extended self-similar scaling law of multi-scale eddy structure in wall turbulence
TRANSCRIPT
Applied Mathematics and Mechanics
(English Edition, Vol. 21, No. 9, Sep 2000)
Published by Shanghai University, Shanghai, China
Article ID : 0253-4827(2000)09-1016-08
E X T E N D E D S E L F - S I M I L A R SCALING LAW OF M U L T I - S C A L E
E D D Y S T R U C T U R E IN WALL T U R B U L E N C E *
JIANG Nan ( ~ ~r WANG Zhen-dong (2E~3~, ) l ' a , SHU Wei ( ~ t-~) I'~"
( 1. Institute of Mechanics LNM, Chinese Academy of Science, Beijing 100080, P R China;
2. Department of Mechanics, Tianjin University, Tianjin 300072, P R China)
(Communicated by Li Jia-chun)
Abstract : The Iongitudinal fluctuating velocity of a turbulent boundary layer was measured
in a water channel at a moderate Reynold~ number. The extended selfl simiIar scaling law of
structure function proposed by Benzi was verified. The longitudinal fluctuating velocity in
the turbulent boundary layer was decomposed into many multi-scale eddy structures by
wavelet transform. The extended self-similar scaling law of structure function for each scale
eddy velocity was investigated. The conclusions are 1 ) The statistical properties of
turbulence could be self-similar not only at high Reynolds number, but also at moderate and
low Reynolds number, and they could be characterized by the same set of scaling exponents
~ t ( n ) = n/3 and ~2( n) = n/3 of the fully developed regime. 2) The range of scales
where the extended self-similarity valid is much larger than the inertial range and extend~ far
deep into the dissipation range with the same set of scaling exponents. 3 ) The extended self-
similarity is applicable not only for homogeneous turbulence, but also for shear turbulence
such as turbulent boundary layers.
Key words: wavelet transform; eddy; scaling law
CLC number: 0357 Document code: A
Introduction
Much work has been devoted in the last few decades to the measurement and modeling of the
scaling law of structure function of turbulent flows. The so-called " velocity structure funcdon of
order n " for turbulent flows is def'med as ( & V ( r ) " ) , where/', V ( r ) = V( x + r) - V( x ) is the
velocity component increment parallel to the relative displacement r of two positions separated by
a distance of r in the flow field.
Let us remember that the research of structure function scaling law is usually limited by the
following assumptions: 1) in the full developed turbulent flow so that the Reynolds number is
inf'mite; 2) local homogeneous and isotropic; 3) for r in the inertial range.
* R e c e i v e d d a t e : 1999-09-03 ; R e v i s e d d a t e : 2000-06-08
F o u n d a t i o n i t e m : the National Natural Science Foundation of China (19732005); Doctoral
Program Foundation of the Education Committee of China (97005612); the National Climbing Protect
Biography: JIANG Nan (1968 ~ ) , Associate Professor, Doctor
1016
Self-Similar Scaling Law of Multi-Scale Eddy Structure 1017
The expectation of the scaling law is that
(AV(r) " ) ~ r~"> ('7<< r<< L), (a) where 7/is the dissipate length, L is the integral scale and ~(r~) is called scaling exponent. The
scaling law is an indication of the existence of scale invariance in turbulence.
For the third-order structure function, one can deduce the following Kolmogorov relation
within above assumptions from the Navier-Stokes equations:
4 ? ( A V ( r ) z ) (2) ( A V ( r ) s) = - ~ e r + 6v ?r '
where V is the kinematics viscosity, (} stands for ensemble averaging and e is the average rate of
energy dissipation per unit mass. Within the inertial range, the second term on the right-hand side
in Eq. (2) can be neglected
4 ( ~ v ( , ) 3) = _ 3 - ~ , .
This means that: ~(3) = 1.
The classical Kolmogorov theory predicts that: ~(r~) -
(3)
(4)
'~ (5 ) 3
Benzi et al ~l] recently showed evidence for the so-called extended self-similarity in their
measurements of turbulence generated either by a wake flow past a cylinder or by a jet at moderate
Reynolds number:
( A V ( r ) " ) = A n I ( A V ( r ) 3 ) I ~(~) = B~<] A V ( r ) 3 [)~'-(~), (6)
where Am and B, are two different sets of constant independent of r . Since the third-order structure
function ( A V ( r ) 3 ) is proportional to r , instead of plotting the nth-order structure function
( A V ( r ) " ) against r , they plotted the nth-order structure function ( A V ( r ) " ) against the third-
order structure function ( A V ( r ) 3 ) . Eq. (6) is valid not only in the fully developed turbulence
but also at moderate and low Reynolds number, even if no inertial range is established.
Moreover, it has been shown that the range of scales where Eq. (6) valid is much larger than the
inertial range and extends far deep into the dissipation range.
Stolovitzky (1993)[z] repeated the experiments of Benzi and pregented their experimental
results. They measured the time series of the fluctuating velocity at a moderate Reynolds number
in a turbulent boundary layer over a flat plate and investigated the extended self-similarity of the
structure function. They revealed that, for low-order moments, a single scaling law with the
same scaling exponents not far from ~ ( n ) = n /3 for dissipate as well as inertial range.
However, as the order of the moment increases, the scaling law in the dissipate region and in the
inertial region separates out. Within the dissipate region, the scaling exponents are nearly given
by ~ ( n ) = n /3 with ~1(8) = 2 .66 , ~ ( 8 ) = 2 .42 . For r in the inertial range, the plot of
versus consists of another linear region of slope ~1 (8) = 2 .05 , ~z (8) = 2.12 slightly less than
~ ( n ) = n / 3 , joined by a smooth transitional region. The difference between the two regimes
becomes increasingly apparent for higher n .
1 Experimental Apparatus and Techniques
Experiments were conducted in a full-developed turbulent flow of a free-surface water
channel. Velocity measurements in the water channel were taken by TSI anemometer system with
1018 JIANG Nan, WANG Zhen-dong and SHU Wei
a TSI model 1210-20W single-sensor hot-fi lm probe and a TSI model 1218-20W single-sensor
hot-f i lm boundary probe. The coming stream velocity and intermediate Reynolds number were
U~. = 0 . 2 8 m / s and Re�9 = 2570 respectively. The hot-Trim probe was located at y+ = 16 above
the lower wall o f the channel. Fig. 1 shows the longitudinal fluctuating velocity signal obtained
from the hot-f i lm probe located in the near wall region of a turbulent boundary layer.
0.6
0 v
" - 0 . 6 0 1 2 3 4 5 6 7 8 9
t t/s
Fig. 1 Longitudinal fluctuating velocity in the near wall region of
a turbulent boundary layer (y+ = 16)
E x t e n d e d Self-Similar i ty of F luc tua t ing Veloci ty S t ruc tu re Func t ion in
Wall Turbulence
In F ig .2 , we show the structure function log I (AV( r ) " > l against log I ( A V ( r ) 3 ) I in inertial
range and in dissipation range where it is shown that the nth-order structure function has apparently
different scaling laws in dissipation range and in inertial range. The slopes in dissipation range are
much smaller than those in inert ia/range. Fig .3 is a plot of ~1 ( n ) in (6) against n in inertial range
where the scaling exponents ~1 ( n ) are aligned on two curves of which one is larger than ~1 ( n ) =
n/3 for odd-order and the other is smaller than ~l ( n ) = n/3 for even-order.
0.01
0.001
.~ 0.0001
<3 v
1E - 005
1 E - 0 0 6
/ / - -
,, -- 2 f / /~ / /
/ /
/ / / / /
r t = 4 ~ . . / /
/
/ , v /
5"5 I �9 5.0 ' 4.5 : " 0 � 9 4.0 i 3.5 i . . . . 00
3.0 ...... ! - �9 ~ �9 v
2.5 2.0 1.5 1.0 0.5
0 . t . . . . . . . . i . . . . , . . . .
l E - 0 0 6 1 E - 0 0 5 0 . 0 0 0 1 0 . 0 0 1 0.01
<av(~) ~) Hg.2 Structure functionlog I (AV(r) ~) I Hg.3
against log I ( A V ( r ) 3) I
. . . . . �9 ' O
: " O Q
Q t 1 '
. . . . i . . . . . . , . . . . ; ~ , , n , , ,
2 4 6 8 10 12 14 16 n
Plot of the scaling exponents
~l ( n ) against n
In F i g . 4 , we show the structure function log(I A V ( r ) ~ I> against log(I A V ( r ) 3 1) . It is
shown that the nth-order structure function has apparently different scaling laws in dissipation range
and in inertial range. The slopes in dissipate range are much smaller than those in inertial range.
Fig .5 is a plot o f ~2 ( n ) in (6) against n in inertial range where it is shown that ~2 ( n ) = n /3 .
3 Multi-scale Eddy Structure Extended Self-slmilariW Scaling Law
As far as turbulence is concerned, wavelet has special physical meaning. " E d d y " provides
�9 Self-Similar Scaling Law of Multi-Scale Eddy Structure 1019
0.01 n =2
i . / 0.001 '
~" n = 4/.,J"" / e l / o.ooo ~ ~ . ; , , , - ~ i . . . . . .
�9 rt = 6 / + " t I I ;
IE - 005 i/ . . .
" o ' . | ' " o . o l ' o .
<<xV(r) 3)
5.0 4.5 4.0 3.5
,-~ 3.0 "~ 2.5
2,0 1,5 1.0 0.5
0
I
2 4 6 8 10 12 14 I1
16
Fig.4 Structure function log( I A V(r)" I ) Fig.5 Plot of the scaling exponent
against log(I AV(r) 3 I ) ~z(n) against n
the most suitable elementary decomposition of turbulence and is first introduced by Tennekes and
Lumley [3] . According to them, eddies are fairly broad and self-similar contributions in the
spectral domain that, unlike "waves" , correspond to localized contributions in the physical
space. They are localized both in spatial space and in time space. Fourier Transform does not
take into account localized eddies in physics and therefore does not suit to decompose turbulence.
This leads the physical meaning of Fourier Transform lost. Wavelet representation provides the
decompositions of turbulence into eddy modes and the wavelet projection could be a very good
alternative. "Eddies" are to turbulence study, what wavelets are. Fig .6 shows the typical shape
of an "eddy" self-correlation function proposed by Tennekes and Lumley based on turbulence
interpretation. Fig.7 shows the shape of an "eddy" self-correlation function of wall turbulence
obtained by wavelet decomposition from experimental measured signals. As a new tool, wavelet
transform can be devoted to the use for decomposing turbulence into eddies modes instead of
Fourier Transform. Fig. 8 shows the reconstructed single scale eddy velocity by wavelet
transformation of the sampled fluctuating velocity signal shown in Fig. 1.
/ / " ~ \ \
/ / / / I / \\\\
2 /k 0.1k 0.6k x 1.6k 10k Ink I i
Fig. 6 An eddy seN-correlation function of wave number k and wavelength 27r/k [31
In Fig .9 , we show the structure function log I ( A V l ( r ) ~) I against log I ( A V l ( r ) 3 ) I where
the nth-order structure function is aligned on a single line of slope ~l ( n ) = n / 3 . Fig. 10 is a
plot of ~ l ( n ) in (6) against n where it is shown that ~ l ( n ) -- n/3.
1020 JIANG Nan, WANG Zhen-dong and SHU Wei
1.5
1.0
0 .5
0 .0
- 0 . 5
- 1 . 0
o.6
1 . l i E - 01-[ . I ]
8 . l i E - 02:
6 . l i e - 02'
4 . l i E - 02:
2 . l i e - 02:
0 . l i e + l i ,
F i g . 7 An eddy sel f -correla t ion funct ion ob ta ined by wavele t t r ans fo rm
0.06~ " ll
_
1000 2000 3000 3000
0 1000 2000 3000 4 0 0 0
0 i5 'Q 1000 2000 3000 4 0 0 0
0 I 0 0 0 ' 2000 3000 4 0 0 0 0 .2
0
- 0 " 2 0 1 000 2 000 4 000 0 . 1 5 / 3 0 ~
0.12'10 1 l iO 2 000 3 000 4 000
0 1000 2000 3000 4 0 0 0
Fig . 8
0.01
0.001
0.000 l
~- I E - 005
<1 1E - 006
1E - 007
1E - 008
Recons t ruc ted veloci ty s ignal for each single scale eddy by wave le t decompos i t ion
I E - 008 1 E - 005i
0.1 0.01
0.001
0.0001
1E - 005
IE - 006
1E - 007 1E - 008
0.01 I
. . . . . o.ooo t )
1 E - 006 ~- ] , - , - i E _ 0 0 7 [ 1 E T , 0 0 8 ' , t E - O 0 5 ,,
IE - 009 I E - 007 0.000 1 1 E - 0 0 9 q E - 007: 0.0001 1 E - 006 0.001 1E - 006 . 0.001 1 E - 006
( •
a = 8 a = 16 a = 32
F i g . 9 The n t h - o r d e r structure funct ion log( I &Vt ( r ) " I ) aga ins t
log( I A Vz ( r ) 3 I ) for each scale eddy
1E - 009 1 E - 007 0.000 0.00t
Self-Similar Scaling Law of Mult i -Scale Eddy Structure 1021
0.01
0.001
0.000 1
1E - 005
I E - 006
1E - 007 IE - 009 I E - 007
I E - 008 1E - 005
0.0001
1
0.1
0.01 ---- - - ~
0.001 - - ~
0.0001 / j ' ' ' /
1E- 005 'l l z - 008 IE - 005~ �9 1 E - 0 0 6
1E - 009 1E - 00T 0.000 IE - 006 0.001
a = 6 4
1E - 006
a = 128
1
0.1
0.01
0.001
0.000 l
1E - 005
IE - 006
0.t301
E: oo8 !z-,,oo5 1 E - 009 1 E - 007. 0.0001
tE - 0t36 0.00t
a = 256
1
0.1
0.01
0.00l
0.0001
1E - 005 1E - 009 1E - 007
IE - 006
f
, /
. - ~ / " j
1E - 008 1E - 005
0.0001 0.001
0.01
0.001
0.000 1
1E - 005
1E - 006 IE - 008 1E - 005 i ,i i , i ,~
1 E - 009 1 E - 007 ' 0.000 1 1 E - 006 0.1301
Fig . 9
a = 512 a = 1024
The n th-order structure function log( I AVi ( r ) " I ) against
log( I A V z ( r ) 3 I ) for each scale eddy
3.5 3.0 2.5
~" 2.o 1.5 1.0 0.5
0
3.5 3.0 2.5 2.0
1.5 1,0 0.5
0
i , ; ' I I i
2 3 4 5 6 7 8 9 1 0 n
a = 8
./ ./
/ : / / "
/. �9 //
X / /
z i i i , , i i
2 3 4 5 6 7 8 9 1 0
3 . 5
3.0 / /
2 .0 1.5 . / 1.0 . . . . . . . 0.5 / / . ,
0 ~ ', , , , i , L
1 2 3 4 5 6 7 8 9 1 0
3 . 5 ' 3.0 2.5 2.0 1.5 1.0 0.5
0
?l
a = 1 6
3.5 3.0 2.5 2.0 1.5 1.0
"l 3.5 . . . . . [ / " 3.0
: / - 2.5 / , / 2.0
/ " l . 5
1 . 0
: / 0 . 5 0 , . . . . , i i
2 3 4 5 6 7 8 9 1 0 rt n
, / /"
/
i i i i , , , i
2 3 4 5 6 7 8 910 TL
a = 3 2
//[ . / / / / ]
/ / /
I . : (
2 3 4 5 6 7 8 9 1 0
a = 64 a = 128 a = 256
Fig . 10 Plot o f ~t ( n ) against n for each scale eddy
1022 J1ANG Nan, WANG Zhen-dong and SHU Wei
3.0 2.5 2.0 . . . . . . . . : ~
1.5 1 1 .o : 0 . 5 . . . . . . . .
0 . . . . . i . . . . . 2 3 4 5 6 7 8 9 1 0
a = 512
3.5 : . . , / 3.0 - / 2.5 2.o i / /
1.5 /
1.0 / 0.5 .
0 . . . . . , , ,
2 34 5 6 7 8 910 11
a = 1024
H g . 10 Plot of ~t ( n ) against n for each scale eddy
F ig . 11 is a p lo t that l o g ( I & V t ( r ) ~ I ) versus l o g ( I A V L ( r ) 3 I ) w h e r e the n th -o rde r
structure funct ion i s a l igned on a s ingle l ine o f s lope ~_ ( n ) = n / 3 . F i g . 12 is a p lo t o f ~,_ ( n ) in
( 6 ) against n where it is also shown that ~_
0.001 0.1
/ 0.01
0.0001 " " ~ ' / " ......... 0.001
IE - 005 IE o08 IE-'oo~ o.ooo x
a = 8
n) = n / 3 .
J
7 / o.oool /
~E- oo5 ~E-005 , 0.ooi 1E-008 0 . 0 0 0 1 0.01
0.1
0.01 f /
O. 001 . / "
. / i "
0.0001
~E-oo5 i z - o o s ,, o.om 1E- 008 0.0001 0.01
a = 1 6 a = 3 2
0.1
o.01
0.001
0.0o01
1E - 005
f /
/
I E - 005 0.001 �9 I , -)- ,
0.0001
a = 6 4
0.01
0.1
0.01 . . . . . . - /
/ / 0 . 0 0 1
/ / / 0.000 1
[E - 005 0 . ( 3 0 l IE IE-008005 , 0 .0~1
t
0.01
a = 128
0.11 I
o.01
0.001
0.o0o 1
IE - 005
/ i /
/ . / *
/ -
1E -005 i 0.(301 1E-008 0.0001
a = 256
0.01
0.1
0.01
0.001 i
/ o.0oo 1 . . . . i
1E- 0 0 5 1 E - 005 0.001 1 E - 0 0 8 0.01301 0.0l
0.1
0.Ol
o.ool
0.OOOl
IE - 005 1E - 008
/ /
o.00Ol o.01
Fig. 11
a = 512 a = 1024
The nth-order structure function log( I A Vz ( r ) " I )
versus log( I A Vt ( r)3 I ) for each scale eddy
Self-Similar Scaling Law of Multi-Scale FAdy Structure 1023
3.5 3.0 2.5 2.0 1.5 1.0 0.5
3.5 3.0 2.5 2.0 1.5 1.0 0.5
0
/ / " / *
/
.f
s
2 34 56 7 8910 n
a = 8
i / / i
2 3 4 5 6 7 8 9 1 0 II
a = 6 4
3.51 3.0: 2 . 5 2.0 1.5 1.O 0.5
0
3.5 3.0 2.5 2.0 1.5 1.0 0.5
0
3.5 3.0 2.5 2.0 1.5 1.0 0.5
0
2 3 4 5 6 7 8 9 1 0 n
a = 512
Fig. 12
2 3 4 5 6 7 8 9 1 0
a = 1 6
"l : �9 / /
/ / / ' / "
2 3 4 5 6 7 8 9 1 0 /l
3.5 3.0 2.5 2.0 1.5 1.0 0.5
0 ; i ; i , i ~ ; 2 3 4 5 6 7 8 9 1 0
n
a = 3 2
3 5 3.0 . , : :
2.5 " //
2.0 �9 / / ' : l 1.01"5 /./// i 0.5
2 3 4 5 6 7 8910 rL
a = 128
3.5 1 3.0 . . . . ;,,/"
7 / / 2.0 . /
i / 1.0 71 / / /
0.5 0
2 3 4 5 6 7 8 9 1 0 I1
a = 1024
Plot ~2 ( n ) against n for each scale eddy
a = 256
4 C o n c l u s i o n s
1) The statistical properties of turbulence could be self-similar not only at high Reynolds
number, but also at moderate and low Reynolds number , and they could be characterized by the
same set of scaling exponents of the fully developed regime.
2) The range of scales where the extended serf-similarity valid is much larger than the
inertial range and extends far deep into the dissipation range.
3) The extended self-similari ty is applicable not only for homogeneous turbulence, but also
for shear turbulence such as turbulent boundary layers .
R e f e r e n c e s :
[1] Benzi R, Ciliberto S, Tripiccione R, et al. Extended self-similarity in turbulence f l o w s [ J j .
Physical Review E, 1993,48 ( 1 ) : 29 ~ 32.
[2] Stolovitzky G, Sreenivasan K R. Scaling of structure functions[ J ] . Physical Review E, 1993,48
(1) : 3 3 - 36.
[3] Tennekes H, Lumley J L. A First Course in Turbulence [ M ] . Cambridge Massachusetts and
London, England: M1T Press, 1972.