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Characteristic chemical time scale analysis of a partial oxidation flame in hot syngas coflow Xinyu Li, Zhenghua Dai, and Fuchen Wang Energy Fuels, Just Accepted Manuscript • DOI: 10.1021/acs.energyfuels.6b02490 • Publication Date (Web): 13 Feb 2017 Downloaded from http://pubs.acs.org on February 14, 2017
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Characteristic chemical time scale analysis of a partial oxidation flame in hot syngas coflow
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Xinyu Li, Zhenghua Dai*, Fuchen Wang*
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Key Laboratory of Coal Gasification and Energy Chemical Engineering of Ministry of
5
Education, East China University of Science and Technology, Shanghai 200237, China
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KEYWORDS: Chemical time scale; Jacobian analysis; Partial oxidation; MILD
7
combustion
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Abstract: Characteristic chemical time scale analysis plays a key role in the
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understanding of turbulence-chemistry interaction in turbulent combustion research, and
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is also important basis for the selection or development of combustion models in
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turbulent combustion modeling. A new method named Main Direction Identification
12
(MDID) was developed based on the modification of CTS-ID (Chemical time scale
13
identification) method to achieve the function of identifying the characteristic time scale.
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Direction weight factor combined with mole fraction limit were used as a criterion in
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MDID to determine the characteristic time scale. MDID was applied to study
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characteristic chemical time scales of a CH4-O2 inverse diffusion flame in hot syngas
17
coflow, which is a model flame developed before to study the combustion process in
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partial oxidation reformers. Results show that chemical time scale given by the MDID
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method is about 10-5s in combustion area and 10-2s in reforming area. The main reaction
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pathway was also analyzed using MDID method. The new method was compared with
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three existing methods published in previous studies, the Damköhler numbers given by
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MDID are more consistent with the mild combustion nature of the flame compared with
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other methods. Then the MDID method was evaluated on a conventional oxy-fuel type
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high temperature flame to assess its flexibility to different reaction regimes. The time
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scale variation accurately reflects the changes of reaction regimes, indicating that the
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MDID method performs well on reacting flows varying from fast reaction regime to slow
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reaction regime. The effect of mole fraction limit on this method was also studied.
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1. Introduction
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Numerical simulation is an important tool in the studying of turbulent reacting process
30
in combustion devices such as gas turbines and gasifiers. In these devices, turbulent flow
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and complex reactions occur simultaneously and interact with each other. Multi-scale is
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an important feature of such combustion device, its flow and chemical timescales often
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vary several orders of magnitude. This multiple time scale phenomenon makes the
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interaction between turbulence and reaction very complex and brings enormous
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difficulties to the development of numerical models
1-3
. So it is critical for the selection
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and development of combustion models to have a deep insight into the interaction
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between turbulence and chemical reaction.
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The analysis of flow time scale and characteristic chemical time scale is an important
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way to understand the turbulence-chemistry interaction. According to the ratio of the two
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time scales, combustion processes can be divided into different regimes
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chemistry is fast compared to the eddy turnover time, the flame is in flamelet regime
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where the flame preserves a laminar flamelet shape within the smallest turbulent
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structures. Chemical reactions and turbulence mixing can be decoupled in numerical
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modeling 6-7. When the chemical time scale is much slower than the flow time scale, the
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overall reaction rate is limited by chemistry. In the case where chemical time scale and
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flow time scale are comparable, both turbulence and chemistry play a fundamental role 8
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and the turbulence-chemistry interaction should be considered in the modeling. Chemical
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time scale analysis is also an important basis for many chemistry reduction methods, e.g.
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the Computational Singular Perturbation (CSP) method
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Dimensional Manifold (ILDM) method 10. Flow time scale usually can be represented by
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two characteristic time scales: the integral time scale = ⁄ and Kolmogorov time
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scale = ⁄ , where is the turbulent kinetic energy (m2·s-2), is the turbulent
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dissipation rate (m2·s-3) and is the kinematic viscosity (m2·s-1).
9
4-5
. When the
and the Intrinsic Low
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But the calculation of characteristic chemical time scale still lacks a unified method. In
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premixed combustion systems, the characteristic chemical time scale is often defined as 3
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the ratio of flame thickness and laminar flame speed : ⁄
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is not suited for non-premixed and Moderate or Intense Low Oxygen Dilution (MILD)
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combustion systems. Such complicated reaction systems usually contain hundreds of
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elementary reactions and the calculation of characteristic chemical time scale of such
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systems remains an open question. For these complex systems, it is usually easy to
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calculate chemical time scales based on the Jacobian matrix analysis method
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substantial literature3, 12-13 exists on this issue. The Jacobian analysis pointed out that
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reciprocals of the eigenvalues of the Jacobian matrix of chemical source terms can be
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regarded as chemical time scales of a reacting system. Such methods give multiple
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chemical time scales of the system but cannot give a characteristic time scale. While in
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the modeling of combustion process, a definite characteristic chemical time scale is
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usually needed to calculate parameters like Damköhler (Da) number. This is very useful
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for the choosing and improving of appropriate combustion models. For example, based
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on the Da numbers which characterize the turbulence-chemistry interaction, it can be
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evaluated whether the fast reaction models can be used for the modeling of a target
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reacting system. The characteristic chemical time scale and Da number can also be
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introduced into Eddy Dissipation Model (EDC) to improve its performance as
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demonstrated by A. Parente et al.
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time scale (MSTS) method based on Jacobian matrix analysis. This method performs
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Jacobian analysis for the artificially selected main species of a reacting system and
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. M. Rehm et al.
15
11
. But this definition
4
and
proposed a main species based
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regards the largest time scale as the characteristic chemical time scale. This method was
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also used by S.N.P. Vegendla
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Caudal et al.
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which can identify serval main characteristic time scales from all the time scales
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calculated by full Jacobian analysis. Principal Variable analysis (PVA) was introduced
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into Jacobian analysis process by B.J. Isaac to calculate characteristic chemical time scale
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18
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Prufert 19 to calculate the characteristic chemical time scale of a partial oxidation flame.
17
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to analyze the time scales in a high pressure gasifier. J.
came up with a chemical time scale identification (CTS-ID) method
. Recently a method called System Progress time scale (SPTS) was proposed by U.
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However, further studies are still necessary because the reliability of these methods
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have not been fully verified and sometimes big discrepancies exist between the results of
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these methods. In the present study a Main Direction Identification (MDID) method was
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developed based on CTS-ID method. And MDID method was further used to study the
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characteristic chemical time scales of a partial oxidation flame in hot syngas coflow. This
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partial oxidation flame is an inverse diffusion flame of CH4-O2 in hot syngas coflow and
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was developed to study the combustion process in non-catalytic partial oxidation
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reformer by the author 20. Previous analysis 20 had shown that the combustion area of this
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flame is in MILD combustion mode, while the chemical time scales and interactions
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between turbulence and chemistry have not been studied. This information is of crucial
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importance for the selection and development of proper combustion models for the
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simulation of partial oxidation process. The partial oxidation flame is also a good case for
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the assessment of different methods due to its multi reaction regime feature.
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In the following, a brief description of mathematical fundamentals of different methods
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is given in Section 2. The partial oxidation flame and some computation details are
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presented in Section 3. In Section 4, chemical time scale results of the partial oxidation
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flame using MDID method and further analysis on reaction pathway and eigenvalue are
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first presented, then validation of the results and a comparison with other methods are
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given in Section 4.2. The flexibility of this new method to different reaction regimes is
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studied in Section 4.3 and Section 4.4 discusses the sensitive of results to a model
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parameter in MDID method.
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2. Mathematical fundamentals
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2.1. Jacobian analysis process
107 108
Considering a reacting system containing K species and I elementary reactions at constant pressure and enthalpy. The chemical reaction system can be expressed as:
109
110
where z is the concentration vector of K species, S is the source terms induced by
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chemical reactions. The chemical source term Sk of the kth species can be written as a
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summation of the production rates for all reactions involving the kth species:
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=
= ∑
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(2)
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where is the stoichiometric coefficient for ith elementary reaction and qi is the ith
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elementary reaction rate which can be expressed as: = ∏%
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!
$ "#
− ' ∏%
!
$$ "#
(3)
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( where, and ' are the forward and reverse rate constant of the ith reaction, and
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(( and are the forward and reverse stoichiometric coefficients. These parameters can be
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calculated using chemical reaction mechanism files by the method given in 21.
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Assuming that the derivative exists, the following equation can be obtained by taking the time derivative of Eq. (1)
)
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-)
= * ∙ , * = -
(4)
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where J is the Jacobian matrix of S. Jacobian matrix J is actually time dependent, but
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considering that only time scales are of interest, the Jacobian matrix can be assumed to be
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locally time independent
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assuming that all the eigenvalues are different, the following equation can be obtained:
22
. So by performing the eigen-decomposition on J and
* = ./.0
127 128
(5)
where P is the matrix of eigenvectors, / is the diagonal matrix of eigenvalues.
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The Jacobian matrix which can be regarded as rate constant matrix of the reacting
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system has a unit of s-1. So the reciprocals of its eigenvalues can be regarded as the
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chemical time scales of the system.
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2 = |4
#|
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It is worth noting that the eigenvalues and eigenvectors of J are either real or complex.
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Complex eigenvalue indicates an oscillatory chemical mode, with the real part represents
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the characteristic velocity of growth or decay and the imaginary part corresponds to the
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oscillation frequency. In this case, the complex eigenvalues and eigenvectors have to be
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transformed into real to make the physical meaning of a time scale analysis obvious. See
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17, 22-23
for details of this algebraic transformation.
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From equations (2) - (4), it can be seen that the components of J depend on z and the
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reaction rate parameters. This implies that the eigenvalues of J will also depend on z.
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Thus once the species space of a reacting system is known, the chemical time scales can
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be obtained by calculating the Jacobian matrix and its eigenvalues at this state point.
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However due to the complex structure of the dynamical system, J has various
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eigenvalues. So multiple chemical time scales can be obtained using this method, but the
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characteristic time scale cannot be given by this method.
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2.2. Chemical Time Scales Identification method
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For a state point M of a reacting system, Jacobian matrix analysis can give chemical
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time scales associated to K system evolution directions. Among these directions, some
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are main directions while the others are minor. J. Caudal et al.
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Time Scales Identification (CTS-ID) method to identify the main directions. Assuming
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the system evolution direction at point M can be represented by chemical source term S
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proposed a Chemical
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of the reacting system, the K projection coefficient sj can be obtained by projecting S on
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the real valued eigenvector V of the Jacobian matrix J:
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155 156 157 158 159
= ∑% 5 5 65
(7)
In fact the above derivation process is the same with CSP analysis, and the projection coefficient s can be seen as the mode vector f in CSP theory. In CTS-ID method, a normalized weight factor 75 was defined to measure the importance of the jth direction to chemical source term. 75 =
89: ;: 8
#∈@,A! ‖9# ;# ‖
(8)
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According to the relevance of jth direction versus system evolution direction which is
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presented by S, 75 varies between 0 and 1. A value close to 1 indicates that this direction
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can be regarded as a main evolution direction of the system, a value close to zero means
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little relevance between this direction and the system main direction. 75 = 0.01 was
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used in CTS-ID method to identify the main directions.
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An index to identify the main chemical reaction pathway along each direction was also
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introduced in CTS-ID. The contribution of species i along direction j can be expressed as:
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F,5 = GHIJ5 K ∑A
;,:
#M@L;#,: L
(9)
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where 6,5 is the ith component of 65 , GHIJ5 K represents the sign of 5 . A positive
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sign of F,5 indicates that species i is produced in the jth direction while a negative sign
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means the opposite. If the weight factor of each direction is considered, then the index
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can be written as: ℎ,5 = F,5 75
172 173
(10)
2.3. Main direction identification method
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The method presented in section 2.2 can identify time scales associated with the several
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main evolution directions of the system, but the characteristic chemical time scale still
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cannot be determined. This study introduced a criterion to determine the characteristic
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time scale based on the above Jacobian analysis and CTS-ID process.
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The characteristic chemical time scale can be chosen as the time scale of the most
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relevant direction to the system evolution direction. An obvious and easy choice for the
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criterion is choosing the direction with largest 75 ( 75 = 1) as the main direction of the
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system. But there are some questions with this choice. One is that it is hard to make a
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choice when the weight factors of several directions are all close to 1. The second is that
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the direction with the largest 75 does not necessarily represent the main direction of the
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reacting system. In the method described in section 2.2, the system evolution direction is
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represented by chemical source term S, while S is determined by both chemical reaction
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rate constant and reactant concentration [X] through multiplicative relation, as shown in
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Eq. (1) and Eq. (2). Thus as long as the chemical reaction rate constant of one reaction
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direction j is large enough, the corresponding projection coefficient component sj
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obtained by Eq. (7) can be largest. So for the reaction direction with largest 75 , there is a 10
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case in which the chemical reaction constant is very large meanwhile the main reactant
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concentrations are very small. Low reactant concentrations mean that only a small
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portion of the system is involved in this direction. In this situation it’s not appropriate to
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choose this direction as the main direction due to its low reactant concentrations.
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To resolve this problem, a minimum concentration limit [Xc] must be made if one
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direction is to be chosen as the main direction. To facilitate comparison, mole fraction
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limit Xc instead of concentration limit [Xc] is used here. In combustion systems, the
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differentiation phenomenon of species concentration is obvious. The mole fractions of
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major species are usually much larger than those of intermediate species. So Xc =0.005 is
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chosen here as the minimum limit for mole fraction. The results are not very sensitive to
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this value in a near region as will be shown in Section 4.4. Assuming that u represents the
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decreasing 75 order, .,O represent the mole fraction of reactants in increasing F,O
202
order, the criterion to identify the characteristic main direction can be expressed as: .O >
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2 , & .RO
>
2
(11)
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If the mole fractions of first two main reactants of the largest weight factor direction
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SP11 and SP21 are both larger than the limit Xc, this direction can be seen as the main
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direction; while if the conditions are not met, the identification procedure Eq. (11) would
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be performed to the remaining directions with the order of u (decreasing 75 ) until the
208
main direction is determined. This method is named as Main Direction Identification
209
(MDID) method in present study. 11
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While it is worth to note that Xc=0.005 is not suited for O2, because even a very low
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mole fraction of O2 still play an important role in reactions. The limit for O2 is chosen as
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the mole fraction when the combustion regime ends which is determined by eigenvalues
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as shown later in Section 4.1.
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2.4. Brief introduction of three existing methods
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2.4.1. PVA and MSTS method
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The existence of high dimension in combustion system bring enormous difficulties to
217
the identification of characteristic chemical time scale. The Principal Variable Analysis
218
(PVA) method
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using Principle Variable method, and selects the slowest time scale of the reduced system
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as the characteristic time scale. The main process of the Principal Variable method is as
221
follow.
18
performs dimension reduction analysis on the high dimensional dataset
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For a dataset D, consisting of n observations of Q variables, its sample covariance
223
matrix can be defined as S = 1⁄I − 1 TU T. The covariance matrix represents the
224
variance of the variables. Values close to one indicate strong correlations between
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variables, whereas a value of zero indicates uncorrelated variables. Based on these
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correlations, unimportant variables can be removed from the origin dataset using B2
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method 24.
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Thus the original dataset D can be divided into two parts: the remained variables D(1)
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and the removed variables D(2). So the sample covariance matrix S can also be expressed
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as: Σ=W
231
232
ΣR X ΣRR
(12)
The partial covariance matrix of D(2) given D(1) can be defined as: 0 ΣR ΣRR, = ΣRR − ΣR Σ
233 234
Σ ΣR
(13)
The trace of ΣRR, was selected as the criterion of choosing q remained variables: 'Y2Z[\]],@ ^_
235
'Y2Z\
≤7
(14)
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Left hand of above equation can be interpreted as the variance information loss
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introduced by selecting q variables instead of origin dataset. In 18, a value of 0.01 was set
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for 7.
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Once the q main variables are obtained, q time scales can be get by performing
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Jacobian analysis, and the largest time scale can be regarded as the characteristic
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chemical time scale.
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The main species based time scale (MSTS) method proposed by M. Rehm et al.
15
is
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similar to the above PVA method. The difference is that MSTS method artificially selects
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q variables as the main variables of a reacting system.
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2.4.2. SPTS method
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The Jacobian matrix J of chemical reaction source S is actually the first partial
247
derivatives of S with respect to mass fraction Y. So considering from the point of
248
differential, for a system state M, the following formula holds:
249
ab
250
cd is the disturbance of mass fraction Y at point M. *cd can be regarded as the
251
velocity vector describing the velocity in which the system reacts on perturbations. So U.
252
Prufert 19 defined a time scale:
= *cd
(15)
e = ‖*cd ‖0
253
(16) )
254
cd can be selected as the direction of chemical source term S: cd = ‖)b ‖ . This system
255
progress time scale (SPTS) can be regarded as the time the system needs to react on
256
perturbations in the direction of linearized progress.
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3. Partial oxidation flame
b
258
The characteristic chemical time scales of a CH4-O2 inverse diffusion flame in hot
259
syngas coflow is studied in this work. A detailed description of the configuration can be
260
found in
261
combustion process in partial oxidation reformer. The hot syngas coflow was used to
262
simulate the hot recirculated syngas in reformer. A schematic view of the configuration is
263
shown in Figure 1 and the boundary conditions are shown in Table 1. The oxygen inlet
264
has an inner diameter of d = 4 mm and a tube thickness of 1 mm. The fuel tube has an
265
inner diameter of df = 8 mm.
20
, only a brief description is given here. This flame was designed to study the
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Figure 1. Geometry of the flame configuration.
268
Table 1. Boundary conditions for the partial oxidation flame. Oxygen
Methane
Coflow
T(K)
300
300
1600
Velocity(m/s)
100
100
5.4
Species(mole fraction) 100%O2 100%CH4 56%H2+32%CO+12%H2O 269
To perform the chemical time scale analysis, CFD simulations were conducted first to
270
get the mass fraction, density and temperature data on each grid. Averaged data from
271
RANS method are widely used in the chemical time sale analysis studies 16, 18-19, 25-27. Due
272
to the present work focused on the time scale model development, the methods used for
273
producing input data were kept similar with other time scale analysis studies. In this
274
study, the CFD modeling was reproduced from our previous study 20. A 2D axisymmetric
275
structured grid containing 50855 cells was chosen after a grid sensitivity study. A
276
modified standard k-ε turbulence model and Eddy Dissipation Concept (EDC) model
277
were adopted to simulate the flame. DRM22 mechanism 28 which contains 24 species and
278
104 elementary reactions was chosen. Detailed boundary conditions and descriptions of
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the modeling effort can be found in 20. In the theory of EDC model, a computational cell
280
is divided into two parts: reacting fine structure and non-reacting surrounding area
281
Thus two kinds of mass fraction can be given by EDC model: averaged mass fraction and
282
fine scale mass fraction. The fine scale mass fraction is directly computed by chemical
283
reaction mechanism in the fine structure, while the cell averaged mass fraction is the
284
weighted average mass fraction of fine scale area and surrounding area
285
this fact, the fine scale mass fraction data was used in this work although only very little
286
deviation exists between the results of the two dataset.
30
29
.
. Considering
287
The chemical time scale analysis were performed at each grid point in the flow field
288
and the analysis in this work were carried out in MATLAB. Symbol calculation was used
289
in the derivation process of chemical source term and Jacobian matrix to reduce the errors
290
caused by numerical calculations.
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4. Results and Discussions
292
4.1. Analysis of the partial oxidation flame using MDID method
293 294
Figure 2. Temperature profile of the CH4-O2 inverse diffusion flame in hot syngas
295
coflow.
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Figure 2 shows the temperature profile of the partial oxidation flame calculated using
297
the CFD model. The temperature is uniform and the peak temperature is about 1700K.
298
Previous study
299
combustion mode.
20
had shown that the combustion area of this flame is in MILD
300 301
Figure 3. Chemical time scales along the axis of the inverse diffusion flame.
302
Figure 3 shows the calculated characteristic chemical time scales along the flame axis.
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Considering that the main concern here is time scales of reacting areas, the time scale
304
calculation is only performed for areas with a temperature above 900K to reduce the
305
calculation costs. As shown in Figure 3, characteristic time scale decreases before x=100d
306
(d=4mm is the diameter of oxygen channel) and reaches minimum at x=100d, then
307
increases and slowly converges to a constant value. This means that the MDID method
308
identified the existence of combustion area and reforming area. The trough refers to
309
combustion area and the slowly increasing area after x=160d refers to the reforming area. 17
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310
The characteristic chemical time scale given by MDID method is about 10-5-10-4s in
311
combustion area and 10-2s in reforming area.
312 313
314
Figure 4. Profiles of largest positive eigenvalues, temperature and HRR along the axis.
The signs of the eigenvalues of Jacobian matrix J indicate the explosive or decaying 12, 31-33
315
nature of the system in the analysis of kinetic systems
316
indicate a trend of the direction towards equilibrium, while positive eigenvalues are
317
referred to explosive modes. To enhance the physical understanding of the system, the
318
eigenvalues were further analyzed. Figure 4 shows the largest positive eigenvalue fgYh ,
319
the hear release rate HRR and the temperature profile along the axis. Positive eigenvalue
320
first appears at x=62.5d. The reaction pathway of the direction associated with this
321
eigenvalue is FR i jFk i lR → FR O i jFo O. Note that this formula only refers to a
322
reaction pathway, so the two sides are not balanced. The weight factor of this direction is
323
1. These mean that ignition occurs at this point. The corresponding temperature is 964K,
324
which is close to the auto-ignition temperature of the local mixture. The HRR also starts 18
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to be positive from this point. The positive eigenvalue increases fast and reaches a
326
maximum at x=100d. Then the eigenvalue starts to decrease and approaches zero at
327
x=160d. So this direction lose their explosive nature at this point, indicating the end of
328
combustion area. The location of the end of combustion area given by eigenvalue
329
analysis agrees well with that given by the HRR and temperature. The HRR decreases to
330
zero at x=160d and the temperature starts to decrease after x=160d. After x=160d, all the
331
eigenvalues became negative, which means that the system evolves towards equilibrium.
332
The analysis of eigenvalues can be used to accurately identify the boundaries of
333
combustion area in partial oxidation flames.
334 335
Figure 5. Weights of leading reaction pathways and their corresponding time scales
336
(abscissa) and main components (blocks) at x=100d and x=250d, each bar corresponds to
337
a reaction pathway.
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338
Reaction pathway analysis of x=100d in combustion area and x=250d in reforming area
339
are shown in Figure 5. Only directions of the first six largest weight factors are given
340
here. For x=100d, the main reaction pathway is associated with the consumption of CH4,
341
H2 and O2 and the production of H2O, CO and CH3. The corresponding time scale is
342
10-5s. The weights of other reaction pathways can be ignored compared to the weight of
343
this pathway. This result shows that the combustion of CH4 and H2 is the main reaction at
344
x=100d and due to the lack of O2 in partial oxidation flame, CH4 is not completely
345
oxidized. Part of CH4 is oxidized into CO and part of CH4 decomposed into CH3 without
346
a further oxidation. At x=250d in reforming area, the main reaction pathway is associated
347
with the consumption of CO, H2O and the production of H2, CO2. This is a slow
348
reforming reaction with characteristic chemical time scale of 10-2s.
349
The discontinuity of the time scale near x=160d in Figure 3 is caused by oscillation
350
behavior of the local reacting system. As the oxygen decreases with x, the oxidation
351
reaction pathway becomes weaker and on the other hand the reforming pathway becomes
352
stronger. These two directions collapse into a complex conjugate pair at the end of
353
combustion area. This is a common phenomenon occurring at the intersection of two
354
stages for dynamic systems
355
factor than other directions near x=160d, was identified as the main direction and the time
356
scale was represented by the real part of its complex eigenvalues. The rapid decrease of
357
real part leads to large time scales near x=160d. After x=160d, reforming pathway was
32, 34
. This complex direction, which has a larger weight
20
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identified as main direction, and the characteristic time scale was also changed
359
accordingly.
360
4.2. Comparison with other methods
361
The present method is next compared with three existing methods which had been
362
employed in characteristic chemical time scale analysis: PVA, SPTS and MSTS. A brief
363
introduction of the three methods is given in Section 2.4. The CTS-ID method is not
364
involved because it gives multiple time scales at one point other than a single
365
characteristic time scale. The main species given by PVA method is H2, H2O2, CH2, CH4,
366
HCO and the main species chosen for MSTS method are CH4, O2, H2, CO, H2O, CO2. It
367
can be seen from Figure 6 that with the increase of x, all the four methods show similar
368
trend. The time scales decrease before x=100d and reach minimum at about x=100d, then
369
increase and stabilize near a constant value. All the methods identified the existence of
370
combustion area and reforming area and gave smaller time scales in combustion area,
371
larger values in reforming area. The time scales given by SPTS and MSTS are similar: in
372
combustion area the given time scales are 10-1s, in reforming area the time scales are
373
100s. While the time scales in combustion area given by PVA method are 10-3s and the
374
time scales in reforming area are 10-2s. Both the values are lower than the values given by
375
SPTS and MSTS. The Different choices of main specie between PVA and MSTS method
376
lead to the very different results. The time scales in reforming area given by MDID
21
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377
method are very similar to that of PVA, but the time scales in combustion area given by
378
MDID are much smaller than other methods, with an order of 10-4-10-5s.
379 380
Figure 6. Comparison of the characteristic time scales calculated by different methods.
381
No experimental work on the measuring of chemical time scale under MILD
382
combustion has been reported due to the difficulties in measurement. But many DNS
383
studies
384
comparable to the Kolmogorov flow time scale for MILD combustion, and the
385
corresponding Damköhler (Da) number defined as the ratio of Kolmogorov time scale
386
and chemical time scale Da = ⁄2 is of the order unity. So the Da number was
387
calculated to evaluate the results given by different methods. Figure 7 shows the Da
388
numbers on the flame axis calculated by different methods.
35-39
on MILD combustion have revealed that the chemical time scale 2 is
22
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389 390
Figure 7. Comparison of the Da numbers calculated by different methods.
391
Due to the formation of MILD combustion in this partial oxidation flame, the
392
combustion occur at a certain distance (about x =75d -125d) from the nozzle. In this
393
combustion area, the results given by the MDID method are very different from those of
394
the other three methods. The Da number given by MDID is of the order unity, indicating
395
that the flow time scale and chemical time scale is comparable and finite chemistry
396
should be considered in the modeling. However, Da numbers given by other three
397
methods are all much smaller than one which means that the flow time scale is much
398
smaller than chemical time scale and the flow is not affected by reactions in the
399
combustion area. This is unreasonable for a flame. The results of the new proposed
400
MDID method are more consistent with the nature of MILD combustion given by DNS
401
studies.
402
4.3. Flexibility of the MDID method to different reaction regimes 23
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403
The flexibility of MDID method to two different reaction regimes with Tr s 1 and
404
Tr ≪ 1 were studied in above sections, but fast reaction regime was not involved. When
405
the inverse diffusion type of the flame in Figure 1 changes to normal diffusion type, a
406
conventional high temperature flame including fast reactions can be obtained
407
also a common flame type in partial oxidation reformers. Figure 8 shows the temperature
408
profile of the partial oxidation flame in normal diffusion type. Since the O2 locates in the
409
outer channel of the burner, O2 reacts with the low velocity hot syngas immediately once
410
leaving the burner, and a high temperature flame is formed near the burner. The peak
411
temperature is about 3100K. To assess the flexibility of the MDID method to fast
412
reaction regime, MDID method was performed along the y=5mm line which penetrates
413
the high temperature area.
20
. This is
414 415
Figure 8. Temperature profile of the normal diffusion type flame in hot syngas coflow.
24
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416 417
Figure 9. Characteristic chemical time scales and temperature along y=5mm line of the
418
normal diffusion case.
419 420
Figure 10. Da numbers along y=5mm line of the normal diffusion case.
421
The characteristic chemical time scales and corresponding Da numbers along the
422
y=5mm line are shown in Figure 9 and Figure 10. In the high temperature area near the
423
burner exit, 2 is very small with an order of 10-8s. With the increase of x, the
424
temperature decreases significantly due to the mixing of low temperature CH4, and 2 25
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425
increases to 10-5s accordingly. In this area, moderate reactions occur between methane
426
and low concentration oxygen which has not been completely consumed. The
427
temperature has a slight increase and 2 shows a decrease correspondingly. Further
428
downstream the oxygen is totally consumed and reforming reactions occupy a dominant
429
position. The time scales slowly increase from 10-5s to 10-2s. The two peaks of time scale
430
at x=25d and x=170d were caused by the oscillation behaviors during the transition of
431
different reaction regimes. The time scale and Da number variations show the existence
432
of three reaction regimes in the flame: fast reaction regime (Tr ≫ 1, moderate reaction
433
regime Tr s 1 and slow reaction regime Tr ≪ 1. The changes of chemical time
434
scales given by MDID method agree well with the changes of reaction regime. This
435
indicates the well flexibility of the MDID method to different reaction regimes.
436
The existence of moderate reaction regime in this normal diffusion type flame in hot
437
syngas coflow has not been observed in previous studies. This observation means that
438
even for this high temperature flame, combustion models based on fast reaction
439
assumption are not enough to accurately describe the temperature and species profiles,
440
turbulence-chemistry interaction must be considered in the modeling.
441
4.4. Effect of minimum mole fraction limit Xc
442
In this section the effect of minimum mole fraction limit Xc on the time scale
443
identification results is studied. First the results of an identification process without a
444
mole fraction limit Xc will be presented. This process identifies the time scale of the 26
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direction with largest γj as the characteristic chemical time scale. The results are shown in
446
Figure 11. It can be seen that without Xc, the time scales become discontinuous and very
447
small time scales are identified in the post combustion range at about x=120d~200d. It is
448
unreasonable that the characteristic chemical time scales in post combustion area are
449
much smaller than those identified in combustion area. Compared with Figure 3 where
450
the Xc is considered, it can be concluded that the time scale results are much better
451
improved by introducing Xc.
452 453
Figure 11. Chemical time scales identified without Xc.
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454 455
Figure 12. Comparison of the chemical time scales obtained by different Xc.
456
However, not all the choices of the minimum mole fraction limit can lead to a good
457
result. The limit Xc=0.005 in MDID method was artificially chosen to distinguish the
458
major species and trace species. As a user input parameter, it may have an influence on
459
the results. So the sensitivity of time scale results on the value of Xc is studied in this part.
460
Since the role of Xc is to distinguish the major species and trace species, Xc should be
461
smaller than the lowest limit of major species and larger than the highest limit of trace
462
species. A reasonable range for Xc is 0.001~0.01. Figure 12 shows the time scales when
463
Xc varies inside of the range and outside of the range. When Xc varies inside of the range
464
(Xc=0.01 and 0.001), the time scale results given by different Xc agree perfectly; But
465
when Xc varies outside of the range, some outlier data points appear. For Xc=0.1, the data
466
points are abnormal in zone A, as shown in the figure. In Zone A, CH4 and O2 are the
467
first two main reactants, but due to the fact that mole fraction of CH4 is lower than the 28
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limit Xc =0.1 in this zone, the oxidation pathway is ignored by the algorithm and a less
469
important reaction pathway CO i FR l → jlR i FR is selected instead. For Xc=0.0005,
470
data points are abnormal in zone B. The mole fraction of CH3 in zone B is larger than the
471
limit Xc =0.0005, as a result the less important reaction pathway FR i jFo → H i jFk
472
is recognized as main pathway instead of the oxidation pathway. The fast time scale with
473
an order of 10-7s is given in zone B. So it can be found that both too high and too low
474
values of Xc will lead to bad results, and 0.001-0.01 is a reasonable range for Xc. The time
475
scale results are insensitive to the value of Xc if Xc is chosen in this specific range.
476
5. Conclusions
477
A characteristic chemical time scale identification method named MDID was
478
developed in the present study to analyze the characteristic chemical time scales of a
479
partial oxidation flame in hot syngas coflow. A criterion based on direction weight factor
480
and mole fraction limit was proposed to identify the characteristic time scale from the
481
numerous time scales obtained by full Jacobian analysis.
482
This method was first used to analyze the characteristic time scale of an inverse
483
diffusion flame of CH4-O2 in hot syngas coflow. Results show that the characteristic
484
chemical time scale is between 10-5s to 10-4s in combustion area, and 10-2s in reforming
485
area. The variations of characteristic time scale and obtained reaction pathway agree well
486
with the changes of reaction regimes in flame. The time scale results given by MDID
487
method were compared to other three existing methods: PVA method, SPTS method and 29
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488
MSTS method. The calculated Da numbers given by MDID method agree better with the
489
MILD combustion nature of the flame than other methods, indicating that MDID
490
performs better in the analysis of the case flame. The flexibility of MDID method for
491
different reaction regimes were further tested on a normal diffusion type partial oxidation
492
flame including fast reaction regime. The variation of calculated characteristic time scale
493
agreed well with the changes of reaction regimes.
494
Results of this study indicate that turbulence-chemistry interaction must be considered
495
in the modeling of partial oxidation process in order to accurately predict the scalar
496
profiles. Combustion models based on fast reaction assumption are not sufficient for the
497
modeling of such systems. The detailed knowledge of characteristic chemical time scales
498
of partial oxidation flames can also be used for the modification of combustion models
499
for partial oxidation reformer to better describe the turbulence-chemistry interaction and
500
this will be the objective of future work.
501
AUTHOR INFORMATION
502
Corresponding Authors
503 504 505
*E-mail:
[email protected] *E-mail:
[email protected] ACKNOWLEDGMENTS
30
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506
This research was supported by the Science and Technology Commission of Shanghai
507
Municipality (No. 15DZ1200802) and the Coal-based Key Science and Technology
508
Program of Shanxi Province, China (No. MH2014-01).
509
NOMENCLATURE
510
MDID = Main Direction Identification
511
CTS-ID = Chemical time scale identification
512
CSP = Computational Singular Perturbation
513
ILDM = Intrinsic Low Dimensional Manifold
514
MILD = Moderate and Intense Low Oxygen Dilution
515
Da = Damköhler
516
EDC = Eddy Dissipation Model
517
MSTS = Main species based time scale
518
PVA = Principal Variable analysis
519
SPTS = System Progress time scale
520
RANS = Reynolds-Averaged Navier-Stokes
521
HRR = Heat release rate
522
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