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Convergent Science Inc. CFD Software and Consulting Services
Experts in Engine CFD Analysis
The CONV ERGET M CFD code
automatically generates a high quality
orthogonal mesh at run-time thus
eliminating all user meshing time
CONVERGETM automatically adds mesh
resolution w hen and w here it is needed
based upon field variables to maximize
accuracy w hile minimizing the run-time
CONVERGETM is loaded w ith the
physical models for spray, turbulence
and combustion needed to accurately
simulate all engine types including
Diesel, gasoline, hydrogen, natural gas,
dual fuel and HCCI
CONVERGETM runs great in parallel
Use CONVERGETM CFD Software for In-Cylinder Spray and Combustion Analysis and Never Make a Mesh Again
[email protected] www.convergecfd.com (830) 481-6434
Optimization with CONVERGETM : Let the computer find the best design
Velocity (left) and temperature contours (right) for SI engine analysis
using detailed chemistry and adaptive mesh refinement (AMR)
CONV ERGETM comes equipped w ith a pow erful optimization
algorithm called CONGO. With CONGO, a merit function (often
a combination of emissions and fuel consumption) is used to
rate the f itness of each design. A population of designs is
automatically run in parallel across many computers, stopping
w hen the time allotted has been reached.
Common optimization parameters include
• Settings (such as spray details, EGR level and spark timing)
• Tables (such as valve lift profiles and spray rate shape)
• Parameterized Geometry (such as piston shape)
Use CONGO and let CONV ERGETM automatically f ind the
optimum design.
Conjugate Heat Transfer (CHT)
modeling with CONVERGETM v2.1
In CONV ERGETM v2.1, the user can readily solve for
the f low and heat transfer in all f luid and solid
components (“conjugate heat transfer”).
As is alw ays the case w ith CONV ERGETM, a body
f itted mesh for all the f luid and solid entit ies is
generated automatically at run-time, thus eliminating
all user meshing time and streamlining the analysis.
Appropriate super-cycling techniques for handling
the disparate time-scales associated w ith heat
transfer and fluid f low are available to minimize the
run-times associated w ith conjugate heat transfer.
Optimum piston bowl shape (top) and merit
map for CONGO genetic algorithm analysis
0
2
4
6
8
10
0 5 10 15 20 25 30 35 40
so
ot
(g/k
g-f
ue
l)
NOx+HC (g/kg-fuel)
Optimum
Conjugate heat transfer (both fluid and solid) simulated
in CONVERGE without any coupling with other tools
Increase Productivity
No user meshing time
Parallel speedup
Handle all geometry types
Handle moving parts
automatically
Increase Accuracy
Orthogonal mesh
Adaptive mesh refinement
Grid scaling & embedding
Perform grid resolution
studies without making any
meshes
Key Physical Models
• SAGE detailed chemistry
solver
• Advanced turbulence
(including LES)
• Spray break-up
• Droplet coll ision and
coalescence
• Multi-component vaporization
• Combustion suite
• Wall fi lm
• Genetic algorithm for
optimization studies
• User routines for custom
model implementation
Multi-component Vaporization
When using detailed chemistry
w ith CONV ERGETM, the user
can specify any desired
chemical mechanism – there is
not a limit on the number of
species or reactions. To
minimize run t ime, it is
obviously desirable to use the
smallest mechanism possible
which w ill provide accurate
results.
To this end, CSI has
implemented a parallel version
of the latest state of the art
mechanism reduction tool,
“Parallel Directed Relation
Graph w ith Error Propagation
and Sens itivity“ (PDRGEPSA).
Unimportant species and
reactions are removed from the
mechanism w ith the goal of
minimiz ing the mechanism size
w hile maximizing the accuracy.
The multi-component vaporization capabilities
of CONVERGET M can handle all modern fuel
injection strategies including dual fuel, ethanol,
cold start and w ater injection.
Each liquid can be comprised of any number of
components. The vaporization algorithm
sources each of the species individually based
upon the component distillation properties.
Regardless of the fuel injection strategy, SAGE-
Multizone can be used to determine the
reaction rates for any mixture of gases.
SAGE-Multizone with n-Dimensional bins for speeding up multi-fuel CFD simulations For some cases such as multi-fuel applications, two
dimensional zoning (i.e. temperature and phi) is insuff icient
to accurately model the combustion. For these cases,
CONVERGE allow s an arbitrary number of bins to be used.
Schematic of PDRGEPSA Mechanism Reduction Algorithm
SAGE-Multizone dramatically reduces the run time associated with detailed chemistry
Including detailed chemistry is essential for accurately
modeling kinetically limited phenomena such as f lame
propagation, auto-ignition and emissions. For this reason,
CONVERGETM comes standard w ith the SAGE detailed
chemistry solver for combustion modeling.
Convergent Science Inc. has licensed the Multi-Zone
Chemistry Solver from Lawrence Livermore National
Laboratory and implemented this into CONVERGETM to
enhance the capabilities of SAGE.
SAGE-Multizone drastically reduces the run-time associated
with detailed chemistry simulations. Typical chemistry
speedups over standard SAGE are 15X for Diesel engines and
50X for spark ignited engines. SAGE-Multizone is available in
the current release of CONVERGETM.
Auto-ignition locations (red) and liquid spray droplets for dual fuel
(Iso-octane+Diesel) test case.
Crank Ang le [degrees]
He
at
Re
lea
se
Ra
te(J
/de
gre
e]
0 5 0 1 0 00
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
M Z-M ap-I (T, , YC7H 16
)
SAG E
M Z-M ap-I (T , )
Crank Ang le [degrees]
Sp
ec
ies
Ma
ss
(kg
)
0 5 0 1 0 0
1 0-8
1 0-7
1 0-6
1 0-5
1 0-4
1 0-3
O H
C O2
C O
M Z-M ap-I (T, , YC7H 16
)
SA G E
M Z-M ap-I (T, )
Crank Ang le [degrees]
Sp
ec
ies
Ma
ss
(kg
)
0 5 0 1 0 01 0
-1 2
1 0-1 0
1 0-8
1 0-6
1 0-4
1 0-2
N O
C8H
1 8
H2O
M Z-M ap-I (T, , YC7H 16
)
SAG E
M Z-M ap-I (T , )
Crank Ang le [degrees]
He
at
Re
lea
se
Ra
te(J
/de
gre
e]
0 5 0 1 0 00
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
1 0 0
M Z-M ap-I (T, , YC7H 16
)
SAG E
M Z-M ap-I (T , )
Crank Ang le [degrees]
Sp
ec
ies
Ma
ss
(kg
)
0 5 0 1 0 0
1 0-8
1 0-7
1 0-6
1 0-5
1 0-4
1 0-3
O H
C O2
C O
M Z-M ap-I (T, , YC7H 16
)
SA G E
M Z-M ap-I (T, )
Crank Ang le [degrees]
Sp
ec
ies
Ma
ss
(kg
)
0 5 0 1 0 01 0
-1 2
1 0-1 0
1 0-8
1 0-6
1 0-4
1 0-2
N O
C8H
1 8
H2O
M Z-M ap-I (T, , YC7H 16
)
SAG E
M Z-M ap-I (T , )
Typical run time for a premixed engine simulation
showing the dramatic reduction in run time
associated with SAGE-Multizone
CONVERGETM Chemical
Mechanism Reduction
Iso-surface of temperature showing the flame front
(red) and locations of auto-ignition (blue) for spark ignited engine.