Detailed description of our objective trough/jet identification technique.
Commonly used
methods of African Easterly Wave (AEW) identification have limitations that
may, on occasion, give a less than ideal representation of the synoptic weather
systems over tropical North Africa. For example, using the point at which the
African Easterly Jet (AEJ)-level meridional wind is equal to zero (perhaps the
most often used method) cannot be used reliable in regions where there is a
'background' meridional flow. Using relative vorticity at the same level often
leads to confusions between the multiple scales of which an AEW is composed.
Some studies have used bandpass filtered winds that give a clear indication of
the synoptic scale weather systems, but these methods cannot be employed
reliably in a real time situation. As a solution, we suggest that AEW trough
axes should be defined based on AEJ-level streamfunction (y), as using y in the
tropics is somewhat analogous to using geopotential height in the mid-latitudes.
Streamfunction has the distinct advantage that the elimination of the divergent
flow reduces noise associated with individual mesoscale convective systems
(MCSs) and offers a smoother field that presents less technical difficulties
for the computation of objective AEW trough axes. Due to the fact that most
numerical models and reanalysis products include this level, we define the AEW
trough axes on the basis of y at 700hPa .
For orientation, an
example of the 700hPa streamfunction field over tropical North Africa during
September 2004, as computed from a global model, is shown in Fig.1 below.
Recalling that the zonal (uy) and meridional (vy)
components of the streamfunction wind (
) are given by:
(1) and
(2),

FIGURE 1 - Example Streamfunction
Field (scaled by 10-6)
The streamfunction
wind components (i.e. the non-divergent wind components) for the example period
shown in Fig.1 (with a slightly zoomed area) are plotted in Fig.2(a). Note the
analogy of streamfunction in the tropics to geopotential height in the
mid-latitudes.

FIGURE 2a - Non-divergent wind components (vectors) on the
Streamfunction field shown in figure 1.
Using the non-divergent wind components, we then compute ‘streamfunction
vorticity’ (
) defined as:
(3).
is a standard gradient
operator and the computed streamfunction vorticity is implicitly a vertical
component. A map of this quantity for the example period is displayed in
Fig.2(b), superimposed on the streamfunction field below. Note that from the
streamfunction vorticity the position of a trough or ridge can be simply
defined to be where:
(4)

FIGURE
2b - 'Streamfunction vorticity' computed from non-divergent wind
components
plotted on top of streamfunction. Only positive values are
shown
for clarity. Vorticity values scaled by 105.
However,
the definition of trough and ridge lines based solely on the advection
streamfunction vorticity of is only mathematically correct for idealized
2-dimensional waves (i.e. where vy is a function of only one
horizontal direction). Those that occur over tropical North Africa are not of
this type, as Fig.1 clearly shows. This is because a large contribution to the
total streamfunction vorticity comes from horizontal shear across the AEJ. The
advection of streamfunction vorticity due to the westwards propagation of AEWs
is obscured by the advection of streamfunction vorticity associated with
relatively small fluctuations in the position or nature of the AEJ. A simple
solution is achieved by partitioning the streamfunction vorticity into shear
vorticity and curvature vorticity components:
(5).
Plots of these two components
for the example period are shown in Fig.2(c) below.

FIGURE
2c - Streamfunction shear (contoured) and curvature
(shaded)
vorticity computed from non-divergent wind
components
plotted on top of streamfunction. Again,
only
positive values are shown for clarity. Vorticity values
are
scaled by 105.
Now, the AEW trough and ridge axes are then re-defined to be where:
(6).

FIGURE 2d - Advection of curvature vorticity equal zero
contour on
top of the original streamfunction field.
In order
to differentiate between AEW troughs and ridges, these lines are only plotted
in regions where curvature vorticity exceeds some threshold (in the case of
troughs) or is below some other threshold (in the case of ridges). This has
been applied in Fig.2(e), overlaying a mask that obscures region in which the
streamfunction curvature vorticity is below 0.5x10-5s-1 (the
same threshold used for our plots), resulting in only trough lines being
displayed.

FIGURE 2e - Advection of curvature vorticity equal zero
contour
in regions where curvature vorticity exceeds 0.25x105
s-1.
However, because there will be instances where curvature reaches a local
minimum, yet is still positive (or conversely reaches a local maximum, yet is
still negative) a further masking diagnostic is required, to remove spurious
lines that are not removed by the streamfunction curvature vorticity mask:
(7),
where K is
positive for plotting troughs and negative for plotting ridges. For our plots
we simply use a value of K=0. This final mask is applied, along with a mask
that removes trough lines in regions where uy is greater than –8ms-1
(since we are looking only for eastwards moving disturbances), in
Fig.2(f) below.
It can also be noted that lines along which streamfunction shear vorticity (
) equals zero denotes the
cores of streamfunction wind speed maxima or minima. This is used by also
noting that wind speed maximum can be removed by applying the following
graphical mask:
(8),
is the unit vector perpendicular to the Earth’s
surface. The AEJ axis has been plotted as a dashed line in Fig.2(d-f) for
completeness.

FIGURE
2f - FINAL PRODUCT....Advection of curvature vorticity equal
zero
contour in regions where curvature vorticity exceeds 0.25x105 s-1,
where
the zonal component of the non-divergent wind is less than zero
and where eq(7) is greater than zero. All
plotted on top of the original
streamfunction
field from figure 1.
A page that shows these 'background' diagnostics for the
current analysis time can be found here.