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Combustion Science Data Management Needs

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Title: Combustion Science Data Management Needs


1
Combustion Science Data Management Needs
  • Jacqueline H. Chen
  • Combustion Research Facility
  • Sandia National Laboratories
  • jhchen_at_sandia.gov
  • DOE Data Management Workshop
  • SLAC
  • Stanford, CA
  • March 16-18, 2004
  • Sponsored by the Division of Chemical Sciences
    Geosciences, and Biosciences, the Office of Basic
    Energy Sciences, the U. S. Department of Energy

2
Challenges in combustion understanding and
modeling
  • Stiffness wide range of length and time scales
  • turbulence
  • flames and ignition fronts
  • high pressure
  • Chemical complexity
  • large number of species and reactions
  • Multi-physics complexity
  • multiphase (liquid spray, gas phase, soot)
  • thermal radiation
  • acoustics ...

Diesel Engine Autoignition, Laser
Incandescence Chuck Mueller, Sandia National
Laboratories
3
Direct Numerical Simulation (DNS) Approach
  • High-fidelity computer-based observations of
    micro-physics of chemistry-turbulence
    interactions
  • Resolve all relevant scales
  • At low error tolerances, high-order methods are
    more efficient
  • Laboratory scale configurations homogeneous
    turbulence, v-flame turbulent jets, counterflow
  • Complex chemistry - gas phase/heterogeneous
    (catalytic)

Turbulent methane-air diffusion flame
4
High-fidelity Simulations of Turbulent
Combustion (TSTC) http//scidac.psc.edu
CFRFS
Software design developments
Numerical developments
. S3D0 F90 MPP 3D . S3D1 GrACE-based . S3D2
CCA-compliant
. IMEX ARK . IBM . AMR
Model developments
CCA
. Thermal radiation . Soot particles . Liquid
droplets
MPP S3D
CMCS DM
Arnaud Trouvé, U. Maryland Jacqueline Chen,
Sandia Chris Rutland, U. Wisconsin Hong Im, U.
Michigan R. Reddy and R. Gomez, PSC
Post-processors flamelet, statistical
5
3D DNS Code (S3D) scales to over a thousand
processors
  • Scalability benchmark test for S3D on MPP
    platforms - 3D laminar
  • hydrogen/air flame/vortex problem (8 reactive
    scalars)
  • Ported to IBM-SP3, SP4, Compaq SC, SGI Origin,
    Cray T3E,
  • Intel Xeon Linux clusters

6
A Computational Facility for Reacting Flow
Science (CFRFS)
  • Develop a flexible, maintainable, toolkit for
    high-fidelity Adaptive Mesh Refinement (AMR)
    Massively-Parallel low Mach number reacting flow
    computations
  • Develop an associated CSP data analysis and
    reduction toolkit for multidimensional reacting
    flow
  • Use CSP and a PRISM tabulation approach to enable
    adaptive chemistry reacting flow computations
  • PRISM Piecewise Reusable Implementation of
    Solution Mapping (M. Frenklach)

CCA GUI showing connections
7
Motivation Control of HCCI combustion
  • Overall fuel-lean, low NOx and soot, high
    efficiencies
  • Volumetric autoignition, kinetically driven
  • Mixture/thermal inhomogeneities used to control
    ignition timing and burn rate
  • Spread heat release over time to minimize
    pressure oscillations

8
Objectives
Chen et al., submitted 2004, Sankaran et al.,
submitted 2004
  • Gain fundamental insight into turbulent
    autoignition with compression heating
  • Develop systematic method for determining
    ignition front speed and establish criteria to
    distinguish between combustion modes
  • Quantify front propagation speed and parametric
    dependence on turbulence and initial scalar
    fields
  • Develop control strategy using temperature
    inhomogeneities to control timing and rate of
    heat release in HCCI combustion
  • deflagration
  • spontaneous ignition
  • detonation

9
Initial conditions
  • Same mean T (1070K)
  • Different T skewness
  • and variance (15,30K)
  • Pressure 41 55 atm
  • Lean hydrogen/air

10
Temperature skewness effect on heat release rate
Heat release, HighT, positive skewness
11
Temperature skewness effect on ignition delay and
burn time
  • Temperature distribution influences ignition and
    duration of burning.
  • Hot core gas
  • Ignited earlier
  • Burns longer
  • Cold core gas
  • Ignited later
  • Slow end gas combustion

12
Ignition front tracking method
  • Density-weighted displacement speed (Echekki and
    Chen, 1999)
  • YH2 8.5x10-4 isocontour location of maximum
    heat release
  • Laminar reference speed, sL based on freely
    propagating premixed flame at local enthalpy and
    pressure conditions at front surface

13
Species balance and normalized front speed
criteria for propagation mode
A
C
Heat release isocontours
B
Black lines sd/sL lt 1.1 (deflagration) White
lines sd/sL gt 1.1 (spontaneous ignition) A
deflagration B, C spontaneous ignition
14
Fraction of front length and burnt gas area
production due to deflagration
  • Solid line front length
  • Dashed line burnt area production

15
Comparison of experimental and DNS data for
ignition/edge flame data
  • Flow divergence effect (Ruetsch et al. 1994)
    upstream divergence of flow due to increase in
    normal component of flow resulting from heat
    release
  • Curvature preferential diffusion focusing
    effect at leading edge

Normalized OH Expt
Normalized OH DNS
Heated air
H2/N2
H2 O OH H O2 H O OH slow OH
recombination
H2
LP
OH
xst
H
DF
RP
16
Apriori testing of reaction models using DNS of
turbulent jet flames
Sutherland et al., submitted 2004
CO/H2/air jet flame, scalar dissipation rate
17
Joint experiment/computation of turbulent
premixed methane/air V-flame
  • Stationary statistics required for turbulent
    premixed flame model development LES/RANS
  • Flame topology curvature stretch statistics
  • Complex chemistry versus simple or tabulated
    chemistry (heat release, radicals, minor species)
  • Is preheat zone thickening due to small scales or
    higher curvatures in thin reaction zone regime?

V-flame, expt. Renou 2003 and DNS, Vervisch 2003
18
Lean premixed combustion at Sandiaswirl burner,
LES, and DNS
DNS E. Hawkes and J.H. Chen
Experiment OH PLIF, PIV R.W Schefer
LES J. Oefelein
19
Data management challenges for combustion science
  • 2D complex chemistry simulations today 200
    restart files (x,y,Z1,Z50) skeletal n-heptane 41
    species, 2000x2000 grid, 1.6 Gbytes/time x200
    files 0.32 Tbyte, 5 runs in parametric study
    1.6 Tbytes raw data
  • Processed data 2 Tbyte data
  • 3D complex chemistry simulations in 5 years 200
    restart files (x,y,Z1,Z50) skeletal n-heptane 41
    species, 2000x2000x2000 grid, 3.2 Tbytes/time x
    200 files 640 Tbytes per run, 5 runs 3.2
    Petabytes raw data
  • Processed data 3 Petabytes
  • Combustion regions of interest are spatially
    sparse
  • Feature-borne analysis and redundant subsetting
    of data for storage
  • Provenance of subsetted data
  • Temporal analysis must be done on-the-fly
  • Remote access to transport subsets of data for
    local analysis and viz.

20
Features
  • Feature is an overloaded word
  • A feature in this context is a subset of the data
    grid that is interesting for some reason.
  • Might call it a Region of Interest (ROI)
  • Also might call it a structure

21
Why Feature Tracking?
  • Reduce size of data
  • How do you find small ROIs in a large 3D domain?
  • Retrieve and analyze only what you need
  • Provide quantification
  • Can exactly define ROI chosen do specific
    statistics
  • Enhance visualization
  • Can visualize features individually
  • Can color code features
  • Facilitate event searching
  • Events are feature interactions

22
Feature Detection
  • Detection Identify features in each time step
  • FDTOOLS tests each cell groups connected ones
  • There are many possible algorithms including
    pattern recognition

23
Feature Tracking
  • Tracking Identify relationships between
    features in different time steps
  • Again, there are many different algorithms, and
    knowing about how your features interact helps

24
Events
  • Merge
  • (Birth)
  • (Death)
  • Split
  • Other domain specific events like hard-body
    collision, vorticity tube reconnect, etc.

25
Design Goal Flexible Reusable
  • Callable from running programs
  • Independent of visualization package
  • Modular
  • Detector plug-ins
  • Tracker plug-ins
  • Other plug-ins
  • CCA compatible
  • Output interface for further analysis

26
DataSet Types
fdRegular 2 3D of
all fdRefined structured (AMR)
27
FDTOOLS Design (Wendy Koegler SNL)
Output Interface
Data Interface
FDTOOLS Component
Director
Feature Manager
Representer
Detector
Analyzer
Tracker
Visualizer
28
Detection and tracking of autoignition features
FDTools (Koegler, 2002) evolution of ignition
features
Hydroperoxy mass fraction
29
Feature graph tracks evolution of ignition
features
time
30
Feature-borne analysis
31
Ignition feature classification
32
Terascale virtual combustion analysis facility

33
Data management framework for combustion science
I
  • Distributed data mining tools feature ID and
    tracking
  • Distributed analysis tools operating on regions
    of interest
  • Reaction source term and Jacobian evaluation
  • Conditional statistics
  • Isolevel surface of multiply-connected 3D
    surfaces
  • Interpolate, integrate, differentiate in
    principle directions to surface
  • Computational singular perturbation analysis
  • Reaction flux analysis
  • Principal component analysis
  • Spectral analysis

34
Data management framework for combustion science
II
  • Data objects, which interface to metadata and
    data
  • Enabling writing and reading data with various
    flexible formats
  • Standard data formats
  • Automatic conversion utilities
  • Flexible, user-configurable, user-friendly GUIs
    to enable
  • user to specify desired operations on data
  • General structured and unstructured adaptive mesh
    data
  • Real-time feature-borne detection, tracking and
    analysis for computational steering (e.g.
    adaptive IO, temporal statistics)

35
Data management framework for combustion science
III
  • Distributed visualization tools
  • scalar and non-scalar data
  • Non-scalar data, i.e. vector or tensor
  • Heterogeneous data combined experimental and
    computational data
  • Iso-surface rendering and interpolating data onto
    user-specified slices
  • Streamlines, information overlays
  • Uncertainty
  • Viz reduced-order representations of flow and
    combustion features
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