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Journal ArticleDOI

The asymptotic structure of counterflow diffusion flames for large activation energies

01 Jul 1974-Acta Astronautica (Pergamon)-Vol. 1, Iss: 7, pp 1007-1039
TL;DR: In this paper, the structure of steady state diffusion flames is investigated by analyzing the mixing and chemical reaction of two opposed jets of fuel and oxidizer as a particular example, and an Arrhenius one-step irreversible reaction in the realistic limit of large activation energies.
About: This article is published in Acta Astronautica.The article was published on 1974-07-01 and is currently open access. It has received 792 citations till now. The article focuses on the topics: Premixed flame & Diffusion (business).

Summary (3 min read)

1. Introduction

  • Two basic classes of non premixed combustion problems can be defined as "initial-value problems", described either by ordinary differential equations with boundary conditions at only one point or by parabolic partial differential equations, and "boundary-value problems", described by ordinary differential equations with two boundary points or by elliptic partial differential equations.
  • In Section 7 the authors summarize the results and compare with other numerical results.
  • Initial value problems in combustion have been analyzed for large activation energies by Lifian and Crespo [25] .

2. Formulation

  • The authors shall analyze the simultaneous mixing and chemical reaction at the stagnation point of two counter-flow streams of fuel and oxidizer.
  • A one-step irreversible Arrhenius reaction will be considered, which is first order with respect to both fuel and oxidizer.
  • The authors shall use Fick's law, with equal diffusivities of mass and heat, to calculate the diffusion velocities.
  • The four different possible regimes that the authors shall encounter for large T a show the existence within the flow field of two regions, where the temperature is given in the first approximation by Eqs. ( 8) to (10) , separated by a thin reaction zone.
  • Too to the adiabatic flame temperature the authors may encounter a nearly frozen ignition regime, a partial burning regime, a pre-mixed flame regime and finally a diffusion controlled or diffusion flame regime.

2. Partial burning regime.

  • Infinitely thin in the limit T a ~* <», reaction region which acts as sink for the reactants; because the reaction rate is not sufficiently fast, leakage of both reactants through the flame occurs.
  • The asymptotic structure of counterfiow diffusion flames 1013.
  • The structure of the reaction zone is the same as the structure of the reaction zone of a premixed flame with heat loss toward the equilibrium side of the flame.
  • Two possibilities arise depending on the value of a+2j3.

4. Diffusion flame or near-equilibrium regime. For sufficiently high

  • Damkohler numbers a diffusion controlled regime exists in which equilibrium is reached, to the first approximation, on both sides of a thin reaction zone.
  • The authors shall see below, when analyzing the structure of the thin reaction zone, that for /3 < 1 and sufficiently high activation energies multiple solutions may exist for Damkohler numbers above a minimum "extinction D" and no solution for D below this value.
  • There are cases in which the extinction conditions do not occur under this regime but under the previous premixed flame regime.
  • The relation between flame temperature and Damkohler number will be obtained, sequentially for the different regimes in the following sections, from the matching conditions between the asymptotic expansions for the temperature in the reaction zone and in the outer regions.

3. Nearly frozen, ignition, regime

  • As indicated before, in this regime the Damkohler number is such that the temperature rise, above the frozen flow value, due to the chemical production term, is of order TJlT a , which is small compared with TV, but large enough so as to force us to retain in the equations the nonlinear effects associated with the Arrhenius exponent.
  • The authors look for the Damkohler number D that produces, at x -1/2 for example, a given increment in temperature of order e above the frozen flow value.
  • Equation (26) may also be obtained from Eq. ( 6) by neglecting the reactant consumption and linearizing the Arrhenius exponent around the higher boundary temperature in the manner of Frank-Kamenetskii [17] .
  • There the authors obtain the following asymptotic expression for the Ignition Damkohler number EQUATION ) where F(j8) is very accurately correlated by F(0) = 2/3 -/3 2 .
  • For £ close to one, in the ignition conditions the reaction zone structure is of the same form as that of the premixed flame regime, and then the results obtained in Section 5 may also be used to determine the ignition conditions.

4. Partial burning regime

  • If the activation temperature is large compared with the local temperature a very small change in this temperature below the maximum is necessary to freeze the chemical reaction.
  • Only at both outer edges of the mixing layer will, again, the large reaction time be comparable with an appropriately large residence time in thick zones, where the chemical reaction will go to completion without a significant increase in temperature.
  • Instead of basing this choice on the matching conditions with an asymptotic reaction zone solution for large activation energies.
  • Matching to the next order, intermediate between e° and e, carried out in intermediate variables, demands the equality, at the outer edges of the reaction zone, of the slopes of the temperature distribution given by the inner and outer expansions.
  • The extinction conditions cannot be determined from the analysis of this regime.

5. Premixed flame regime

  • This is not the case if 3 < 1, because then the temperature reaches its maximum value within the reaction zone, and the flow outside will be chemically frozen, to all algebraic orders in T a ' 1 ; the fuel and oxidizer after crossing the reaction zone will coexist in frozen flow.
  • The analysis is completely analogous, and the results may be directly written, for the case a +23 >.
  • The chemical reaction will be frozen to all algebraic orders in e, because the temperature in this region will be lower than T p and the Damkohler number is not high enough to offset the effect of the Arrhenius exponent.
  • Equation ( 52) is to be solved with the boundary conditions obtained from the matching conditions with the outer solutions given by Eq. ( 19) and (44).
  • The partial burning analysis of the previous reaction should be used for m > 1/2. When T p becomes close to T e the concentrations of both reactants in the reaction zone are small and have relative variations of order unity; then the authors must use the analysis of the near-equilibrium, diffusion flame regime that follows.

6. Near equilibrium, diffusion flame, regime

  • Finally, a diffusion controlled regime exists for which the flow is everywhere near equilibrium, so that in a first approximation the flame position and temperature distribution are determined by Eqs. (20) to (23) independently of chemical kinetics.
  • This corresponds to the Burke-Schumann[l8] and classical diffusion flame analysis [19] .
  • Equations ( 75) to (77) describe in the first approximation the non equilibrium effects, as dependent only on the reduced Damkohler number and y.
  • The retention in Eq. ( 75) of the exponential Arrhenius factor is essential for evaluating the non equilibrium effects in the near-extinction conditions.
  • There is leakage of both reactants through the flame as evidenced from the fact that (j8, -£)» and (j8i + £)_» are, functions of y and 8, different from zero.

7. Discussion and generalization

  • The analysis of the previous sections covers all the regimes that can be found when analysing diffusion flames, unless they are of the unsteady or evolution type [251, or the chemical reaction is multi-step and does not admit a simplified description by a single overall irreversible reaction.
  • It is interesting to observe that the parameter TJTr is the product of the nondimensional activation energy and the nondimensional heat release, or third Damkohler number, both based on the characteristic thermal energy at the temperature of the reaction zone.
  • Both curves, T b (D) and T P (D), have branches that exhibit an increasing temperature with decreasing Damkohler numbers.
  • The analysis is not included because this transition regime will always be unstable (as is also the case with the partial burning regime).
  • Results for ignition, partial-burning and premixed-flame regimes appear, as well as a comparison of extinction Damkohler numbers with their numerical results.

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Citations
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Journal ArticleDOI
TL;DR: In this paper, the steady laminar counterflow diffusion flame exhibits a very similar scalar structure as unsteady distorted mixing layers in a turbulent flow field, and the conserved scalar model is interpreted as the most basic flamelet structure.

1,933 citations

Journal ArticleDOI
01 Jan 1988
TL;DR: In this article, it is shown that the inner structure of the flamelets is one-dimensional and time dependent, and a new coordinate transformation using the mixture fraction Z as independent variable leads to a universal description.
Abstract: The laminar flamelet concept covers a regime in turbulent combustion where chemistry (as compared to transport processes) is fast such that it occurs in asymptotically thin layers—called flamelets—embedded within the turbulent flow field. This situation occurs in most practical combustion systems including reciprocating engines and gas turbine combustors. The inner structure of the flamelets is one-dimensional and time dependent. This is shown by an asymptotic expansion for the Damkohler number of the rate determining reaction which is assumed to be large. Other non-dimensional chemical parameters such as the nondimensional activation energy or Zeldovich number may also be large and may be related to the Damkohler number by a distinguished asymptoiic limit. Examples of the flamelet structure are presented using onestep model kinetics or a reduced four-step quasi-global mechanism for methane flames. For non-premixed combustion a formal coordinate transformation using the mixture fraction Z as independent variable leads to a universal description. The instantaneous scalar dissipation rate χ of the conserved scalar Z is identified to represent the diffusion time scale that is compared with the chemical time scale in the definition of the Damkohler number. Flame stretch increases the scalar dissipation rate in a turbulent flow field. If it exceeds a critical value χ q the diffusion flamelet will extinguish. Considering the probability density distribution of χ , it is shown how local extinction reduces the number of burnable flamelets and thereby the mean reaction rate. Furthermore, local extinction events may interrupt the connection to burnable flamelets which are not yet reached by an ignition source and will therefore not be ignited. This phenomenon, described by percolation theory, is used to derive criteria for the stability of lifted flames. It is shown how values of ∋ q obtained from laminar experiments scale with turbulent residence times to describe lift-off of turbulent jet diffusion flames. For non-premixed combustion it is concluded that the outer mixing field—by imposing the scalar dissipation rate—dominates the flamelet behaviour because the flamelet is attached to the surface of stoichiometric mixture. The flamelet response may be two-fold: burning or non-burning quasi-stationary states. This is the reason why classical turbulence models readily can be used in the flamelet regime of non-premixed combustion. The extent to which burnable yet non-burning flamelets and unsteady transition events contribute to the overall statistics in turbulent non-premixed flames needs still to be explored further. For premixed combustion the interaction between flamelets and the outer flow is much stronger because the flame front can propagate normal to itself. The chemical time scale and the thermal diffusivity determine the flame thickness and the flame velocity. The flamelet concept is valid if the flame thickness is smaller than the smallest length scale in the turbulent flow, the Kolmogorov scale. Also, if the turbulence intensity v′ is larger than the laminar flame velocity, there is a local interaction between the flame front and the turbulent flow which corrugates the front. A new length scale L G =v F 3 /∈ , the Gibson scale, is introduced which describes the smaller size of the burnt gas pockets of the front. Here v F is the laminar flame velocity and ∈ the dissipation of turbulent kinetic energy in the oncoming flow. Eddies smaller than L G cannot corrugate the flame front due to their smaller circumferential velocity while larger eddies up to the macro length scale will only convect the front within the flow field. Flame stretch effects are the most efficient at the smallest scale L G . If stretch combined with differential diffusion of temperature and the deficient reactant, represented by a Lewis number different from unity, is imposed on the flamelet, its inner structure will respond leading to a change in flame velocity and in some cases to extinction. Transient effects of this response are much more important than for diffusion flamelets. A new mechanism of premixed flamelet extinction, based on the diffusion of radicals out of the reaction zone, is described by Rogg. Recent progress in the Bray-Moss-Libby formulation and the pdf-transport equation approach by Pope are presented. Finally, different approaches to predict the turbulent flame velocity including an argument based on the fractal dimension of the flame front are discussed.

1,268 citations

Journal ArticleDOI
TL;DR: In this paper, the main issues and related closures of turbulent combustion modeling are reviewed and a review of the models for non-premixed turbulent flames is given, along with examples of numerical models for mean burning rates for premixed turbulent combustion.

1,069 citations

Journal ArticleDOI
TL;DR: In this article, a review of recent developments in flame theory is provided, in sufficient detail to give the reader a comprehensive introduction to the field, including the stability and flammability limits of planar fronts, cellular flames, flame stretch, turbulent and self-turbulizing flames, hydrodynamic interactions between weakly turbulent gas flows and wrinkled flame fronts, molecular diffusion effects of intermediate species involved in chain reactions.

912 citations

References
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Journal ArticleDOI
TL;DR: In this paper, the adequacy of direct one-step chemical kinetics for describing ignition and extinction in initially unmixed gases is studied through the particular case of inviscid axisymmetric stagnation-point flow.
Abstract: The adequacy of direct one-step chemical kinetics for describing ignition and extinction in initially unmixed gases is studied through the particular case of inviscid axisymmetric stagnation-point flow. Oxidant is assumed to blow from upstream infinity at a non-gaseous reservoir of pure fuel at its boiling (or sublimating) temperature. Before reaching the reservoir the oxidant reacts with gaseous fuel flowing in the opposite direction to form product and release heat. This heat is in part conducted and diffused to the reservoir interface to transform more fuel into the gaseous state and continue the steady-state burning. Second-order Arrhenius kinetics for Lewis-number unity is examined. A critical parameter characterizing the phenomenon is shown to be the first Damkohler similarity group D1, the ratio of a time characterizing the flow to a time characterizing the chemical activity.For small D1 the reactants convect away heat without releasing the energy stored in their chemical bonds. Regular perturbation about chemically frozen flow establishes this condition as the weak burning limit. For large D1 singular perturbation describes a narrow region of intense chemical activity. For infinite D1 (indefinitely fast rate of reaction) the region is reduced to a surface of discontinuity (the thin-flame kinetics of Burke & Schumann).For intermediate D1 numerical techniques establish that a solution describing burning of moderate intensity joins the two previously mentioned asymptotic limits. It is suggested that sudden transition of the system between the various branches in this domain of intermediate D1 accounts for the phenomena of ignition and extinction of burning.

274 citations

Journal ArticleDOI
TL;DR: In this paper, the limit of large activation energy for the process of simultaneous mixing and chemical reaction of two reactants undergoing a one-step irreversible Arrhenius reaction is studied.
Abstract: The limit of large activation energy is studied for the process of simultaneous mixing and chemical reaction of two reactants undergoing a one-step irreversible Arrhenius reaction. Consideration is restricted to problems of the evolution type—like unsteady mixing and boundary-layer combustion—for which the solution is uniquely determined in terms of the initial conditions. The continuous transition from the nearly-frozen to the near-equilibrium regimes is described. The analysis uncovers the existence of: (i) An ignition regime, in which a mixing layer develops with only minor effects of the chemical reaction, until a thermal runaway occurs somewhere within the mixing region; at this location chemical equilibrium then is established rapidly, (ii) A deflagration regime, in which premixed flames originate from the ignition point and move through the mixing region to burn completely the reactant not in excess. And (iii) a diffusion-flame regime, in which a thin diffusion flame, that is established w...

206 citations

Journal ArticleDOI
TL;DR: In this article, the transient state of a simplified model of a one-dimensional diffusion flame is considered and the governing equations which take into account diffusion, heat conduction, heat losses and finite-rate chemical kinetics are treated numerically to obtain steady-state solutions.

111 citations


"The asymptotic structure of counter..." refers background or methods or result in this paper

  • ...The middle branch, where Tb increases with decreasing Db, will very likely turn out to be unstable in a stability analysis similar to that presented by Kirkby and Schmitz[15,16]....

    [...]

  • ...That only the portion of the curve between the vertical tangents is dynamically unstable has been demonstrated by transient stability analysis, under suitably restricted conditions [16], The curve giving the maximum temperature vs the Damkohler number has been generated by somewhat laborious numerical solutions of the steady state equations [3-8,15,16] and by approximate methods of an ad hoc nature [1,8-10]....

    [...]

  • ...Stagnation-point counterflow of fuel and oxidizer [1-7], combustion of a spherical fuel droplet in an oxidizing atmosphere [8-12], planar one dimensional interdiffusion and reaction of fuel and oxidizer [14-16], are among the boundary-value problems that have been studied in efforts to clarify diffusion-flame structure....

    [...]