basic definitions . reynolds averaging
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Statistical theory of the isotropic turbulence (K-41 theory) 1. Basic definitions of the statistical theory of turbulence Lecture 3. Basic definitions . Reynolds averaging. Basic definitions . Correlation function. Correlation function Correlation function in homogeneous turbulence - PowerPoint PPT PresentationTRANSCRIPT
Lehrstuhl fürModellierung und Simulation
Statistical theory of the isotropic turbulence (K-41 theory)
1. Basic definitions of the statistical theory of turbulence
Lecture 3
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Basic definitions. Reynolds averaging Basic definitions. Reynolds averaging
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3
ij i j
ij i j
R ( x,r ) u ( x )u ( x r ),
R ( r ) u ( x )u ( x r ),
Basic definitions. Correlation function Basic definitions. Correlation function
2
0
i iii
i
ij ii j j
u ( x )u ( x r )( x,r ) ,
u ( x )
L ( x ) ( x,x )dx
2
0
i iii
i
i ii
u ( t ,x )u ( t ,x )( ,x ) ,
u ( t ,x )
T ( x ) ( ,x )d
Correlation functionCorrelation functionCorrelation function in homogeneousCorrelation function in homogeneousturbulence turbulence
Autocorrelation functionAutocorrelation function
Integral lengthIntegral length
Autocorrelation temporal functionAutocorrelation temporal function
Integral time Integral time
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SamplesSamples
4
0 20 40 60 80 100 120 140 160point num ber across the m ixer
-0.40
-0.20
0.00
0.20
0.40
0.60
0.80
1.00
Aut
ocor
ella
tion
func
tion
of f
50
mm
50 m
m
Resolution 300 Resolution 300 µµ
2D2D
AA
BB
CC
AABBCC
Typical form of the autocorrelation coefficient. Scalar turbulenceTypical form of the autocorrelation coefficient. Scalar turbulence
PLIF Measurements of the LTT RostockPLIF Measurements of the LTT Rostock
Physical meaning of sign changePhysical meaning of sign change
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SamplesSamples
5
50
mm
50 m
m
Resolution 300 Resolution 300 µµ
2D2D
Typical distribution of the integral length along the jet mixer. Typical distribution of the integral length along the jet mixer. Scalar turbulenceScalar turbulence
PLIF Measurements of the LTT RostockPLIF Measurements of the LTT Rostock
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Typical autocorrelation coefficient Typical autocorrelation coefficient along the jetalong the jet
6
(from Ginevsky et al. (2004) Acoustic control of turbulent jets. Springer)
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1 along upper border of nozzle at x/D=0.51 along upper border of nozzle at x/D=0.52 along the jet axis at x/d=3.02 along the jet axis at x/d=3.0
autocorrelation coefficient of the autocorrelation coefficient of the longitudinal velocity longitudinal velocity
Isotropic turbulenceIsotropic turbulence
7
2 2
2t t
u (x)u (x r) r F(r) G(r) u f ,
u (x)u (x r) u g G(r).
l l
t t
t t
u (x)u (x r) u (x)u (x r)f (r) ,g(r) ,
u (x)u (x) u (x)u (x)
l l
l l
2t t i iu u (x)u (x) u (x)u (x) .....u (x)u (x), l l
ij i j ijR F(r)r r G(r) 2ij i j ij2
f gR u ( r r g )
r1 f
g f r2 r
2t t i iu u (x)u (x) u (x)u (x) 1 / 3u (x)u (x), l l
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8
f
g
Taylor longitudinal length Taylor longitudinal length
Taylor transverse length Taylor transverse length
/Re u / g
Taylor Reynolds number Taylor Reynolds number
2 22 4
2 2 2
2 2
2 2 2
2
2
1 f f 1f (r) 1 (0)r O(r ) (0)
2 r r 2
r g 1f (r) 1 (0)
2 r 2
rg(r) 1 .
f
f g
g
Isotropic turbulenceIsotropic turbulence
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Correlation function in Fourrier spaceCorrelation function in Fourrier space
9
3
1
8
ikr
ikr
ˆf ( r ,t ) f ( k ,t )e dk ,
f̂ ( k ,t ) f ( r ,t )e dr
3
1
8
ikr ikr
ij ij ij ijR ( r ) ( k )e dk , ( k ) R ( r )e dr
1 11 1 1 1 2 3 2 3
10 0
2
ik rij ij ij( k ) R ( r , , )e dr ( k ,k ,k )dk dk
Usually it is possible to measure only the Usually it is possible to measure only the „„One dimensional spectral Function“One dimensional spectral Function“
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Proof
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1 1
1 1
1 1 1
1 1 1
1( ,0,0) ( ,0,0) ,
2
( ,0,0) ( ,0,0)
ik rij ij
ik rij ij
k R r e dr
R r k e dk
1 2 3 1 2 3 1 2 3( , , ) ( , , ) ikrij ijR r r r k k k e dk dk dk
1 1 2 3 2 3( ,0,0) ( , , ) ,ij ijk k k k dk dk
1 11 1 2 3 2 3 1( ,0,0) ( , , ) ik r
ij ijR r k k k dk dk e dk
Spectral density of the kinetic energySpectral density of the kinetic energy
11
0
0
1 1
2 2ii ii ii
ii
k
TKE R (o ) ( k )dk ( k )dk ,
E( k ) ( k )dk ,
TKE( k ) E( k )dk ,
E(k) dk is the contribution of oscillations with the wave numbers k<k<k+dkE(k) dk is the contribution of oscillations with the wave numbers k<k<k+dk to the kinetic energy of the turbulent motion.to the kinetic energy of the turbulent motion.E(k) is the density of the kinetic energy depending on wave numbers. E(k) is the density of the kinetic energy depending on wave numbers. The dependence E(k) isreferred to as the energy spectrumThe dependence E(k) isreferred to as the energy spectrum
3
1
8
ikr ikr
ij ij ij ijR ( r ) ( k )e dk , ( k ) R ( r )e dr ij i jR ( r ) u ( x )u ( x r )
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