Fig. 1. Bottom-corner region in a linearly stratified rotating circular basin. (a) Schematics of a circular basin and the definition of variables, and b,c) flow field under fundamental-mode internal Kelvin wave with $S=0.3$ and Poincaré wave with $S=1.0$, respectively. $E/S=3 \times 10^{−3}$ is used for plotting. In the inviscid limit, no radial and vertical velocities are induced at the phase shown, and the azimuthal velocities above the bottom boundary layer are into the display. Blue lines indicate the angle of internal-wave ray, with the vertical distance corresponding to the bottom-boundary-layer thickness $\Delta_z$. Modified from a figure in Shimizu and Imberger (2009, J. Fluid Mech.).
Fig. 2. Dispersion relationships and damping rates of fundamental-mode internal Kelvin and Poincaré waves in a circular basin. Coloured lines show contributions of different mechanisms. $\chi$ is a non-dimensional factor that depends on the vertical mode of interest, and $\chi \approx 2$ for vertical mode 1 under linear stratification and the Boussinesq approximation. Modified from a figure in Shimizu and Imberger (2009, J. Fluid Mech.).
Fig. 3. Horizontal structure of fundamental-mode internal Kelvin and Poincaré waves. (1st row): weakly viscous solution, (2nd row): inviscid solution, and (3rd-5th row) 1st-order correction due to spin-down, internal wave cancelling by bottom friction, and that by side wall friction, respectively. Colour shading and vector show isopycnal displacements and horizontal velocities, respectively, at $z/H=−0.75$. Isopycnal displacements $\eta$ and horizontal velocity $\vec{v}$ are respectively scaled by $a$ and $ca/R$, where $a$ is the maximum isopycnal displacement. Weakly viscous solution (top) is given by $\xi=\xi^{(0)}+(E/S)^{1/2} \left( \xi_{sp}^{(1)} + \xi_{iwc}^{(1)} + (H/R) \xi_{sw}^{(1)} \right)$, where $\xi=\eta, \vec{v}$. $E/S=0.08$ is used for plotting. Modified from a figure in Shimizu and Imberger (2009, J. Fluid Mech.).
In our study on the damping of basin-scale internal waves in Lake Kinneret, we found that the waves are damped within a few days in a 40-m-deep lake by bottom friction. When we got this result, my PhD supervisor, Jörg Imberger, asked me how this is possible, because the momentum or energy loss within the boundary layer cannot diffuse into the interior so rapidly. It turned out that this was an unsolved problem for gravity waves under the Coriolis effect. The answer to this question is essential to model damping of internal waves in a physically plausible way.
Our approach was to solve the problem analytically using a singular perturbation method by combining the following limiting cases:
Conveniently, these processes could be combined in a singular perturbation theory because both of them occur through boundary-normal velocity (or unsteady Ekman pumping velocity), which is induced by the divergence of volume-transport deficit due to boundary friction (or unsteady Ekman transport). Note, however, that the processes within the interior are different in the two cases.
These damping processes are much faster than diffusional damping because the damping of the interior flow occurs through inviscid processes.
In addition to the two known cases, solving the problem required two additional processes: side-wall boundary layer, induces additional wave-cancelling process, and Boundary-layer/interior flow communication in the bottom corner region.
To derive an analytic solution, we considered a rotating, linearly stratified basin with cylindrical shape and flat bottom. Schematics of the problem and the definition of variables are shown in Fig. 1a. The solution is written in a perturbation expansion of the form:
\begin{align} \xi=\xi^{(0)}&+(E/S)^{1/2}\xi^{(1)}+\cdots,\\ E&=\frac{\nu}{fH^2},\\ S&=\frac{c}{fR}, \end{align}where $\xi=\omega, \eta, \vec{v}$, $E$ is the Ekman number, $S$ is the Burger number 1), $\omega$ is the complex-valued angular frequency (the imaginary part represents the damping rate), $c$ is the celerity of the vertical mode of interest, and $\nu$ is the kinematic viscosity. We use $H/R=0.01$ in our examples.
Zoom-up of the solution in the bottom corner region is shown in Fig. 1b,c. Bottom friction creates the bottom boundary layer (grey shading) and the side-wall boundary layer (too thin to be seen in the figure), which modify the interior flow from the inviscid solution. Note that the boundary layer flow has a transverse component to the left of the interior flow when $\omega/f < 1$, but to the right when $\omega/f > 1$. Note also that the discontinuity of the Ekman transport at the bottom corner induces a corner jet when $\omega/f \ll 1$2),7), but an internal wave beam when $\omega/f \approx 1$. As a result, the contributions of different processes change rapidly near $\omega/f = 1$ (Fig. 2b).
Damping rates and horizontal structure of the fundamental-mode (i.e., vertical mode 1, radial mode 1, azimuthal mode 1) internal Kelvin and Poincaré waves are illustrated in Fig. 2 and Fig. 3.
Details are available in
This study was conducted when I was a PhD candidate at Centre for Water Research, University of Western Australia, with financial support of Japanese government (MEXT) scholarship and Tokyo-Tech Long-term Overseas Study Support Program.