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ˆ
(
)
from streamwise vorticity
Uyz
therefore depends only on
y
and
z
. The authors assume
that the field
. The basic flow
ω
,
x
ˆ
(
)
() (
)
(
) ( )
Uyz
,
=
Uy
+ Δ
u
2 cos
β
zgy
s
[5.55]
ˆ
ˆ
VW
==
0
accurately models the flow engendered by a streak extending
outside of the buffer sublayer
, rather than only in the near-
wall sublayer at
, where the quasi-streamwise
structures are mainly concentrated. The distribution
y
+
≤
30
()
Uy
in [5.55] is the turbulent profile of the mean lo
ca
l velocity of
the channel flow, the Reynolds number is
Re
=
U h
ν
=
2, 000
,
c
()
g y
is an amplitude function which satisfies the non-slip
conditions at the wall and is of the form
(
)
()
.
The analysis is limited solely to the bottom wall of the
channel. The adjustment parameter
g
yy
∝
exp
−
ς
y
2
can be used to locate
the maximum wall-normal vorticity surrounding the streak
ς
ˆ
(
)
[5.56]
ω∂
ˆ
=
Uz
∂
=
β
Δ
u
2
y
max
s
in the buffer sublayer
20
, in accordance with what is
observed in fully developed near-wall turbulence. As the
streaks are typically spaced around 100 inner variables
apart, the wavenumber
y
≤≤
30
πβ
+
=
. The flow
is periodic in the spanwise direction. The periodicity imposed
means that the disturbances must be in accordance with
Floquet theory
20
[DRA 81], i.e. it must be of the form
β
is such that
2
100
s
s
20 Numerous references are to be found in the existing literature on the
stability of periodic flows in general and
time
-periodic flows in particular.
For example, readers could consult [AKH 91] for a specific application of
the Floquet theory to oscillating Stokes flows.
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