application of zonal hybrid urans/les modeling to...
TRANSCRIPT
APPLICATION OF ZONAL HYBRID URANS/LES MODELING TO INTERNAL COMBUSTION ENGINE FLOWS
V. K. Krastev1, A. D’Adamo2, S. Breda3, S. Fontanesi2
1 Department of Economics, Engineering, Society and Business Organization, University of Tuscia,
01100 Viterbo, Italy
2 DIEF - "Enzo Ferrari" Engineering Department, University of Modena and Reggio Emilia, 41125
Modena, Italy
3 R&D CFD SRL - Via Pietro Vivarelli 2, 41125 Modena, Italy
LES4ICE 2018
Outline
V. K. Krastev et al. 2
• Background o URANS/LES hybrids in ICE modeling
o Motivations
• Zonal modeling formulation & calibration
• Applications o Static valve intake flow
o TCC-III Engine multi-cycle analysis
• Conclusions
LES4ICE 2018
Outline
V. K. Krastev et al. 3
• Background o URANS/LES hybrids in ICE modeling
o Motivations
• Zonal modeling formulation & calibration
• Applications o Static valve intake flow
o TCC-III Engine multi-cycle analysis
• Conclusions
LES4ICE 2018
Outline
V. K. Krastev et al. 4
• Background o URANS/LES hybrids in ICE modeling
o Motivations
• Zonal modeling formulation & calibration
• Applications o Static valve intake flow
o TCC-III Engine multi-cycle analysis
• Conclusions
LES4ICE 2018
Outline
V. K. Krastev et al. 5
• Background o URANS/LES hybrids in ICE modeling
o Motivations
• Zonal modeling formulation & calibration
• Applications o Static valve intake flow
o TCC-III Engine multi-cycle analysis
• Conclusions
LES4ICE 2018
Background
V. K. Krastev et al. 6
URANS/LES hybrids in the ICE modeling community
Cumulative graph of the published journal papers with relevant hybrid
URANS/LES applications in the ICE field (source+: www.scopus.com)
+The collected data might not be fully exhaustive
o LES methods for ICE modeling are being developed
for 25 years, but …
o …in recent years the interest for URANS/LES hybrids
is apparently growing
o Potential gains in computational robustness and
efficiency, keeping scale-resolving capabilites
where needed
o Several seamless (SAS, DES, DLRM) and zonal
(ZDES) alternatives proposed
LES4ICE 2018
Background
V. K. Krastev et al. 7
URANS/LES hybrids in the ICE modeling community
Cumulative graph of the published journal papers with relevant hybrid
URANS/LES applications in the ICE field (source+: www.scopus.com)
+The collected data might not be fully exhaustive
o LES methods for ICE modeling are being developed
for 25 years, but …
o …in recent years the interest for URANS/LES hybrids
is apparently growing
o Potential gains in computational robustness and
efficiency, keeping scale-resolving capabilites
where needed
o Several seamless (SAS, DES, DLRM) and zonal
(ZDES) alternatives proposed
LES4ICE 2018
Background
V. K. Krastev et al. 8
URANS/LES hybrids in the ICE modeling community
Cumulative graph of the published journal papers with relevant hybrid
URANS/LES applications in the ICE field (source+: www.scopus.com)
+The collected data might not be fully exhaustive
o LES methods for ICE modeling are being developed
for 25 years, but …
o …in recent years the interest for URANS/LES hybrids
is apparently growing
o Potential gains in computational robustness and
efficiency, keeping scale-resolving capabilites
where needed
o Several seamless (SAS, DES, DLRM) and zonal
(ZDES) alternatives proposed
LES4ICE 2018
Background
V. K. Krastev et al. 9
Meanwhile, in the aerospace/turbomachinery engineering fields…
Complete aircraft at scale 1:1 in true flight conditions (Ma=0.8, Re ~ 5∙107, ~ 2∙108 grid points)+
+Picture taken from: S.Deck et al, Phil. Trans. R. Soc. A 372: 20130325 (2014).
o DES and Zonal-DES modeling have proven to be highly efficient in complex aerospace
applications
o The flexibility of hybrid modeling allows the accurate resolution of different types of internal
and external, flows within the same computational domain
o Care is needed for the optimal domain decomposition and numerics choice
LES4ICE 2018
Background
V. K. Krastev et al. 10
o Single, URANS-based turbulence modeling framework
o Activation of LES only where actually needed
o Less troublesome BCs
o Reported to be competitive with LES on sub-optimal grids,
especially for wall-impinging flows+
+See e. g. K. Keskinen et al. International Journal of Heat and Fluid Flow 65 (2017)
141–158
Why (Z)DES for ICE?
LES4ICE 2018
Background
V. K. Krastev et al. 11
o Assess if a (relatively) basic ZDES model is capable of
handling complex multi-cycle engine simulations with a
reasonable level of accuracy
Comparable with experimental data sets
Comparable with modern LES approaches on engineering-
grade meshes
More specifically:
LES4ICE 2018
Modeling
V. K. Krastev et al. 12
From two-equation URANS to (Z)DES
Basis:
o General URANS two-equation form:
o Strelets et al. (2001) showed that URANS can be
turned into DES by modifying Sk only
TKE sink term modification (1)
,
k k k k
t
kt
t
f k
C P S D
C P S D
LES4ICE 2018
Modeling
V. K. Krastev et al. 13
From two-equation URANS to (Z)DES
Basis:
o General URANS two-equation form:
o Strelets et al. (2001) showed that URANS can be
turned into DES by modifying Sk only
TKE sink term modification (1)
3/2
,; ,
RANSk RANSRANS
kl f k
l S
3/2
,; ,
DES RANS DESk DESDES
kl min l C
l S
(gridf )
,
k k k k
t
kt
t
f k
C P S D
C P S D
DESC O(1)
LES4ICE 2018
Modeling
V. K. Krastev et al. 14
From two-equation URANS to (Z)DES
Basis:
o General URANS two-equation form:
o Strelets et al. (2001) showed that URANS can be
turned into DES by modifying Sk only
TKE sink term modification (1)
3/2
,; ,
RANSk RANSRANS
kl f k
l S
3/2
,; ,
DES RANS DESk DESDES
kl min l C
l S
,
k k k k
t
kt
t
f k
C P S D
C P S D
, ,DESk DES k RANSFS S
max / ,1DES RANS DESlF C
Final
form
LES4ICE 2018
Modeling
V. K. Krastev et al. 15
From two-equation URANS to (Z)DES
TKE sink term modification (2) Seamless DES:
o URANS-to-LES managed entirely by the model (user
decisional load kept to a minimum), but…
o …the triggering mechanism is not always efficient
Zonal DES:
o URANS and LES (or DES) regions explicitly marked by
the user
o Better control of the solution behavior (at the expense
of nontrivial a-priori decisions)
o Good candidate for complete ICE simulation
* *, ,DESk DES k RANSFS S
*1 11DES z DES z ZDESC F C FF
2 21 RANSZDES z z
DES
lC C
CF
LES4ICE 2018
Modeling
V. K. Krastev et al. 16
From two-equation URANS to (Z)DES
TKE sink term modification (2) Seamless DES:
o URANS-to-LES managed entirely by the model (user
decisional load kept to a minimum), but…
o …the triggering mechanism is not always efficient
Zonal DES:
o URANS and LES (or DES) regions explicitly marked by
the user
o Better control of the solution behavior (at the expense
of nontrivial a-priori decisions)
o Good candidate for complete ICE simulation
* *, ,DESk DES k RANSFS S
*1 11DES z DES z ZDESC F C FF
2 21 RANSZDES z z
DES
lC C
CF
Cz1 Cz2 Simulation
type Mode
0 1 URANS I
1 1/0 DES II
0 0 LES III
LES4ICE 2018
Modeling
V. K. Krastev et al. 17
Implementation overview
Which turbulence model?
o RNG k-e model
• Improved, shear-dependent e-equation
• Widely adopted in the ICE community
Methodology implementation/calibration:
o The CDES value must ensure a consistent turbulent
energy decay in mode III (pure LES)
o The optimal value depends on:
• the specific underlying turbulence model (k-e,
k-w…)
• the accuracy/behavior of the discretization
schemes
o Calibration tests needed
Which CFD code?
o STAR-CD v4.22c (Siemens PLM)
• Unstructured FVM code
• Second-order accurate in space and time
• ZDES formulation implemented through user-
supplied Fortran subroutines
LES4ICE 2018
Modeling
V. K. Krastev et al. 18
CDES calibration: turbulence box
o Standard test for DNS and SGS models
o Cubic domain with cyclic BCs in each direction, N3
perfectly cubic cells (N=64)
o Flow field initialized with an incompressible
divergence-free turbulent spectrum
o Turbulence is left to spontaneously decay driven
by mode III of ZDES
o CDES is varied in the 0.4-0.61+ range
o MARS scheme for momentum convection (BF = 0.5
and BF = 1)
o Comparisons with the Comte-Bellot and Corrsin§
database (energy spectra)
+CDES = 0.61 is the first “standard” value reported in the literature for k-e based DES models
§G. Comte-Bellot G and S. Corrsin Journal of Fluid Mechanics 1971; 48(2): 273–337.
LES4ICE 2018
Modeling
V. K. Krastev et al. 19
CDES calibration: turbulence box
o The BF effect is dominant
o BF = 1 assumed as default for the LES mode (mode III)
o CDES = 0.61 assumed as standard
t = t1 t = t2
LES4ICE 2018
Applications – Static valve
V. K. Krastev et al. 20
Case overview
Preliminary remarks: o Intake port geometry with an axis-centered fixed poppet valve, Reb ≈ 3 x 104
o LDA (velocity) and axial pressure measurements available
Valve Stem Diameter (Ds) 16 mm
Intake Duct Diameter (Di) 34 mm
Cylinder Diameter (Dc) 120 mm
Valve Head Diameter (Dv) 40 mm
Intake Duct Length (Li) 140 mm
Cylinder Length (Lc) 300 mm
Valve Lift (LL) 10 mm
Inlet Bulk Velocity (Ub) 60 m/s
Fluid air at NIST standard conditions
Inlet Bulk Reynolds Number (Reb) ~ 3 x 104
LES4ICE 2018
Applications – Static valve
V. K. Krastev et al. 21
Case overview
Preliminary remarks: o Intake port geometry with an axis-centered fixed poppet valve, Reb ≈ 3 x 104
o LDA (velocity) and axial pressure measurements available
o Mode I numerics: MARS 0.5 for momentum and scalars
o Mode II/III numerics: MARS 1 for momentum, MARS 0.5 for scalars
o Standard inflow/outflow incompressible BCs, WFs at the walls
o Comparisons with experiments and OpenFOAM results (same turbulence model and grid, similar numerics)
Mode II = Z1
Mode III = Z2
LES4ICE 2018
Applications – Static valve
V. K. Krastev et al. 22
Results (x = 20 mm)
Mean axial velocity RMS axial velocity fluctuation
o Significant improvements compared to steady RANS profiles (code-by-code differences due to numerics)
o Z1 and Z2 time-averaged profiles very close (Mode II is likely to trigger LES in most of the domain)
LES4ICE 2018
Applications – Static valve
V. K. Krastev et al. 23
Results (axial pressure development)
LES4ICE 2018
Applications – Static valve
V. K. Krastev et al. 24
Results (axial pressure development)
o Even more pronounced improvements compared to RANS (same code-by-code differences)
o Z1 and Z2 time–averaged profiles very close (Mode II is likely to trigger LES in most of the domain)
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 25
Case overview
Preliminary remarks (1): o Selected for the ease of reproduction and large experimental PIV data set
o 1300 RPM and 40 kPa intake manifold pressure
o Availability of LES data sets from UniMoRe
Engine Data
Bore 92 mm
Stroke 86 mm
Connecting rod length 231 mm
Geometrical compression ratio 10:1
Operation 4-stroke
N. of valves 2
Combustion chamber type Pancake
RPM 1300
Intake manifold pressure 40 kPa
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 26
Case overview
Preliminary remarks (2): o Full domain splitted in 5 zones (cylinder, intake/exhaust ports, plenums)
o Only the cylinder zone treated in scale-resolving mode (Mode II or Mode III)
o Max 2M cells at BDC, ~ 0.75 mm base cell dimension in the cylinder
Mode II = TCC-Z1
Mode III = TCC-Z2
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 27
Case overview
,1
1 n
i i jj
u un
2
, ,1
1
1
n
i rms i j ij
u u un
PIV grid point
cycle number
50
i
j
n
Preliminary remarks (3): o Postprocessing initially focused on the vertical planes
o S_2013_10_24_01 and S_2014_02_05_02 reference data sets (same windows/resolution in the simulations)
o Previous LES DSM results (on the same CFD grid) added for comparison
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 28
Results (Y = 0): 475 CA E
ns
. A
vg
. R
MS
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 29
Results (Y = 0): 475 CA
o Good average jet shape prediction by TCC-Z1 (added modeled visosisty?)
o Underestimation of RMS fluctuations close to the piston head
En
s. A
vg
. R
MS
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 30
Results (Y = 0): 540 CA E
ns
. A
vg
. R
MS
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 31
Results (Y = 0): 540 CA E
ns
. A
vg
. R
MS
o DSM closer to experiments
o TCC-Z1 slighlty more consistent with DSM and experiments
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 32
Results (Y = 0): 630 CA E
ns
. A
vg
. R
MS
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 33
Results (Y = 0): 630 CA E
ns
. A
vg
. R
MS
o DSM still in good agreement with the experiments
o Anomalous shift of the RMS peak values
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 34
Results (X = 0): 475 CA E
ns
. A
vg
. R
MS
o Good overall consistency for all numerical predictions
o Small differences persist between TCC-Z1 and TCC-Z2
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 35
Results (X = 0): 540 CA E
ns
. A
vg
. R
MS
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 36
Results (X = 0): 540 CA E
ns
. A
vg
. R
MS
o Much better main vortex average shape description for TCC-Z1 and TCC-Z2
o DSM seems to overestimate RMS fluctuations
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 37
Results (X = 0): 630 CA E
ns
. A
vg
. R
MS
LES4ICE 2018
Applications – TCC III
V. K. Krastev et al. 38
Results (X = 0): 630 CA E
ns
. A
vg
. R
MS
o Vortex compression better described by DSM
o TCC-Z1 (still) slightly more consistent than TCC-Z2 (average flow)
LES4ICE 2018
Conclusions
V. K. Krastev et al. 39
Final remarks
o Is the evaluated ZDES formulation reasonably adequate for
engine multi-cycle simulation?
LES4ICE 2018
Conclusions
V. K. Krastev et al. 40
Final remarks
o Is the evaluated ZDES formulation reasonably adequate for
engine multi-cycle simulation?
Yes, but…
LES4ICE 2018
Conclusions
V. K. Krastev et al. 41
What’s next?
o More TCC-III results (in progress):
• complete the analyses on the vertical planes (LES
quality indicators, LES or DES for the cylinder?);
• more planes;
• different zonal setups.
o Modeling aspects (LES mode, wall modeling)
o Different engines (pentroof, 4 valves, GDI?)
o Combustion?
LES4ICE 2018
Conclusions
V. K. Krastev et al. 42
Acknowledgments
GM (through the GM University of Michigan
Automotive Cooperative Research Laboratory,
Engine Systems Division).
Siemens PLM Software Inc.
TCC-III database
STAR-CD software licensing (through
UniMoRe HPC resources)
LES4ICE 2018
Conclusions
V. K. Krastev et al. 43