Wave attractor
is a peculiar but important phenomenon of internal/inertial waves self-focusing
under proper conditions [1], leading to the formation of a stable wave of a
specific shape (called a wave attractor) which is prone to accumulate the
energy incoming
into the system. Due to the increase of the
amplitude on an attractor, there appears an opportunity for the instability
formation, that hides the coherent structure formed [2]. The energy overpumping
into the system, with the consequent production of secondary waves, is named
one of the main reasons for why attractors are so hard to discover in the real
ocean [3] where they are supposed to present respectively frequently [4].
The
experimental investigation of the phenomenon has been mainly concentrated on the
simple-shaped geometry [3,5–12]. Simultaneously, attractors have been
successfully studied via numerical simulation [11, 13–18]. The main method of
the visualization has remained to be velocity-based: slices or isosurfaces of a
component/modulus [19].
However, these
methods become inapplicable for visualization with the growth of instabilities.
This makes one to seek for new visualization approaches. The latest works
concerning attractor in enlarged geometries [18], with modified density
gradient [20], in specifically-shaped domains [21] revealed effects that
require more precise visualization.
On
the other hand, in gas dynamics, there is a method called numerical Schlieren
used for the visualization of the internal structure of a flow. In experiments,
the Schlieren method is an optic method; for numerical simulation, considering
density gradient
(
)
yield the
same picture in binary colormap as black-and-white photography in experiment
[22, 23]. Since attractors are considered in liquid, it is an incompressible
medium; hence, considering density gradient is senseless. Because of it, we
propose to consider a pressure gradient instead of density one:
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(1)
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To
apply this method we selected the following computational cases from [24, 14,
18, 20, 21]:
• Attractor
in trapezoid geometry
• Attractor
in basin with non-linear stratification
• Attractor
in large aspect ratio domain
• Attractor
in geometry with underwater peak
• (2,1)
attractor in domain with underwater plateau
All these cases
were simulated using Nek5000 [25] software, solving the system of Navier-Stokes
equation in Boussinesq approximation, salt transport equation (with Schmidt
number being 700) and incompressibility condition.
Here
is a fresh
water density,
is density
increase caused by dissolved salt,
is salt
diffusivity (was taken so that
).
The external
forcing was provided via a wave-maker [26] located on the top side (numerically
it was a boundary condition for velocity). The visualization is tested for 2D
cases, after the dimension-reduction approach being approved in [11, 13, 14,
17, 27].
Fig. 1: Spectral
element computational grids: a) for base trapezoidal case and halocline
profile, b) for geometry with underwater step, c) for geometry with mid-depth
plateau, d) for large aspect ratio geometry
Nek5000, being
a spectral-element method, provides a high-order solution. The element grids
for cases considered hereinafter are depicted on Fig. 1. However, the data were
written in regular post-processing grid (300x101 for the large aspect ratio
domain, 150x101 for the rest). For better understanding how do these meshes
correspond to each other, one can take a look at Fig. 2. It is an example with
reduced element/points number to be readable (e.g., spectral mesh is shown to
be 5x5 instead of 48x48 really used for this geometry). The spectral mesh consists
of inclined elements, with data being written in Gauss-Lobatto-Legeandre points
(cross-points of the thinnest lines); the post-processing grid is orthogonal,
with more points to use the post-processing data “as is”, without after-reading
interpolation.
It should be
noted that the gradient was calculated on the post-processing grid with 2nd
order finite-difference method, not by internal Nek5000 gradient method,
despite the latter being finer. This was done to prove the ability of the
visualization method proposed to work in post-processing mode on a secondary
grid.
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a)
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b)
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Fig. 2: Principle meshes
types used in this work: a) spectral-element mesh for CFD computation (5x5
example for better view; thinnest lines for Gauss-Lobatto-Legeandre nodes) and
b) regular post-processing grid on the same geometry (25x20 example)
To test the new
method, we will compare it with convenient visualization with a vertical
velocity slice. We will not plot the colorbar (values range scale) for
pressure-gradient method, hence the values plotted are mostly contingent and
vary from case to case. Velocity snapshots will be accompanied by colorbars
with values in cm/s, hence they have real physical sense.
For
all the cases, we must note a thing. Hence we drop the data on a
post-processing grid, for a faster work it is useful to make the grid regular.
Since one of the necessary conditions for the presence of an attractor is a
slope [1], some points appear to be outside the computational domain. We are
ready to put up with it to maintain the regularity of the history points grid,
but while the plotting slice, we have to separately cut the under-slope
regions. In the figures below, we deliberately did not do that, to show the pressure-gradient
method’s advantage: for it, it is not necessary.
Results
of pressure-gradient will be represented in black-and-white palette (black for
higher values), following the Schlieren method. As one can see in what follows,
it will be useful, because out-of-bounds regions (appeared in secondary
post-processing mesh, but in fact not belonging to computational domain, like
right white triangle on Fig. 2(b)) will automatically be colored white in this
painting scheme. It is important, for instance, in case of complex-shaped
domain like those with plateau or underwater peak (see below).
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a)
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b)
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Fig. 3: Attractor
in model trapezium domain: a)
snapshot (cm/s), b) pressure gradient method
Before using
the new method for specific cases, let us make sure that it works properly on
classical cases. For this reason we apply it to the well-studied attractor flow
[14,28,29] in trapezium geometry with linear stratification profile. The
laminar attractor is clearly visible even if the
velocity-component visualization is used; we consider it to validate that the
new-proposed method works for a known case not worse than the methods used
before.
It is so;
moreover, one can see an advantage of the pressure-gradient method: the bottom right
ray looks brighter (Fig. 3(b)), indicating the more energy accumulation on the
first attractor ray. It is known from the precious studies [28, 30], but is not
visible on the velocity snapshot on Fig. 3(a).
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a)
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b)
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Fig. 4:
Attractor in domain with halocline salinity profile: a)
snapshot
(cm/s), b) pressure gradient method
The next case is non-linear
salinity. Vertical stratification is principal for wave attractor formation
hence it requires buoyancy [1, 5]. In model set-ups it widely considered to be
linear [1, 2, 14, 28]. For real systems it is no more so [31–33], and the
attractor’s properties change. For instance, as it was found for a salinity
profile with sharp-gradient density range (halocline), typical for
subequatorial basins [32], attractors in such system accumulate more energy
than those in the same geometry with linear stratification [20]. The
instability develops non-homogeneously in basin space (on Fig. 4(a) one can see
that the upper part is more disturbed than the lower one). Pressure gradient
visualizes clearly the attractor contour as well as the secondary waves of
instability (Fig. 4(b)), which is incapable for
snapshot.
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a)
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b)
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Fig. 5:
Attractor in domain with large aspect ratio: (a)
snapshot
(cm/s), (b) pressure gradient method
The real systems where attractors
can exist are typically enlarged horizontally [35, 36], thus, it is reasonably
to consider attractors in domains with large aspect ratio. Attrac-tors of this
type are characterized by a greater energy accumulation, comparatively to those
in domains with comparable sizes [18] (even in a greater degree than a
halocline attractors from previous subsection [20]); and, subsequently, the
more energy accumulation leads to earlier instability production (with slighter
forcing) that ’disturbs’ the main attractor view. On Fig. 5(a) one can hardly
guess the presence of an attractor. The pressure-gradient method allows
revealing its contour (Fig. 5(b)) considerably clearer.
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a)
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b)
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Fig. 6: Attractor in domain with underwater mountain: (a)
snapshot
(cm/s), (b) pressure gradient method
Despite the model
attractor basic setup presumes that an attractor occupies the whole domain
(thus the side walls the attractor reflects from can be supposed to extend bot-tom
to surface), normally it is not so easy, and a real attractor reflects from
underwater structure which has a shape of a mountain or plateau slope which top
not necessary reaches the surface [34]. This fact made us to investigate an
attractor in such peculiar geometry in [21]. It was discovered that a domain
with an underwater peak may lead to a qualitatively new flow pattern: in such
geometry there can appear an additional ”viscous” coherent structure. The main
feature is that it cannot be predicted using the inviscid approximation
(ray-tracing), and disappears if the viscous in the simulation tends to zero;
thus, for small viscosities it is hardly seen (see Fig. 6(a): the main
attractor on the left, with the ”viscous” structure poorly visible on the
background). Pressure gradient allows to fully visualize both main and
collateral attractor structures better than
slice (cf. Fig. 6(a) and 6(b)).
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a)
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b)
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Fig. 7:
Attractor in domain with underwater plateau: (a)
snapshot
(cm/s), (b) pressure gradient method
No less important geometry
is that with the mid-depth underwater plain. This case is interesting by a new
instability formation type [24]. For this geometry type, we simulate an
asymmetric (2,1)-type attractor [1] with moderate instability intensiveness
(Fig. 7(a)). Despite the structure is resolved quite good by vy
spashot, pressure-gradient Schlieren method reveals also the background structure
(Fig. 7(b)), which is visible worse on the snapshot. Herewith, this case
shows the limitations of the method: too heavy turbulence can still overlay the
attractor, despite for moderately-turbulent flows it is better than velocity
component snapshot.
Previously,
wave attractors were visualized by velocity. However, this method shows clearly
enough only laminar attractors; such things as secondary instability waves, inhomogeneity
of their production over volume or another coherent substructure presence
complicates the visualization. The recent investigations of wave attractors
faced with the phenomenon mentioned, motivated the reconsideration of
approaches for wave attractor visualization.
Following the
gas dynamics that widely uses the numerical Schlieren method, we adopted the
latter for an incompressible flow to apply to wave attractor problems. In
stead of density gradient, we consider the pressure gradient. By
an example of a set of known cases, it was shown that the method proposed can
be successfully used, revealing both attractor and instability structure. It
was shown that for moderate instability pressure gradient Schlieren analogue
visualizes the structure more clearly, which makes this method to be preferable
for wave attractors.
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