Combustion Modeling in FLUENT: Overview and Applications
This software training provides an overview of the capabilities of FLUENT for combustion modeling, including chemical kinetics, gas phase combustion models, discrete phase models, and pollutant models. Participants will learn about the wide range of applications for FLUENT, including furnaces, boilers, process heaters, gas turbines, and rocket engines. Key guidelines for combustion simulation are also covered.
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About Combustion Modeling in FLUENT: Overview and Applications
PowerPoint presentation about 'Combustion Modeling in FLUENT: Overview and Applications'. This presentation describes the topic on This software training provides an overview of the capabilities of FLUENT for combustion modeling, including chemical kinetics, gas phase combustion models, discrete phase models, and pollutant models. Participants will learn about the wide range of applications for FLUENT, including furnaces, boilers, process heaters, gas turbines, and rocket engines. Key guidelines for combustion simulation are also covered.. The key topics included in this slideshow are FLUENT, combustion modeling, chemical kinetics, gas phase combustion, pollutant models,. Download this presentation absolutely free.
1. Fluent Inc. 4/12/2015 1 Fluent Software Training TRN-99-003 Combustion Modeling in FLUENT
2. Fluent Inc. 4/12/2015 2 Fluent Software Training TRN-99-003 Outline Applications Overview of Combustion Modeling Capabilities Chemical Kinetics Gas Phase Combustion Models Discrete Phase Models Pollutant Models Combustion Simulation Guidelines
3. Fluent Inc. 4/12/2015 3 Fluent Software Training TRN-99-003 Applications Wide range of homogeneous and heterogeneous reacting flows Furnaces Boilers Process heaters Gas turbines Rocket engines Predictions of: Flow field and mixing characteristics Temperature field Species concentrations Particulates and pollutants Temperature in a gas furnace CO 2 mass fraction Stream function
4. Fluent Inc. 4/12/2015 4 Fluent Software Training TRN-99-003 Aspects of Combustion Modeling Dispersed Phase Models Droplet/particle dynamics Heterogeneous reaction Devolatilization Evaporation Governing Transport Equations Mass Momentum (turbulence) Energy Chemical Species Combustion Models Premixed Partially premixed Nonpremixed Pollutant Models Radiative Heat Transfer Models
5. Fluent Inc. 4/12/2015 5 Fluent Software Training TRN-99-003 Gas phase combustion Generalized finite rate formulation (Magnussen model) Conserved scalar PDF model (one and two mixture fractions) Laminar flamelet model ( V5 ) Zimont model ( V5 ) Discrete phase model Turbulent particle dispersion s Stochastic tracking Particle cloud model ( V5 ) Pulverized coal and oil spray combustion submodels Radiation models: DTRM, P-1, Rosseland and Discrete Ordinates ( V5 ) Turbulence models: k- , RNG k- , RSM, Realizable k- ( V5 ) and LES ( V5 ) Pollutant models: NO x with reburn chemistry ( V5 ) and soot Combustion Models Available in FLUENT
6. Fluent Inc. 4/12/2015 6 Fluent Software Training TRN-99-003 Modeling Chemical Kinetics in Combustion Challenging Most practical combustion processes are turbulent Rate expressions are highly nonlinear; turbulence-chemistry interactions are important Realistic chemical mechanisms have tens of species, hundreds of reactions and stiff kinetics (widely disparate time scales) Practical approaches Reduced chemical mechanisms Finite rate combustion model Decouple reaction chemistry from turbulent flow and mixing Mixture fraction approaches s Equilibrium chemistry PDF model s Laminar flamelet Progress variable s Zimont model
7. Fluent Inc. 4/12/2015 7 Fluent Software Training TRN-99-003 Generalized Finite Rate Model Chemical reaction process described using global mechanism. Transport equations for species are solved. These equations predict local time-averaged mass fraction, m j , of each species. Source term (production or consumption) for species j is net reaction rate over all k reactions in mechanism: R jk (rate of production/consumption of species j in reaction k ) is computed to be the smaller of the Arrhenius rate and the mixing or eddy breakup rate. Mixing rate related to eddy lifetime, k / . Physical meaning is that reaction is limited by the rate at which turbulence can mix species (nonpremixed) and heat (premixed).
8. Fluent Inc. 4/12/2015 8 Fluent Software Training TRN-99-003 Setup of Finite Rate Chemistry Models Requires: List of species and their properties List of reactions and reaction rates FLUENT V5 provides this info in a mixture material database. Chemical mechanisms and physical properties for the most common fuels are provided in database. If you have different chemistry, you can: Create new mixtures. Modify properties/reactions of existing mixtures.
9. Fluent Inc. 4/12/2015 9 Fluent Software Training TRN-99-003 Generalized Finite Rate Model: Summary Advantages: Applicable to nonpremixed, partially premixed, and premixed combustion Simple and intuitive Widely used Disadvantages: Unreliable when mixing and kinetic time scales are comparable (requires Da >>1). No rigorous accounting for turbulence-chemistry interactions Difficulty in predicting intermediate species and accounting for dissociation effects. Uncertainty in model constants, especially when applied to multiple reactions.
10. Fluent Inc. 4/12/2015 10 Fluent Software Training TRN-99-003 Conserved Scalar (Mixture Fraction) Approach: The PDF Model Applies to nonpremixed (diffusion) flames only Assumes that reaction is mixing-limited Local chemical equilibrium conditions prevail. Composition and properties in each cell defined by extent of turbulent mixing of fuel and oxidizer streams. Reaction mechanism is not explicitly defined by you. Reacting system treated using chemical equilibrium calculations ( prePDF ). Solves transport equations for mixture fraction and its variance, rather than species transport equations. Rigorous accounting of turbulence-chemistry interactions.
11. Fluent Inc. 4/12/2015 11 Fluent Software Training TRN-99-003 Mixture Fraction Definition The mixture fraction, f , can be written in terms of elemental mass fractions as: where Z k is the elemental mass fraction of some element, k . Subscripts F and O denote fuel and oxidizer inlet stream values, respectively. For simple fuel/oxidizer systems, the mixture fraction represents the fuel mass fraction in a computational cell. Mixture fraction is a conserved scalar: Reaction source terms are eliminated from governing transport equations.
12. Fluent Inc. 4/12/2015 12 Fluent Software Training TRN-99-003 Systems That Can be Modeled Using a Single Mixture Fraction Fuel/air diffusion flame: Diffusion flame with oxygen- enriched inlets: System using multiple fuel inlets: 60% CH 4 40% CO 21% O 2 79% N 2 f = 1 f = 0 35% O 2 65% N 2 60% CH 4 40% CO 35% O 2 65% N 2 f = 1 f = 0 f = 0 60% CH 4 20% CO 10% C 3 H 8 10% CO 2 21% O 2 79% N 2 f = 1 f = 0 f = 1 60% CH 4 20% CO 10% C 3 H 8 10% CO 2
13. Fluent Inc. 4/12/2015 13 Fluent Software Training TRN-99-003 Equilibrium Approximation of System Chemistry Chemistry is assumed to be fast enough to achieve equilibrium. Intermediate species are included.
14. Fluent Inc. 4/12/2015 14 Fluent Software Training TRN-99-003 PDF Modeling of Turbulence-Chemistry Interaction Fluctuating mixture fraction is completely defined by its probability density function (PDF). p ( V ), the PDF, represents fraction of sampling time when variable, V , takes a value between V and V + V . p ( f ) can be used to compute time-averaged values of variables that depend on the mixture fraction, f : Species mole fractions Temperature, density
15. Fluent Inc. 4/12/2015 15 Fluent Software Training TRN-99-003 PDF Model Flexibility Nonadiabatic systems: In real problems, with heat loss or gain, local thermo-chemical state must be related to mixture fraction, f , and enthalpy, h . Average quantities now evaluated as a function of mixture fraction, enthalpy (normalized heat loss/gain), and the PDF, p ( f ). Second conserved scalar: With second scalar in FLUENT , you can model: Two fuel streams with different compositions and single oxidizer stream (visa versa) Nonreacting stream in addition to a fuel and an oxidizer Co-firing a gaseous fuel with another gaseous, liquid, or coal fuel Firing single coal with two off-gases (volatiles and char burnout products) tracked separately
16. Fluent Inc. 4/12/2015 16 Fluent Software Training TRN-99-003 Mixture Fraction/PDF Model: Summary Advantages: Predicts formation of intermediate species. Accounts for dissociation effects. Accounts for coupling between turbulence and chemistry. Does not require the solution of a large number of species transport equations Robust and economical Disadvantages: System must be near chemical equilibrium locally. Cannot be used for compressible or non-turbulent flows. Not applicable to premixed systems.
17. Fluent Inc. 4/12/2015 17 Fluent Software Training TRN-99-003 The Laminar Flamelet Model Temperature, density and species (for adiabatic) specified by two parameters, the mixture fraction and scalar dissipation rate Recall that for the mixture fraction PDF model (adiabatic), thermo-chemical state is function of f only can be related to the local rate of strain Extension of the mixture fraction PDF model to moderate chemical nonequilibrium Turbulent flame modeled as an ensemble of stretched laminar, opposed flow diffusion flames
18. Fluent Inc. 4/12/2015 18 Fluent Software Training TRN-99-003 Laminar Flamelet Model (2) Statistical distribution of flamelet ensemble is specified by the PDF P(f, ) , which is modeled as P f (f) P ( ) , with a Beta function for P f (f) and a Dirac-delta distribution for P ( ) Only available for adiabatic systems in V5 Import strained flame calculations prePDF or Sandias OPPDIF code Single or multiple flamelets Single: user specified strain, a Multiple: strained flamelet library, 0 < a < a extinction a=0 equilibrium a= a extinction is the maximum strain rate before flame extinguishes Possible to model local extinction pockets (e.g. lifted flames)
19. Fluent Inc. 4/12/2015 19 Fluent Software Training TRN-99-003 The Zimont Model for Premixed Combustion Thermo-chemistry described by a single progress variable, Mean reaction rate, Turbulent flame speed, U t , derived for lean premixed combustion and accounts for Equivalence ratio of the premixed fuel Flame front wrinkling and thickening by turbulence Flame front quenching by turbulent stretching Differential molecular diffusion For adiabatic combustion, The enthalpy equation must be solved for nonadiabatic combustion
20. Fluent Inc. 4/12/2015 20 Fluent Software Training TRN-99-003 Discrete Phase Model Trajectories of particles/droplets/bubbles are computed in a Lagrangian frame. Exchange (couple) heat, mass, and momentum with Eulerian frame gas phase Discrete phase volume fraction must < 10% Although the mass loading can be large No particle-particle interaction or break up Turbulent dispersion modeled by Stochastic tracking Particle cloud ( V5) Rosin-Rammler or linear size distribution Particle tracking in unsteady flows ( V5 ) Model particle separation, spray drying, liquid fuel or coal combustion, etc. Continuous phase flow field calculation Particle trajectory calculation Update continuous phase source terms
21. Fluent Inc. 4/12/2015 21 Fluent Software Training TRN-99-003 Turbulent dispersion is modeled by an ensemble of Monte-Carlo realizations (discrete random walks) Particles convected by the mean velocity plus a random direction turbulent velocity fluctuation Each trajectory represents a group of particles with the same properties (initial diameter, density etc.) Turbulent dispersion is important because Physically realistic (but computationally more expensive) Enhances stability by smoothing source terms and eliminating local spikes in coupling to the gas phase Particle Dispersion: The Stochastic Tracking Model Coal particle tracks in an industrial boiler
22. Fluent Inc. 4/12/2015 22 Fluent Software Training TRN-99-003 Particle Dispersion: The Particle Cloud Model Track mean particle trajectory along mean velocity Assuming a 3D multi-variate Gaussian distribution about this mean track, calculate particle loading within three standard deviations Rigorously accounts for inertial and drift velocities A particle cloud is required for each particle type (e.g. initial d, etc.) Particles can escape, reflect or trap (release volatiles) at walls Eliminates (single cloud) or reduces (few clouds) stochastic tracking Decreased computational expense Increased stability since distributed source terms in gas phase BUT decreased accuracy since Gas phase properties (e.g. temperature) are averaged within cloud Poor prediction of large recirculation zones
23. Fluent Inc. 4/12/2015 23 Fluent Software Training TRN-99-003 Particle Tracking in Unsteady Flows Each particle advanced in time along with the flow For coupled flows using implicit time stepping, sub-iterations for the particle tracking are performed within each time step For non-coupled flows or coupled flows with explicit time stepping, particles are advanced at the end of each time step
24. Fluent Inc. 4/12/2015 24 Fluent Software Training TRN-99-003 Coal/Oil Combustion Models Coal or oil combustion modeled by changing the modeled particle to Droplet - for oil combustion Combusting particle - for coal combustion Several devolatilization and char burnout models provided. Note : These models control the rate of evolution of the fuel off-gas from coal/oil particles. Reactions in the gas (continuous) phase are modeled with the PDF or finite rate combustion model.
25. Fluent Inc. 4/12/2015 25 Fluent Software Training TRN-99-003 NO x Models NO x consists of mostly nitric oxide (NO). Precursor for smog Contributes to acid rain Causes ozone depletion Three mechanisms included in FLUENT for NO x production: Thermal NO x - Zeldovich mechanism (oxidation of atmospheric N) Most significant at high temperatures Prompt NO x - empirical mechanisms by De Soete, Williams, etc. Contribution is in general small Significant at fuel rich zones Fuel NO x - Empirical mechanisms by De Soete, Williams, etc. Predominant in coal flames where fuel-bound nitrogen is high and temperature is generally low. NO x reburn chemistry ( V5 ) NO can be reduced in fuel rich zones by reaction with hydrocarbons
26. Fluent Inc. 4/12/2015 26 Fluent Software Training TRN-99-003 Soot modeling in FLUENT Two soot formation models are available: One-step model (Khan and Greeves) Single transport equation for soot mass fraction Two-Step model (Tesner) Transport equations for radical nuclei and soot mass fraction concentrations Soot formation modeled by empirical rate constants where, C , p f , and are a model constant, fuel partial pressure and equivalence ratio, respectively Soot combustion (destruction) modeled by Magnussen model Soot affects the radiation absorption Enable Soot-Radiation option in the Soot panel
27. Fluent Inc. 4/12/2015 27 Fluent Software Training TRN-99-003 Combustion Guidelines and Solution Strategies Start in 2D Determine applicability of model physics Mesh resolution requirements (resolve shear layers) Solution parameters and convergence settings Boundary conditions Combustion is often very sensitive to inlet boundary conditions Correct velocity and scalar profiles can be critical Wall heat transfer is challenging to predict; if known, specify wall temperature instead of external convection/radiation BC Initial conditions While steady-state solution is independent of the IC, poor IC may cause divergence due to the number and nonlinearity of the transport equations Cold flow solution, then gas combustion, then particles, then radiation For strongly swirling flows, increase the swirl gradually
28. Fluent Inc. 4/12/2015 28 Fluent Software Training TRN-99-003 Combustion Guidelines and Solution Strategies (2) Underrelaxation Factors The effect of under-relaxation is highly nonlinear Decrease the diverging residual URF in increments of 0.1 Underrelax density when using the mixture fraction PDF model (0.5) Underrelax velocity for high bouyancy flows Underrelax pressure for high speed flows Once solution is stable, attempt to increase all URFs to as close to defaults as possible (and at least 0.9 for T, P-1 , swirl and species (or mixture fraction statistics)) Discretization Start with first order accuracy, then converge with second order to improve accuracy Second order discretization especially important for tri/tet meshes Discrete Phase Model - to increase stability, Increase number of stochastic tracks (or use particle cloud model) Decrease DPM URF and increase number of gas phase iterations per DPM
29. Fluent Inc. 4/12/2015 29 Fluent Software Training TRN-99-003 Combustion Guidelines and Solution Strategies (3) Magnussen model Defaults to finite rate/eddy-dissipation (Arrhenius/Magnussen) For nonpremixed (diffusion) flames turn off finite rate Premixed flames require Arrhenius term so that reactants dont burn prematurely May require a high temperature initialization/patch Use temperature dependent C p s to reduce unrealistically high temperatures Mixture fraction PDF model Model of choice if underlying assumptions are valid Use adequate numbers of discrete points in look up tables to ensure accurate interpolation (no affect on run-time expense) Use beta PDF shape
30. Fluent Inc. 4/12/2015 30 Fluent Software Training TRN-99-003 Combustion Guidelines and Solution Strategies (4) Turbulence Start with standard k- model Switch to RNG k- , Realizable k- or RSM to obtain better agreement with data and/or to analyze sensitivity to the turbulence model Judging Convergence Residuals should be less than 10 -3 except for T , P-1 and species , which should be less than 10 -6 The mass and energy flux reports must balance Monitor variables of interest (e.g. mean temperature at the outlet) Ensure contour plots of field variables are smooth, realistic and steady
31. Fluent Inc. 4/12/2015 31 Fluent Software Training TRN-99-003 Concluding Remarks FLUENT V5 is the code of choice for combustion modeling. Outstanding set of physical models Maximum convenience and ease of use Built-in database of mechanisms and physical properties Grid flexibility and solution adaption A wide range of reacting flow applications can be addressed by the combustion models in FLUENT . Make sure the physical models you are using are appropriate for your application.