liu turbulence sas modeling
TRANSCRIPT
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Scale-AdaptiveSimulation (SAS)Turbulence Modeling
F.R. MenterANSYS Germany GmbH
Torbjrn VirdungANSYS Sweden AB
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Unsteady RANS Based Models
URANS (Unsteady Reynolds averaged
Navier Stokes) Methods URANS gives unphysical single mode unsteadybehavior
Some improvement relative to steady state (RANS)but often not sufficient to capture main effects
Reduction of time step and refinement of mesh donot benefit the simulation
SAS (Scale-Adaptive Simulation) Method
Extends URANS to many technical flows Provides LES-content in unsteady regions Produces information on turbulent spectrum Can be used as basis for acoustics simulations
URANS
SAS-URANS
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Assumptions Two-Equation
Models
Largest eddies are most effective in mixing
Two scales are minimum for statistical description oflarge turbulence scales
Two model equations of independent variables define
the two scales Equation for turbulent kinetic energy is representing the large scale
turbulent energy
Second equation ( , , kL) to close the system Each equation defines one independent scale
Both - and -equations describe the smallest (dissipate) eddies Rotta developed an exact transport equation for the large turbulent
length scales. This is a much better basis for a term-by-term modelling
approach
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Classical Derivation 2 Equation Models
( ) ( )
+=
+
jk
t
j
k
j
j
x
k
xkcP
x
kU
t
k
( ) ( ) ( )
+
=
+
j
t
j
k
j
j
xxk
kP
kxU
t
k
t=
The k-equation: Can be derived exactly from the
Navier-Stokes equations
Term-by-term modelling
The - (-) equation: Exact equation for smallest
(dissipation) scales Model for large scales not based
on exact equation
Modelled in analogy to k-
equation and dimensionalanalysis
Danger that not all effects areincluded
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Source Terms Equilibrium k- Model
Only one Scale in Sources (S~1/T)
Turbulence ModelInput S
Output
Output k
O ?
( )
( )
2 2
2 2
1 2
( )( )
( )( )
j tt
j j k j
j t
j j j
U kk kS c
t x x x
Uc S c
t x x x
+ = +
+ = +
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Determination of L in k-Model
k-equation:
+=
+
y
kk
ycS
k
x
kU
t
k
k
k
)(
)()( 22
+=
kkccS
k 1)(0 22
2
2~0
kcSc +=
D
F
C
N ,
22~ Sk
S~ from -equation
2 2
~ ~ ~tk S
LS
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Rottas Length Scale Equation
To avoid the problem that the () equation is an equation
for the smallest scales, an equation for the large (integral)
scales is needed.
This requires first a mathematical definition of an integral
length scale, L.
In Rottas (1968) approach this definition is based on two-pointcorrelations
Based on that definition of L, an exact transport equation can
be derived from the Navier-Stokes equations (the actual
equation is based on kL) This exact equation is then modelled term-by-term
R, J.C.: M B ,
A G, R. 69 A14, (1968).
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Two-Point Velocity Correlations
Measurement of velocity fluctuations with two probesat two different locations
For small r, all eddies contribute
For large r, only large scales contribute
For r > L, correlation goes to zero
Integral vs. rproportional to size of large eddies L
rr
Fixed Probe
Shifted Probe
ijR~
1
r
L
Eddies
),('),('
),('),('~
txutxu
trxutxuR
ji
ji
ij rr
rrr+
=
rr
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Rottas k-kL Model
Integral Length Scale:( , ) ( , , )
iiL x t c R x t r dr
= %
, , .
N.
E ( , ..) .
ry
1
L
Rii
rr
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Exact Transport Equation Integral
Length-Scale (Rotta)Exact transport equations for =kL (boundary layer form):
( )( )
( ) ( ) ( )
++
+
+
+
=
+
yvpvpR
y
drrr
RdrRR
r
drRy
rxUdrRy
xU
x
U
t
ii
y
kk
iiyikiiik
k
y
y
y
k
k
''1
16
3
8
3
16
3
)(
16
3)(
16
3)()(
2
2
)(
1221
I :
)(xkL=with
y
yidrR
y
rxU12
)(
16
3
+
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Expansion of Gradient Function
Important term:
R:
22 3
y yy2 3
U ( x r ) r U ( x ) U ( x ) U ( x )r ...y y y y 2
+ = + + +
+
+
+
yyyyyy
ydrRr
y
xUdrRr
y
xUdrR
y
xUdrR
y
rxU
12
2
3
3
122
2
1212
)(
2
1)()()(
0)(
122
2
=
yy drRr
y
xU
D R
ry
1Rij
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I 3=0 N N
Transport Equation Integral
Length-Scale (Rotta)Transport equations for kL:
( )
+
+
=
+
yyqcc
yxUL
yxULuv
xU
t
tL
ii
k
k
2/32
3
33
32
)()()()(
E :
33
3
2
/
/
yU
yUccL l
=
P 3 :
N
N 03=
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Virtual Experiment 1D Flow
?
Logarithmic layer Lt=y
2
122 0y y
Ur R dr
y
=
)(~
)(~
1212 y
II
y
IrRrR
rr