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Zhuyin Laniu Ren

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Advantage of dimension reduction combined with ISAT in CFD simulation ... Flamelet generated manifolds (FGM) 2 Roussel & Fraser algorithm (RF) 2 Pre-Image Curves ... – PowerPoint PPT presentation

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Title: Zhuyin Laniu Ren


1

Dimension Reduction of Combustion Chemistry
  • Zhuyin (Laniu) Ren
  • S. B. Pope
  • Mar. 29th, 2005

2
Outline
  • Motivation
  • Advantage of dimension reduction combined with
    ISAT in CFD simulation
  • Dimension reduction of combustion chemistry
  • Pre-image curve method

3
Motivation
  • Knowledge of detailed mechanism
  • Continually increasing in accuracy and scope
  • 50 1000 species in detailed description
  • Use in computations of combustion
  • DNS, LES, PDF and other approaches
  • Need general methodology to
  • Reduce the computational cost
  • Retain accuracy and adequate detail

Reduce the computational cost by using
dimension reduction combined with ISAT
4
CFD/Full Chemistry/Direct Integration
Schematic of DI with full representation used in
the reaction fractional step of a CFD computation.
Computationally prohibitive with large detailed
mechanism (Both CPU/Memory)
5
CFD/ Full Chemistry/ISAT
Schematic of ISAT with full representation used
in the reaction fractional step of a CFD
computation.
  • Computationally much less expensive (100-1000
    fast than previous approach)
  • Memory issue!

6
CFD/Dimension Reduction (via Species
Reconstruction)/ISAT
Schematic of ISAT with dimension reduction (via
species reduction and reconstruction) used in
the reaction fractional step of a CFD computation.
  • Use only the major species both in CFD and ISAT
    (Both speed up the CFD part and ISAT retrieval
    solve memory issue )
  • ISAT allows more expensive procedure to do the
    dimension reduction
  • Error in dimension reduction (in species
    reconstruction part) is crucial to this
    methodology.
  • Develop more accurate method to do the dimension
    reduction!!

7
Dimension Reduction of combustion chemistry
Represent combustion chemistry in terms of
reduced composition r (nr) (e.g. major species )
instead of the full composition f(nf) (e.g. full
species)
1 Unimportant species and reactions in the
detailed mechanism 2 Large range of chemical
time scales
8
Dimension Reduction of combustion chemistry
--1d-5 sec --1d-6 sec --1d-7 sec
PRF Primary Reference Fuel mixture of Heptanes
and Octane ---1034 species 4236
reactions Great potential for dimension reduction
9
Existing Dimension Reduction methods
  • Skeletal mechanism
    ?1
  • Quasi-steady state assumptions (QSSA)
    ?2
  • Intrinsic low-dimensional manifolds (ILDM)
    ?2
  • Rate-controlled constrained equilibrium (RCCE)
    ?2
  • Trajectory-generated low-dimensional manifold
    ?2
  • Flamelet generated manifolds (FGM)
    ?2
  • Roussel Fraser algorithm (RF)
    ?2
  • Pre-Image Curves
    ?2

General procedure of dimension reduction of
combustion chemistry Step 1 Detailed mechanism
gt Skeletal mechanism (Small detailed mechanism)
Step 2 Further reduction based on time scale
analysis
10
Evaluation of existing methods
  • Accuracy (very important)
  • Easy to generate and use
  • X Quasi-steady state assumptions (QSSA)
  • ---difficult to choose QSSA species
  • X Intrinsic low-dimensional manifolds (ILDM)
  • X Rate-controlled constrained equilibrium
    (RCCE)
  • ---difficult to choose constraints
  • X Trajectory-generated low-dimensional
    manifold
  • X Flamelet generated manifolds (FGM)
  • X Roussel Fraser algorithm (RF)
  • Pre-Image Curves
  • ---Easy to choose the reduced composition
    while maintain the
  • accuracy
  • ---Reconstructed composition is
    independent of the reduced composition,
  • fully determined by the chemical
    kinetics

11
Dimension Reduction (Geometric Picture)
  • Represent combustion chemistry in terms of
    reduced
  • composition r (nr) instead of the full
    composition f(nf)
  • Impose nu nf-nr conditions which determine the
    manifold fm
  • ----i.e., given a reduced composition r,
    provide a procedure to
  • determine the corresponding full
    composition on the
  • manifold fm (Species reconstruction)

12
Pre-Image Curves (Ideas)
  • Use the fact that trajectories will be attracted
    to the low
  • dimension attracting manifold
  • Identify the corresponding composition point at
    the attracting
  • manifold as the reconstructed composition.
    (Identify the
  • attracting manifold)
  • The reconstructed composition (manifold
    construction) is
  • independent of the reduced composition r
  • Give the reduced composition r, construct a curve
    (Pre-image
  • curve) in the full composition space (the
    trajectories
  • starting from this curve will have the same
    reduced composition at some positive time)

13
Pre-Image Curves
  • Assumption there is an attracting manifold
    (black line)
  • Ideally, species reconstruction should identify
    point A
  • A good approximation to point A can being
    obtained by following the reaction trajectory
    from a point such as I
  • A suitable initial point I is achieved by
    generating a curve C in the pre-image manifold
    from a starting feasible point, denoted by O

Sketch of reaction trajectories in the pre-image
manifold MP.
How to generate the Pre-Image Curves?
14
Pre-Image Curves (Current Status)
  • Have identified the tangent space of the
    pre-image manifold
  • Have formulated different ways to construct the
    pre-image curves
  • Have understood the method itself to some extent
  • Plan to do a PaSR simulation to solve the
    embarrassment

15
Dimension reduction by Pre-Image Curves method
Trajectories colored by dimension
Reconstructed 1-dimension manifold (blue dashed
line)
16
Pre-image Curves Performance- Comparison with
QSSA and RCCE
QSSA Q10, Q12 RCCE R4, R6 Pre-image curve B4,
B6
Normalized error in reconstructed species at
different temperatures during autoignition.
Normalized errors in Pre-Image Curve are less
than those in RCCE and QSSA
17
Conclusion
  • Dimension reduction of combustion chemistry is
    crucial
  • and promising in numerical simulation of
    combustion
  • process with complicated fuels.
  • Developing new method with great accuracy
  • Combining dimension reduction with ISAT in
    simulations
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