking the first indentation ends on this profile, indicating that the indention is no longer detectable at later times. (As discussed in detail in Reference Erinin, Liu, Wang and DuncanPart 1, the first indentation forms the boundary between the top surface of the plunging jet and the splash that it creates.) This region of high droplet number is located on the back face of the wave near the crest. As the breaker strength is decreased, the high-droplet-number region becomes more diffuse and begins at earlier times (profiles), before the end of the first indentation. The surface profile normal standard deviation, $n_{sd}$, and the surface profile arc length standard deviation, $s_{sd}$, (both defined in Reference Erinin, Liu, Wang and DuncanPart 1 and in the caption of figure 6 in the present paper) show only moderate values at the time and position ranges of this intensive droplet flux, see Reference Erinin, Liu, Wang and DuncanPart 1, figures 12 and 13. As discussed in Reference Erinin, Liu, Wang and DuncanPart 1, this is the region where the deep crater in the bottom of the first indentation pinches off close to its deepest point and retracts rapidly toward the free surface leaving a small region of bubbles in front and near the bottom of the tube of air entrapped at jet impact, see Movie 1 given as supplemental material.

Figure 4 contains, two sequences of three images, taken from Movie 2 (the strong breaker), that show the moments before, during and after the indentation closure. The images in the top row (a,c,e) and bottom row (b,d, f) are from the camera views take from above and below the water surface, respectively. Images (a,b) show the indentation 147 ms after jet impact and just before the crater below the indentation closes. By this time, the crest point (the highest point on a given wave profile) is located on the splash-up generated by the plunging jet impact. In the below-surface image, the view of the roller of air entrained at the moment of jet impact is nearly obscured by the crater that extends downward from the indentation at the surface. Only 4 ms later, images (c,d), the indentation crater has nearly reached full retraction as shown in image (d) and leaves behind a small number of air bubbles, which can be more clearly seen in Movie 2, Movie 3 and Movie 4. In images (e, f), taken 182 ms after jet impact, the indentation crater is completely retracted and droplets are being ejected all along the indentation. From the plots in figure 3, it can be seen that the number of droplets in this crater closure region increases dramatically with breaker strength. Also, in view of the fact that the region of high droplet number is small, well defined and close to the crater location, it is likely that the droplets’ initial velocities are nearly vertical and that the free surface in this region is close to the measurement plane. Droplet generation during the closure of the indentation is also seen in the numerical simulations of Wang et al. (Reference Wang, Yang and Stern2016) and Mostert et al. (Reference Mostert, Popinet and Deike2022).

Figure 4.

Three white-light image pairs in a time sequence of the closing of the first indentation with views from above the water surface (panels a,c,e) and below the water surface (panels b,d, f) for the strong breaker. The cyan arrows point to the indentation in each above-surface image and the magenta arrows point to the tip of the indentation crater in the below-surface images. Each pair of panels (a,b), (c,d) and (e, f) was captured simultaneously 147 ms, 151 ms and 182 ms after jet impact, respectively, and the first and last image pairs approximately correspond to profiles (ii) and (iii) in figure 3(c). See the text for more details. These images were taken from Movie 2. See also the edited version of this movie, Movie 1. Both movies are given as supplementary material.

Another region of intense droplet flux through the measurement plane is found over the breaking wave crest between profiles (iii) and (vi). These droplets are most likely generated by two breaking processes: splashing and bubble popping near the leading edge of the breaking zone on the downstream side of this high droplet flux region and the bursting of the large bubbles on the back face of the wave on the upstream side of the region. These large bursting bubbles on the back face are from the air entrapped under the jet at the moment of jet impact. Both of these droplet ejection processes can be seen clearly in the movies given as supplemental material. Also, both regions associated with these processes contain some of the highest values of $n_{sd}$ and $s_{sd}$, see figures 12 and 13, respectively, in Reference Erinin, Liu, Wang and DuncanPart 1 and the discussion of figure 6 in § 3.2 of the present paper.

For later analysis of droplet number, diameter and velocity distributions, the droplet generation shown in figure 3 is broken into two regions. The first region, called region I-A and marked by the orange background, includes the jet impact, formation of the first splash, and the formation and closing of the first indentation. The second region, called I-B and indicated by the blue background, covers the remaining regions of the breaking crest and includes the subsequent sequence of splash impacts and splash ups as well as the emergence and bursting of the large bubbles that were entrapped at the moment of jet impact. The spatial and temporal boundaries of regions I-A and I-B are given in table 1.

Table 1.

The number of droplets generated per breaking event per metre of crest length in regions I-A, I-B and II as well as the total for each of the three breakers. The spatial and temporal limits of the three droplet-producing regions are also given. The per cent contributions of each region relative to the total number of droplets is given in parenthesis.

3.2. The distribution of droplets over the entire wave field

As discussed above, the position ($\tilde x$), time ($\tilde t$), diameter ($d \geq 100\,\mathrm {\mu }{\rm m}$) and 2-D velocity ($\boldsymbol{v} = u\hat i + v\hat j$) of each droplet is measured as it travels upward across the measurement plane. Here we define the droplet-number distribution function $N(\tilde x , \tilde t, d, u, v)$ to be the number of droplets per breaking event per metre of crest length in bins centred on the values of the five independent variables within the ranges $0\leq \tilde x \leq 1050$ mm, $0\leq \tilde t \leq 2000$ ms, $d\geq 100\,\mathrm {\mu }{\rm m}$, $-3 \leq u\leq 3$ ${\rm m}\,{\rm s}^{-1}$ and $0 \leq v \leq 3$ ${\rm m}\,{\rm s}^{-1}$. In the following, we present results from various integrations of the distribution function over one or more of these independent variables. For notation, the distribution function is always presented with the independent variables that remain after the integrations. For example, the local number of droplets of all diameters and velocities per breaking event per metre of crest length is written $N(\tilde x, \tilde t\,)$ and the total number of droplets per breaking event is $N$.

Contour plots of $N(\tilde x, \tilde t\,)$ are given for the weak, moderate and strong breakers in figures 5(a), 5(b) and 5(c), respectively. See the figure caption for exact definitions and details. The most striking features of these droplet-number contour plots are the two large spatio-temporal regions of droplet production tilted with a slope close to the speed of the toe of the wave shortly after jet impact, $\langle u_{toe} \rangle$, and with their dark blue boundaries extending approximately 0.7$\lambda _0$ horizontally and 0.6$T_0$ vertically. These two regions were previously identified for the weak breaker in figure 2 of Erinin et al. (Reference Erinin, Wang, Liu, Towle, Liu and Duncan2019). In the present paper, the rectangular regions encompassing each of the main droplet-producing regions are called region I (roughly the lower half of each plot and consisting of regions I-A (orange background) and I-B (blue background) as previously defined in figure 3) and II (roughly the upper half of each plot, tan background). To aid in comparing the droplet production regions with the surface profile data shown in Reference Erinin, Liu, Wang and DuncanPart 1, the $N(\tilde x, \tilde t\,)$ contour plots from figure 5 for the three waves are superposed on the contour plots of the average surface height ($\langle y - y^i_c\rangle$) in figure 6(a–c), the profile normal distance standard deviation ($n_{sd}$) in figure 6(d–f) and the profile arc length standard deviation ($s_{sd}$) in figure 6(g–i). The original contour plots of $\langle y - y^i_c \rangle$, $n_{sd}$ and $s_{sd}$ are given in figures 11, 12 and 13, respectively, of Reference Erinin, Liu, Wang and DuncanPart 1 and the definitions of $n_{sd}$ and $s_{sd}$ can be found in figure 8 of Reference Erinin, Liu, Wang and DuncanPart 1 and in the caption of figure 6 in the present paper. As can be seen in figure 6(a–c), the area of large droplet production in region I is generally aligned with the breaking wave crest and in region II with the following wave crest.

Figure 5.

Contour maps of $N(\tilde x,\tilde t\,)$, the number of droplets moving up across the measurement plane per surface area (m$^2$) per ms per breaking event are shown for the weak, moderate and strong breakers in (a,b,c), respectively. The data are from at least 10 breaker realizations at each droplet measurement location and from interpolation in $\tilde x$ intervals where no data were recorded. The contour maps are shown in the laboratory reference frame and cover the full measurement region, $\approx 1050$ mm in streamwise distance and $\approx 2000$ ms in time with a resolution of 13.02 mm by 25 ms. Only droplets with $d\geq 100\,\mathrm {\mu }{\rm m}$ are counted. Spatio-temporal bins where $N(\tilde x, \tilde t\,) \leq 0.05$ are coloured solid orange, light blue and tan in droplet-producing regions I-A, I-B and II, respectively. The magenta curves mark locations of the three indentations. The horizontal and vertical orange lines indicate the locations of the maxima of $N(\tilde t\,)$ and $N(\tilde x)$, respectively, see figure 7, with the solid, dashed and dotted-dashed lines for the first, second and third local maxima, respectively. The solid black lines are drawn with their slopes corresponding to, $\langle u_{toe} \rangle$, the average speed of the toe shortly after jet impact as computed from the data plotted in figure 10(a) of Reference Erinin, Liu, Wang and DuncanPart 1. For reference, the last wave profile shown in each of the three panels of figure 3 was recorded at $\tilde t = 0.851f_0^{-1}$. The white-filled black circle, black triangle and black square in each plot mark the locations of the local maxima at the end of the first indentation, between the first and second splash ups and the bursting of large air bubbles on the back face of the wave, respectively.

Figure 6.

Contour plots of $N(\tilde x$, $\tilde t\,)$ as 50 %-transparent overlays on contour plots of the ensemble average surface height ($\langle y-y^i_c \rangle$, a–c), the surface normal standard deviation ($n_{sd}$, d–f) and the arc length standard deviation ($s_{sd}$, g–i) for the three breakers with plots for the weak, moderate and strong breakers in (a,d,g), (b,e,h) and (c, f,i), respectively. As defined in Reference Erinin, Liu, Wang and DuncanPart 1, $n_{sd}=\sqrt {\langle [n-\langle n\rangle ]^2\rangle }/\lambda _{gc}$, where $n$ is the distance between the average profile and an individual profile measured at each point along the average profile in the direction of its local normal and $s_{sd}=\sqrt {\langle [s/s_m-1]^2\rangle }$, where $s$ is the local arc length of an individual profile and $s_m$ is the corresponding local arc length of the ensemble average profile. In each plot, the $N(\tilde x$, $\tilde t\,)$ overlay contours are presented in the teal-pink colour range. The $\langle y - y^i_c \rangle$, $n_{sd}$ and $s_{sd}$ contours in the background are opaque and are plotted in the black – yellow colour range. The three short curves in the lower portion of the plots, which are coloured magenta in the underlying plots and appear red in the top row of plots, are the three indentations as described in Reference Erinin, Liu, Wang and DuncanPart 1, figures 9 and 11–13. The circles, triangles and squares with black outlines and white fill are the same points as are in the corresponding $N(\tilde x, \tilde t\,)$ plots in figure 5; (a) $\langle y-y^i_c \rangle$ weak, (b) $\langle y-y^i_c \rangle$ moderate, (c) $\langle y-y^i_c \rangle$ strong, (d) $n_{sd}$ weak, (e) $n_{sd}$ moderate, ( f) $n_{sd}$ strong, (g) $s_{sd}$ weak, (h) $s_{sd}$ moderate, (i) $s_{sd}$ strong.

Figure 7.

Droplet-number distributions $N(\tilde t\,)$, $N(\tilde x)$ and $N^\prime (\tilde x^\prime )$ are given in (a,b,c), respectively. The spatial and temporal resolutions of the panels are $\Delta x = 21.6$ mm and $\Delta t =25.0$ ms respectively. Data for the weak, moderate and strong breakers are given as the green solid, blue dashed and red dotted lines, respectively. The coloured backgrounds in (a,b) indicate the approximate temporal and spatial limits, respectively, of the three droplet-producing regions defined in § 3.2. The function $N^\prime (\tilde x^\prime )$ presented in (c) is obtained by integrating $N(\tilde x^\prime,\tilde t\,)$ over all time, where $\tilde x^\prime =(\tilde x +\langle u^i_c\rangle \tilde t\,)$, i.e. the streamwise position in a coordinate system moving downstream with speed $\langle u^i_c\rangle$, the speed of the crest point at the time of jet impact.

In region I, the local maxima of $N$ vary in spatio-temporal location and in magnitude for the three breakers. From inspection of white-light movies of the breaking events and the comparisons with the contour plots of $n_{sd}$ and $s_{sd}$, these maxima seem to be associated with different physical surface processes in the breakers. For the weak breaker, there are three prominent local maxima in region I, as originally identified and discussed in detail in Erinin et al. (Reference Erinin, Wang, Liu, Towle, Liu and Duncan2019). The first local maximum (identified by the white-filled black circle in figure 5a) occurs shortly after and downstream (to the left) of jet impact (at $(\tilde x, \tilde t)=(0, 0)$). This location is near the end of the first indentation, which is marked by the right-most magenta curve at the bottom of the plot and by the rightmost string of downward magenta triangles in figure 3(a). The second maximum, marked by the white-filled black triangle, is just to the right of the second indentation and occurs in a region of low surface normal and arc length standard deviations between two regions of high standard deviation which stem from the first and second splashup on the two sides of the second indent, see figure 6(d,g). The third local maximum (marked by the solid black square) is located close to the region of high standard deviation associated with the bursting of large air bubbles that were initially entrained under the plunging jet. This local maximum is on the back face of the wave crest, figure 6(d,g).

For the moderate and strong breakers, region I contains only two prominent local maxima which are in similar spatio-temporal locations for the two waves. The first maxima (marked by the white-filled black circle) is located at approximately ($\tilde x$, $\tilde t$ ) = ($0.220\lambda _0$, $0.259f_0^{-1}$) and ($0.212\lambda _0$, $0.374f_0^{-1}$) for the moderate and strong breakers, respectively. This region seems to issue from the end of the first indentation and droplets produced in this region are confined to a narrow spatial and temporal location. The number of droplets increases with breaker intensity. The second local maxima (marked by the white-filled black triangle) is located on or to the right of the second indentation, at approximately ($\tilde x$, $\tilde t$ ) = ($0.381\lambda _0$, $0.374f_0^{-1}$) and ($0.415\lambda _0$, $0.518f_0^{-1}$) for the moderate and strong breakers, respectively. As in the second maximum for the weak breaker, these maxima occur in a region of low surface normal and arc length standard deviation which is enclosed by two regions of high surface normal and arc length standard deviation located directly downstream and upstream, see figure 6(e, f,h,i). From visual inspection of white-light movies, this local maximum is associated with the splash region at the leading edge of the breaking zone and the sudden eruption of large air bubbles that were entrapped under the plunging jet at impact. Thus, it appears that the second maxima in the moderate and strong breakers is composed of droplets from the leading edge splashing and large bubble bursting that create the second and third maxima, respectively, in the weak breaker.

In region II, there are no pronounced local maxima and the magnitudes of $N(\tilde x,\tilde t\,)$ are similar for the three waves. Observations from the white-light movies indicate that the droplets measured in region II are primarily the result of small bubbles that burst when reaching the free surface, after the main sources of droplets on the breaking crest have ceased production. It is shown in § 3.4 that these small bursting bubbles are generated with comparatively low vertical velocities. Thus, it is theorized that the reason that the droplets in region II are measured only over the following wave crest, is that the droplets do not travel vertically more than a few centimetres and only the crest of the following wave is within this distance from the measurement plane.

In order to make better quantitative comparisons of $N(\tilde x, \tilde t\,)$ from one breaker to another, the distribution is integrated in $\tilde x$ to obtain $N(\tilde t\,)$ and in $\tilde t$ to obtain $N(\tilde x)$. In addition, the integration

(3.1)\begin{equation} N^\prime(\tilde x^\prime) = \int_0^{2000\,{\rm ms}} N(\tilde x^\prime,\tilde t\,)\,{\rm d}\tilde t, \end{equation}

is performed where $\tilde x^\prime =\tilde x +\langle u^i_c\rangle \tilde t$ is the streamwise coordinate of a reference frame moving with speed $\langle u^i_c\rangle$, the speed of the crest point at the moment of jet impact, see Reference Erinin, Liu, Wang and DuncanPart 1 for details. The results are shown in figure 7 where $N(\tilde t\,)$, $N(\tilde x)$ and $N^\prime (\tilde x^\prime )$ are plotted in (a,b,c), respectively. Each panel contains three curves, one for each breaker. See the figure caption for details.

The three curves of $N(\tilde t\,)$ and $N(\tilde x)$, in figures 7(a) and 7(b), respectively, where jet impact occurs at the left and right ends of the horizontal axes, respectively, contain a number of local maxima. The locations of the first of these maxima (moving to the right in (a) and to the left in b) are marked by solid red vertical lines and also by vertical and horizontal lines on the edges of the contour plots of $N(\tilde x, \tilde t\,)$ in figure 5. In the curve for the weak breaker in 7(b), the overall maximum of the curve is marked as the first local maximum since the other local maxima are not significant. As can be seen in the contour plots of figure 5, the two solid red line segments would cross near the white-filled black circles, indicating that these $N(\tilde t\,)$ and $N(\tilde x)$ local maxima are due to droplets generated during the collapse of the crater at the bottom of the first indentation. From (a,b), it can be seen that the peak values of $N(\tilde t\,)$ and $N(\tilde x)$, increase by factors of 3.8 and 3.9, respectively, from the weak to the strong breaker. The second local maxima are marked by vertical red dashed lines and these maxima point to the white-filled black triangle in figure 5, indicating that these local maxima are due to a combination of droplets from the splash region and the bursting of large bubbles entrained under the plunging jet. The peak values of $N(\tilde t\,)$ and $N(\tilde x)$ at these locations increase by factors of 2.5 and 3.5, respectively, from the weak to the strong breaker. In the plot of $N(\tilde t\,)$, there is a small local peak at approximately $\tilde t = 0.58f^{-1}$ in all the curves and finally a consistent small peak in all curves at $\tilde t = 1.5f^{-1}$, which is the midpoint of the passage of the following wave crest. This latter peak does not appear in the plots of $N(\tilde x)$ because the integrations in time smear the effects of the breaking and following crests.

In the crest-fixed coordinates of 7(c), the computation of $N^\prime (\tilde x^\prime )$ results in a plot consisting of only two very clearly defined maxima for each breaker. This is because in this moving coordinate system, the integrations over the breaking and following crests are entirely separated and within each crest the various peaks overlap when integrating in $\tilde t$. The areas under the first and second peaks are the total number of drops measured in regions I and II. The magnitude of the first peak increases monotonically by a factor of approximately 3.0 from the weak to the strong breaker while the magnitude of the second peak increases from the weak to the moderate breaker and then decreases for the strong breaker to a value less than that for the weak breaker. The origin of this non-monotonic behaviour is under investigation.

The number of droplets produced in each droplet-producing region (I-A, I-B and II) and the total number of droplets measured for each breaker are given in table 1 along with the precise definitions of each region. These region definitions are set according to the local minima in the plots of $N(\tilde x\,)$ and $N(\tilde t\,)$ in figure 7(a,b). As indicated in the table, the droplets generated from the closing of the first indentation crater (region I-A) comprise on average 32 % of the total produced by each breaker. Both the number of droplets in II-B and the number in II-B as a per cent of the total number of droplets increase with breaker strength. The total number of droplets measured over the breaking crest, i.e. those in regions I-A and I-B combined, comprise approximately 80 % of the totals. The number of droplets produced by regions I-A, I-B and II and the total are plotted vs the area under the plunging jet's upper surface at the moment of jet impact, $Q^i$, and the vertical component of the crest point velocity at moment of jet formation, $\langle v_c^f\rangle$, (see Reference Erinin, Liu, Wang and DuncanPart 1 for detailed definitions) in figure 8, panels (a,b), respectively. The fact that the two plots look similar is a result of the nearly linear relationship between $Q$ and $v^f_c$ as shown in Reference Erinin, Liu, Wang and DuncanPart 1.

Figure 8.

In (a,b), the total number of droplets and the number of droplets measured in each subregion are plotted vs $Q^i$, the area under the plunging jet at $t=\langle t^i\rangle$, and $v_c^f$, the vertical velocity of the crest point at $t=\langle t^f\rangle$, respectively. As defined in Reference Erinin, Liu, Wang and DuncanPart 1, quantities with superscript $f$ were measured at the moment of jet formation and those with superscript $t$ were measured at the moment of jet impact.

3.3. Droplet diameter distributions

The droplet diameter distributions $N(\tilde t, d)$ and $N(d)$ are discussed in this subsection. Contour plots of $N(\tilde t, d)$, for the weak, moderate and strong breakers are shown in figures 9(a), 9(b) and 9(c), respectively. The three contour maps look qualitatively similar with two main droplet-producing regions, I and II, and separate peaks in $N$ in regions I-A and I-B at small $d$ (as seen most clearly in figure 9c). There are also a number of large-scale trends with varying breaker intensity. First, the number of droplets generally increases with breaker intensity at all diameters. Second, the diameters of the largest droplets ($d=d_{max}$), which are produced early in the breaking events as the crater at the bottom of the first indentation closes at $\tilde t \approx 0.41 f_0^{-1}$, increase from $d_{max} \approx 1200\,\mathrm {\mu }{\rm m}$ for the weak breaker to $d_{max} \approx 3000\,\mathrm {\mu }{\rm m}$ for the strong breaker (note the logarithmic scale of the $d$ axis in the plots). Finally, the ratio of the maximum diameters in region I-A to those in I-B increases with increasing breaker intensity.

Figure 9.

Contour maps of $N(d,\tilde t\,)$, the number of droplets per breaking event per metre of crest length per logarithmic diameter bin, for the weak (a), moderate (b) and strong (c) plunging breakers. The contour maps begin at the time of jet impact, $\tilde t = 0$, and cover approximately two wave periods ($\tilde t f_0 \approx 2.2$), with a temporal resolution of $\Delta t = 28.8$ ms. The scale of the vertical axis is logarithmic. The coloured orange/tan/blue backgrounds in each panel show the temporal limits of the three droplet-producing regions as identified in § 3.2.

The droplet diameter distributions, $N(d)$, are presented in the five log–log plots in figure 10. Each panel contains three data sets from the present experiment, one for each breaker. See the figure caption for additional details. Figure 10(a) contains the data for the entire data set for each of the three breakers. The curves are a bit noisy but generally indicate an increasing droplet number with increasing breaker strength at diameters above approximately 400 $\mathrm {\mu }{\rm m}$, the curves converge at smaller diameters. A number of authors have measured droplet diameter distributions in breaking wave and wind wave systems in the laboratory (see for example Veron et al. Reference Veron, Hopkins, Harrison and Mueller2012; Ortiz-Suslow et al. Reference Ortiz-Suslow, Haus, Mehta and Laxague2016; Erinin et al. Reference Erinin, Néel, Ruth, Mazzatenta, Jaquette, Veron and Deike2022; Ramirez de la Torre et al. Reference Ramirez de la Torre, Petter Vollestad and Jensen2022), the field (Wu et al. Reference Wu, Murray and Lai1984; Monahan Reference Monahan1968) and in DNSs with and without wind (Wang et al. Reference Wang, Yang and Stern2016; Tang et al. Reference Tang, Yang, Liu, Dong and Shen2017; Mostert et al. Reference Mostert, Popinet and Deike2022). Many of the distributions in these studies are either fitted or compared with separate power-law functions at small and large droplet diameter ranges. In view of these earlier studies, straight lines were fitted by least square error minimization separately to the smaller-diameter and larger-diameter droplet data in figure 10(a) for each of the three waves. The droplet diameter ($d_i$) at the boundary between the larger and smaller diameter groups was determined by an iterative bisection-like routine outlined in Erinin (Reference Erinin2020) and the supplemental material in Erinin et al. (Reference Erinin, Wang, Liu, Towle, Liu and Duncan2019). It should be noted that this determination of $d_i$ is inherently inaccurate because of the small number of droplets in each bin at the larger diameters. This is a classic problem in bubble and droplet measurements and to emphasize this inadequacy the power laws fitted to the large-diameter droplet data are drawn as dashed lines. The values of $\alpha$, $\beta$ and $d_i$ for the three breakers studied herein are given in table 2. The slope for the small diameters, $\alpha$, increases monotonically with increasing breaker strength while the slope for the large droplets first decreases and then increases. The intersection diameter increases monotonically with values ranging from 820 to 1480 $\mathrm {\mu }{\rm m}$. If the data from (a) are plotted with the $d/d_i$ as the independent variable, this normalization nearly collapses the data to a single two-slope curve.

Figure 10.

Plots of the droplet diameter distributions, $N(d)$, for various regions of the measurement plane. In each plot, the green circles, blue triangles and red squares are the data from the weak, moderate and strong breakers, respectively. Along the horizontal axis, the diameter bins are logarithmically spaced from $d = 100$ to $4000\,\mathrm {\mu }{\rm m}$ with 32 bins. In order to decrease the noise in these plots, all bins containing less than five measured droplets (all found at large $d$) are removed. The data in (a) are from the droplets measured over the full range of time ($0 < t < 2200$ ms) and streamwise position ($0 < x < 1050$ mm). Panel (a) shows $N(d)$ and the dashed lines are fits of straight lines to the values from the large-and small-diameter ranges as discussed in the text. Panel (b) shows $N(d)$ for region I. The solid lines are the results from previously published numerical simulations and experiments, see plot key and the text for details. In (c,d,e), $N(d)$ for regions I-A, I-B and II, respectively, are shown. The spatio-temporal limits of these regions are defined in table 1.

Table 2.

Parameters for the straight lines fitted by least squares error minimization to the distributions of droplet diameter in figure 10(a). The variables $\alpha$ and $\beta$ are the slopes of the straight lines for the small- and large-diameter droplet data, respectively, while $d_i$ is the diameter at which the two lines intersect.

Figure 10(b) contains the present data from region I and the droplet diameter distributions from the DNS results of Wang et al. (Reference Wang, Yang and Stern2016) and Mostert et al. (Reference Mostert, Popinet and Deike2022) as well as the no-wind case of breaking as a focused wave packet approaches a shoal in the laboratory experiments of Ramirez de la Torre et al. (Reference Ramirez de la Torre, Petter Vollestad and Jensen2022). Information about the numerical studies is given at the end of § 1 in the present paper, as well as in the original references. The data from Mostert et al. (Reference Mostert, Popinet and Deike2022) are obtained from the $Bo=1000$ case in their figure 19 and the capillary length scale $\ell _c$ is taken as 2.73 mm. The data from the no-wind $ak=0.66$ case in figure 6 of Ramirez de la Torre et al. (Reference Ramirez de la Torre, Petter Vollestad and Jensen2022) are reproduced by taking the value of the average droplet diameter as $\overline {D_e} = 1.75$ mm. The data from the high resolution case in figure 13 of Wang et al. (Reference Wang, Yang and Stern2016) are reproduced directly. In the cases of Wang et al. (Reference Wang, Yang and Stern2016) and Ramirez de la Torre et al. (Reference Ramirez de la Torre, Petter Vollestad and Jensen2022), the curves are adjusted vertically so that they approximately match the present data. The methods used to count droplets in each paper are different from those used in the present study and this adjustment is necessary in some cases. As can be seen from the panel, the shapes of the two CFD-based probability distributions are fairly similar to the present results, in spite of the differences in the wave motion, path to breaking, and wavelength between the DNS and the present study. Distributions from the experiments of Ramirez de la Torre et al. (Reference Ramirez de la Torre, Petter Vollestad and Jensen2022) fall off the present distributions at small diameter.

The droplet diameter distributions ($N(d)$) for droplet-producing regions I-A, I-B and II in the present experiments are given in (c), (d) and (e) of figure 10, respectively. Each plot is created from many fewer droplet measurements than in (a) and (b) but still displays interesting features. In region I-A, the two linear regions of the curves for the moderate and strong breakers are still evident; however, in view of the noisy data, the power-law fitting was not performed. The vertical separation between the curves is larger than in the distribution for the full data set, but the trend with breaker strength is only monotonic for $d \gtrsim 300\,\mathrm {\mu }{{\rm m}}$. For the data in region I-B, the curves are less noisy and closer together. The two-slope nature of the previously discussed distributions has been replaced by smooth arcs in which the local slope magnitude increases with increasing $d$. This trend continues in region II where the data form smooth curves that are nearly on top of one another. The structure of these data sets is thought to be a result of the different droplet generation mechanisms in the three regions. The very different curves in region I-A are thought to be a result of variations in droplet production during the crater collapse at the bottom of the first indent as was discussed in § 3.2 and as seen in Movie 1 given as supplementary material. This hypothesis is also supported by the droplet velocity data reported in the following subsection. In region II, droplets are generated as small bubbles come to the surface and burst. This leads one to hypothesize that the main difference between the three distributions in figure 10(e) is the number of droplets, $N_{II}$, i.e. the area under the three curves. Though the three data sets look similar in the log–log plot, $N_{II}$ varies between the data sets, see table 1. As a test, the probability distribution, $N(d)/N_{II}$, was examined (not presented herein). In this probability density function plot, the three data sets in are even closer together than in the $N(d)$ plot, thus supporting this small-bubble-bursting hypothesis. Finally, comparing the $N(d)$ plots in the three sub regions to that in the entire data sets in (a) indicates that region I-A is the only region in which the data sets show the two-slope structure found in the full data sets. This supports the idea that this two slope structure is create by the droplets generated by the closure of the first indentation.

3.4. Droplet velocity distributions

The distributions of the streamwise and vertical droplet velocity components, $u$ and $v$, respectively, and the 2-D speed, $V=\sqrt {u^2+v^2}$, are presented and discussed in this subsection. In all cases, $u$, $v$ and $V$ are reported relative to the laboratory reference frame. Contour plots of the droplet-number distributions $N(u,d)$, $N(v,d)$ and $N(V,d)$ are given for all the droplets for each of the three breakers in the nine panels of figure 11, see caption for details. From these contour plots, one can see that as the breaking intensity increases (moving down from plot to plot in each column), the number of droplets with large diameter and the range of $u$, $v$ and $V$ also increase. The peaks of the distributions are located at small diameters and at small values of $u$, $v$ and $V$. The distributions $N(u,d)$ (left column) indicate that there are droplets with positive (in the direction of wave travel) and negative horizontal velocities at all diameters and that the distributions are centred vertically at slightly positive values of $u$. The distributions $N(v,d)$ (centre column) are located, of course, entirely in the region of positive $v$ with a few droplets having speeds of nearly 4 ${\rm m}\,{\rm s}^{-1}$ and the number of these fast moving droplets increasing with breaker intensity. In considering these droplet speeds, it should be kept in mind that for these breakers the plunging jet speed ($\langle V^i_j\rangle$) and crest speed $(\langle u^i_c\rangle$) at jet impact are approximately, 2.0 ${\rm m}\,{\rm s}^{-1}$ and 1.3 ${\rm m}\,{\rm s}^{-1}$, respectively (see table 2 in Reference Erinin, Liu, Wang and DuncanPart 1 for details). The droplet velocity estimates divided by the crest speeds from the numerical calculations reported in Mostert et al. (Reference Mostert, Popinet and Deike2022), where the breaker wavelengths are approximately 30 and 50 cm, are similar in range to the present results where the nominal wavelength is 118 cm.

Figure 11.

Contour maps of the number of droplets per breaking event per metre of crest width per bin widths as a function of droplet velocity component $u$ and $d$, $N(u,d)$ (a,d,g), $N(v,d)$ (b,e,h) and $N(V,d)$ (c, f,i), for the weak (a–c), moderate (d–f) and strong (g–i) plunging breakers, where $V = (u^2+v^2)^{0.5}$ is the 2-D speed. In all panels, the vertical axis has equally spaced bins of height $0.1\,{\rm m}\,{\rm s}^{-1}$ and the horizontal axis has 80 logarithmically spaced bins with bin edges from $d = 100$ on the left to $2844\,\mathrm {\mu }{\rm m}$ on the right. The horizontal solid red and yellow lines in the $N(V,d)$ and $N(u,d)$ panels, respectively, are located at the values of $\langle V^i_j \rangle$ (the plunging jet speed at impact) and $\langle u^i_c \rangle$ (the crest point speed at jet impact), respectively, from table 2 of Reference Erinin, Liu, Wang and DuncanPart 1.

Probability distributions of $u$, $v$ and $V$ are presented for all of the droplets and for the droplets in regions I-A, I-B and II in figure 12, panels (a–l). See the figure caption for additional details. Average values of $u$, $v$ and $V$ corresponding to these plots are given in table 3. The p.d.f.s of $u$ (the four panels in the left column) are approximately symmetric with peaks located between approximately 0.1 and 0.3 ${\rm m}\,{\rm s}^{-1}$ and average values between 0.05 and 0.75 ${\rm m}\,{\rm s}^{-1}$. Among the three sub-regions, the average values of $u$ in region I-B (0.58 ${\rm m}\,{\rm s}^{-1}$ averaged over the three breakers) are the highest while the average $u$ in regions I-A and II are only 0.18 and 0.21 ${\rm m}\,{\rm s}^{-1}$, respectively. As mentioned above, droplets in region II are generated as small bubbles reach the surface and burst. Small bubbles bursting on a water surface with zero mean flow are expected to produce symmetric $u$ (and $w$ if measured) p.d.f.s with zero mean. Thus, the small positive mean and most probable $u$ values of approximately $u = 0.14\langle u^i_c\rangle$ in region II are probably an indication of horizontal fluid motion due the decaying surface drift current from breaking and the particle velocity in the crest of the non-breaking following wave. In the p.d.f.s of $v$ (the four panels in the middle column), the average value of $v$ and the range of $v$ decrease monotonically in going down in the column of plots from all droplets to regions I-A to I-B to II. These differences and trends in the $u$ and $v$ p.d.f.s between the three droplet-producing regions and the three breakers are consistent with the picture of the droplet-producing mechanisms in the three regions: crater collapse in the first indentation in region I-A, splashing and large and small bubble bursting in region I-B and small bubble bursting in region II. The corresponding p.d.f.s for 2-D droplet speed, $V$, are given for the interested reader.

Figure 12.

The probability density functions (p.d.f.s) of the horizontal velocity component ($u$, a,d,g,j), and vertical velocity component ($v$, b,e,h,k) and the 2-D speed ($V=\sqrt {u^2+v^2}$, c, f,i,l) of droplets as they pass through the measurement plane. The data covering all regions and regions I-A, I-B and II are given in (a–c), (d–f), (g–i) and (j,k,l), respectively. The width of all bins on the horizontal axis is 0.1 ${\rm m}\,{\rm s}^{-1}$ in all panels and the p.d.f. calculations are terminated after a bin contains less than 3 droplets. In each plot, data are given for the three breakers and the plotting symbol definitions are given in the key in (c). (a–c) All regions, (d–f) I-A, (g–i) I-B, (j–l) II.

Table 3.

The average horizontal velocity component ($\bar {u}$), vertical velocity component ($\bar {v}$), 2-D speed ($\bar {V}=\sqrt {{\bar {u}}^2+{\bar {v}}^2}$), 2-D average velocity angle ($\bar {\theta }$) relative to horizontal ($\bar {\theta } =0$ defined as downstream) and number of droplets ($N$) are given for each wave and separately for regions I-A, I-B and II. The values $N$ are the number of droplets per breaking event per metre of crest width in each region, the same numbers are reported in table 1.

The differences in the droplet velocities and their relationship to the droplet production mechanisms is further demonstrated by the examination of the droplet velocity direction, as measured by the angle ($\theta$) between the 2-D velocity vector and horizontal direction of wave motion. The distributions of $N(d,\theta )$ and $N(\theta )$ are presented in seven polar panels in figure 13. See the figure caption for details. Panels (a,b,c) are contour plots of $N(d,\theta )$ for all droplets in the weak, moderate and strong breakers, respectively. The radial and azimuthal coordinates are $d$ and $\theta$, respectively. All three distributions have an isolated region of high $N(d,\theta )$ at small 100 $< d \leq 300\,\mathrm {\mu }{\rm m}$ and $\theta \approx 60^\circ$. To better compare the three waves, the distribution $N(\theta )$ for all the droplets in each wave is plotted in polar coordinates with $N(\theta )$ and $\theta$ as the radial and azimuthal coordinates, respectively, in (d). There is one curve for each breaker intensity. The curves are somewhat irregular but one can see that the values of $\theta$ at the highest values of $N(\theta )$ increase with increasing breaker intensity. This increase in $\theta$ with breaker intensity is reflected in the average values of $\theta$ for all droplets as given in the next to last row of table 3. Panels (e, f,g) contain polar plots of $N(\theta )$ for regions I-A, I-B and II, respectively. These plots and the $\bar {\theta }_m$ data in table 3 demonstrate clear differences in droplet production between the three regions. In the three panels, one can see that $\theta _m$ is only approximately 20$^\circ$ downstream from vertical, i.e. in regions I-A and II, while it is of the order of 40$^\circ$ downstream from vertical in region I-B. This trend is reflected in the average values of $\theta$ in the three regions: 81.1$^\circ$, 56.2$^\circ$ and 74.1$^\circ$ in regions I-A, I-B and II, respectively, where each value is the average over the three waves. The narrow distribution of nearly vertical motion of the droplets in region I-A is clearly observed in Movie 1 given as supplementary material and is thought to be related to the generation during the closure of the crater at the bottom of the first indentation. The narrow nearly vertical distribution in region II is probably due to a combination of the distribution of droplet velocity in an individual small bubble-bursting event and the fact that measuring the droplets as they pass through the measurement plane above the generation point favours droplets generated with velocity vectors pointing up.

Figure 13.

Panels (a–c) are polar contour maps of $N(d,\theta )$, the number of droplets per breaking event per metre of crest length per diameter bin per $\theta$ bin, where $\theta$ is the angle of the mean 2-D velocity vector ($\boldsymbol{v} =u\hat i + v\hat j$) relative to horizontal in each diameter bin for the weak, moderate and strong breakers, respectively. The radial and azimuthal coordinates are $d$ and $\theta$, respectively. The motion of the wave is in the direction of $\theta = 0^{\circ }$ and $\theta = 90^{\circ }$ is vertically up. Panels (d–g) are polar line plots of $N(\theta )$, the number of droplets per breaking event per metre of crest length per $\theta$ bin for the three breakers for all regions in (d) and regions I-A, I-B and II in (e–g), respectively. The radial and azimuthal coordinates are $N(\theta )$ and $\theta$, respectively. The $\theta$ bin width $= 5.625^\circ$ in all plots and the $d$ bins in (a–c) are logarithmically spaced from $d = 100$ to $3000\,\mathrm {\mu }{\rm m}$ with 63 bins; (e) I-A,( f) I-B, (g) II.

3.5. Low-order predictions of droplet generation sites and time of flight

As discussed above, the droplet data presented herein are measured as the droplets move upward through the measurement plane just above the wave crest. In an effort to determine an approximate time and position of the generation of each droplet at the water surface, the measured droplet data are used with a model of the droplet motion to simulate the trajectories of the droplets backward in time until they intersect with the time evolving ensemble average profile history. This model also yields an estimate of the droplet time of flight ($\Delta t_f$) as it travels from the water surface to the measurement plane. Estimates of $\Delta t_f$ are essential for calculations of the reduction in droplet diameter due to evaporation before each droplet is measured. In this model, the forces on the particles are assumed to be those due to gravity and drag relative to still air, with the drag coefficient taken from the correlation for a spherical particle given by Cheng (Reference Cheng2009). Since, the air motion is very likely an important factor in determining the droplet motion, particularly for the smaller droplets, the degree to which the computed generation sites seem plausible is used to indicate the importance of the air velocity in the calculation and thus motivate additional research.

The results of these droplet trajectory calculations are shown in figure 14 where two plots of the ensemble averaged profiles from the strong breaker are shown along with the same set of droplets measured from three realizations of the strong breaker. In figure 14(a), which is a copy of the plot in figure 3(c), the droplets are shown on the profiles measured at the time the droplets crossed the measurement plane and at the corresponding streamwise positions. In figure 14(b), the water surface profiles in figure 14(a) are repeated but the droplets are plotted on the profiles and at streamwise positions computed by the backward tracking model. As can be seen by comparing the two plots, many of the droplets that were measured over the breaking crest in region I-B are predicted to have been generated near where they were measured, i.e. on the turbulent breaking region. Also, the area where many droplets were measured in region I-A in a sharply defined region filling the region between profiles (ii) and (iii) in figure 14(a) have tightened to a smaller range of time just after profile (ii). The number of droplets in this region of figure 14(b) is only a little less than in the corresponding region of figure 14(a); this result is not visible in the plots because many of the droplets are plotted on top of one another. An additional important feature of the plots is that many of the smaller droplets and some larger ones, 40 % of the total of 2158 droplets in the figure, are predicted to have been generated on the smooth water surface downstream (to the left) of the leading edge of the breaking zone. Though examination of the white-light movies does indicate that a few secondary droplets are generated in this downstream region due to primary droplet impacts, the large number of droplets predicted to be generated is thought to be non-physical and an indication of the need for including the temporally evolving breaker-generated air flow field in the calculation of the droplet motion.

Figure 14.

(a) The spatio-temporal distribution of droplets from three realizations of the strong breaker plotted on the corresponding ensemble averaged wave profiles (from 10 realizations). Each droplet is plotted on the profile when and the streamwise position where it crossed the measurement plane. This is the same plot as given in figure 3(c) (see that figure for more plotting details). (b) The spatio-temporal positions of the droplets (a) projected back to their generation sites as determined by the simplified droplet motion model described in the text. Figure 3(c) is shown here to facilitate the comparison between the measured droplet locations in(a) and the estimates of the locations where they were generated in (b).

The calculated values of $\Delta t_f$ for the droplets considered in figure 14 are presented as a function of $d$ in figure 15. From the plot, it can be seen that the data for the droplets with the smallest diameters fall on a single line with positive slope and values ranging from $\Delta t_f \approx 25$ ms at $d=100\,\mathrm {\mu }{\rm m}$ to $\Delta t_f \approx 40$ ms at $d=200\,\mathrm {\mu }{\rm m}$. For larger diameters, the data at each $d$ spread out vertically with the smallest to largest $\Delta t_f$ values ranging from approximately 30 to 70 ms and generally increasing monotonically with breaker strength. These times of flight were used in § 2.3 to estimate the effect of evaporation on the measured diameters of the droplets in this study.

Figure 15.

Estimates of the time of flight of droplets as a function of droplet diameter for the weak, moderate and strong breakers. These estimates are based on the time, position and velocity of the droplets measured as they move upward through the measurement plane, the ensemble average profile sequence and the simplified droplet motion model discussed in § 3.5. The standard deviation of $\Delta t_f \approx 30$ ms for $d \approx 100\,\mathrm {\mu }{\rm m}$ and $\approx$50 ms for $d \approx 500\,\mathrm {\mu }{\rm m}$.