2D Direct Numerical Simulation of methane/air turbulent premixed flames under high turbulence intensity Julien Savre 04/13/2011

Size: px
Start display at page:

Download "2D Direct Numerical Simulation of methane/air turbulent premixed flames under high turbulence intensity Julien Savre 04/13/2011"

Transcription

1 1 2D Direct Numerical Simulation of methane/air turbulent premixed flames under high turbulence intensity Julien Savre 04/13/2011

2 2 Outline Why studying turbulent premixed flames under high turbulent intensity? A free, open-source compressible DNS code for combustion applications: The pencil-code What is the pencil-code? Numerics (brief) Physical modules Description of the cases and related issues Results Computational domain Initialization Characteristics

3 3 Outline Why studying turbulent premixed flames under high turbulent intensity? A free, open-source compressible DNS code for combustion applications: The pencil-code What is the pencil-code? Numerics (brief) Physical modules Description of the cases and related issues Results Computational domain Initialization and homogeneous turbulence Characteristics

4 4 Turbulent premixed flames at high Ka Combustion regimes and diagrams (Poinsot & Veynante, 2001): Ka 100 Karlovitz number: or

5 5 Turbulent premixed flames at high Ka Combustion regimes and diagrams (Poinsot & Veynante, 2001): (Kolmogorov scale smaller than the inner reaction zone thickness) Local/global extinction Combustion instabilities (blow-off)

6 6 Turbulent premixed flames at high Ka There is not a good understanding of what happens in that regime A good example: quenching/reignition phenomena A clear, comprehensive definition of quenching phenomena has yet to be given Several theories have been proposed and reviewed: Peters theory: the smallest turbulent eddies are able to penetrate the reaction zone and quench it Poinsot s suggestion: those small eddies are too weak and do not survive long enough to effectively quench the flame (importance of unsteadiness) Several mechanisms are involved and their respective contribution is still unclear (thermo-diffusive instabilities, differential diffusion, heat losses, flame strain, flame wrinkling...)

7 6 Turbulent premixed flames at high Ka There is not a good understanding of what happens in that regime A good example: quenching/reignition phenomena A clear, comprehensive definition of quenching phenomena has yet to be given Several theories have been proposed and reviewed: Peters theory: the smallest turbulent eddies are able to penetrate the reaction zone and quench it Poinsot s suggestion: those small eddies are too weak and do not survive long enough to effectively quench the flame (importance of unsteadiness) Several mechanisms are involved and their respective contribution is still unclear (thermo-diffusive instabilities, differential diffusion, heat losses, flame strain, flame wrinkling...)

8 7 Turbulent premixed flames at high Ka Studies of flames in the distributed reaction zone regime and limits: Few publications: Experimentally, the conditions required to create a flame in that regime are difficult to sustain (stability issues) Numerically, several obstacles must be overcome (size, memory, accuracy...) The existing investigations rely mainly on laminar flame/vortex interactions (f.i. Poinsot et al., JFM 1991)

9 7 Turbulent premixed flames at high Ka Studies of flames in the distributed reaction zone regime and limits: Few publications: Experimentally, the conditions required to create a flame in that regime are difficult to sustain (stability issues) Numerically, several obstacles must be overcome (size, memory, accuracy...) The existing investigations rely mainly on laminar flame/vortex interactions (f.i. Poinsot et al., JFM 1991) Mueller et al. 26th Symp., 1996

10 7 Turbulent premixed flames at high Ka Studies of flames in the distributed reaction zone regime and limits: Few publications: Experimentally, the conditions required to create a flame in that regime are difficult to sustain (stability issues) Numerically, several obstacles must be overcome (size, memory, accuracy...) The existing investigations rely mainly on laminar flame/vortex interactions (f.i. Poinsot et al., JFM 1991) Numerical issues: Finite chemistry phenomena require the use of relatively detailed kinetic mechanisms The grid resolution must be very small as the small dissipative turbulent scales are smaller than the inner reaction layer of the flame The time history of flame/turbulence interactions have to be accounted for (importance of transient phenomena)

11 8 Objectives The distributed reaction zone regime is relevant in various practical applications where quenching/reignition may occur No turbulent combustion model is really efficient to predict those phenomena At present, flamelet models are widely used, even under conditions for which they were not designed There is a real need in further improving our knowledge of this regime and in developing dedicated models

12 8 Objectives The distributed reaction zone regime is relevant in various practical applications where quenching/reignition may occur No turbulent combustion model is really efficient to predict those phenomena At present, flamelet models are widely used, even under conditions for which they were not designed There is a real need in further improving our knowledge of this regime and in developing dedicated models 2D DNS cases are designed here to study methane/air premixed flames in the distributed reaction zone regime

13 9 Outline Why studying turbulent premixed flames under high turbulent intensity? A free, open-source compressible DNS code for combustion applications: The pencil-code What is the pencil-code? Numerics (brief) Physical modules Description of the cases and related issues Results Computational domain Initialization Characteristics

14 10 What is the pencil-code? The pencil-code is a free, open-source, fully-compressible, high-order DNS code (available at Developed since 2001, originally for magnetohydrodynamics/astrophysics applications (A. Brandenburg, Stockholm and W. Dobler, Potsdam) Main characteristics: The code is accessible via SVN Systematic reproducibility auto-tests for troubleshooting The equations are solved along pencils in order to optimize the cash memory: all the instantaneous physical quantities are stored in 1D vectors in the x direction The code benefits from the contribution of several research groups around the world: very mature code Written in fortran 90/95 Easy to program and share its developments with the community via SVN

15 11 Numerics Compressible balance equations (solved under a non-conservative form): continuity equation equation of motion (for the velocity) entropy equation (temperature) species equations perfect gas law The equations are solved using a centered sixth-order explicit finite difference scheme (as opposed to compact schemes): facilitates parallelization (compact schemes require the resolution of a tridiagonal system) to avoid wiggles, upwind schemes are also available for entropy and density equations (5th or 4th order)

16 12 Numerics Domain, grids and BCs: Cartesian, cylindrical or spherical referential Cartesian grids (preferably in a power of 2 for FFTs) Non regular grids with local stretching (but no adaptive refinement) Available BCs: periodicity, walls (heated or not), symmetry (no-slip walls), regular inflow/outflow, nonreflecting inflow/outflow (characteristic boundary conditions) Time-stepping: A 3rd order 2N-Runge Kutta scheme is commonly used Possibility to use an implicit solver for stiff ODEs in combustion applications (LSODE, symmetric flux splitting procedure) The time step can either be chosen constant or set by limitations on the convective, diffusive or reaction terms: Compressible code: CFL based on acoustic waves

17 13 Physical modules Great modularity of the code: each physical process has its own module Great transparency as a lot of unnecessary modules remain black boxes (only the required modules are compiled) Easy to understand and to contribute Easy to debug For combustion applications, the main required modules are: NSCBC (non-reflecting boundary conditions) Entropy (resolution of the temperature equation) Equation of state Time-step Chemistry (for the implementation and validation of chemistry in pencil, see Babkovskaia et al., JCP 2011)

18 14 Chemistry module Evaluation of the chemical reaction rates as well as the transport and thermodynamic properties: The CHEMKIN formalism is employed All the input files are taken from CHEMKIN (chem.inp, tran.dat) This enables the use of generic detailed as well as reduced kinetics (ready-to-use CHEMKIN files can be found on the net) Transport properties: three possibilities available CHEMKIN format: species diffusion coefficients evaluated as mixture averages of simplified binary diffusion coefficients (Hirschfelder and Curtiss formalism) + flux expressed in terms of molar fraction gradient with the possibility to add Dufour and Soret effects Constant Lewis numbers for each species + Fick s law Simplified diffusion coefficients (power law of T) + Fick s law

19 15 Outline Why studying turbulent premixed flames under high turbulent intensity? A free, open-source compressible DNS code for combustion applications: The pencil-code What is the pencil-code? Numerics (brief) Physical modules Description of the cases and related issues Results Computational domain Initialization Characteristics

20 16 Intro DNS of premixed flame/turbulence interactions at high Karlovitz number (Ka >> 100) Short litterature review: Very limited simulations of flames under such conditions were reported: Poludnenko and Oran (C&F 2010), Aspden et al. x2 (33rd Symp., 2011) Remarks: the simulations reported are not DNSs (low-order schemes were used), Aspden et al. are underresolved, P&O use a 1-step irreversible chemistry Conclusion: Even with huge computational resources, DNSs of flames under high intensity turbulence are still out of reach unless stringent simplifications are made Considering the existing works on the topic, we don t have to be afraid of simplifying the simulations

21 17 Cases description Computational domain: 2D: in the flamelet regime, the flame is most likely to take a cylindrical shape (2D) rather than a spheroidal one (3D) 0.6x0.6 cm2 1024x1024 grid Dx 5.9 µm Boundary conditions: Periodic in y non-reflecting inflow/outflow in x Initialization: A cold turbulent field is first generated using a forcing function in the momentum equation: with: A laminar premixed flame calculated with FlameMaster is then overimposed to this initial turbulent field

22 18 Cases description Physics and Chemistry: We are here interested in methane/air flames A 16 species, 25 reactions scheme is used, suitable for lean premixed flames (Smooke & Giovangigli, 1991) Simplified transport is employed (constant Le for each species and heat conductivity expressed as a power of temperature) For all cases, the turbulence decays over a time equivalent to 1 eddy turnover-time Cases L (cm) u (cm/s) eta (µm) Re Ka Case Case Case

23 19 Outline Why studying turbulent premixed flames under high turbulent intensity? A free, open-source compressible DNS code for combustion applications: The pencil-code What is the pencil-code? Numerics (brief) Physical modules Description of the cases and related issues Results Computational domain Initialization Characteristics

24 20 2D decaying homogeneous turbulence Properties of decaying turbulence are crucial in those simulations. We have to be carefull that: The simulation is sufficiently well resolved (in our case, the flame front being much larger than the Kolmogorov scale, the resolution criterion is imposed by turbulence and not by the flame) Turbulence does not decay too much Decay of TKE in power of t after a short transient period: After some manipulations:

25 20 2D decaying homogeneous turbulence Properties of decaying turbulence are crucial in those simulations. We have to be carefull that: The simulation is sufficiently well resolved (in our case, the flame front being much larger than the Kolmogorov scale, the resolution criterion is imposed by turbulence and not by the flame) Turbulence does not decay too much Decay of TKE in power of t after a short transient period: After some manipulations: Existence of a threshold at high Re (m=-1) over which viscous effects decrease during the decay : physically inconsistent but hard to avoid

26 21 2D decaying homogeneous turbulence L=0.209, 1024 L=0.209, 2048 L=0.209, L=0.209, 1024 L=0.209, 2048 L=0.126, Ka=7000 L=0.209, Ka=820 k Ka x10 7 n = n = n = x10-7 1x Ka=7000, 1024 Ka=7000, 2048 Ka=820, 1024 Ka=7000, L=0.126 t t/tau To characterize the overall resolution: nu_e Fluid Mechanics seminar series t/tau 04/13/2011

27 21 2D decaying homogeneous turbulence L=0.209, 1024 L=0.209, 2048 L=0.209, L=0.209, 1024 L=0.209, 2048 L=0.126, Ka=7000 L=0.209, Ka=820 k Ka x10 7 n = n = n = x10-7 1x Ka=7000, 1024 Ka=7000, 2048 Ka=820, 1024 Ka=7000, L=0.126 t t/tau To characterize the overall resolution: nu_e Numerical dissipation Fluid Mechanics seminar series t/tau 04/13/2011

28 22 Instantaneous snapshots L=0.209, Ka=820 Progress variable contours: L=0.126, Ka=7000 Reaction zone: 0.75 < c < 0.95 L=0.209, Ka=7000 Vorticity iso-lines Fluid Mechanics seminar series 04/13/2011

29 23 Instantaneous snapshots Heat release contours and vorticity lines L=0.209, Ka=7000 L=0.209, Ka=820

30 23 Instantaneous snapshots Heat release contours and vorticity lines L=0.209, Ka=7000 L=0.209, Ka=820 Presence of small vortices within the reaction zone at Ka=7000

31 23 Instantaneous snapshots Heat release contours and vorticity lines L=0.209, Ka=7000 L=0.209, Ka=820 Presence of small vortices within the reaction zone at Ka=7000 Existence of low HR regions: local quenching in progress

32 24 Curvature correlations Correlations between local curvature and heat release rate at c=0.8 (inside the reaction zone) Positive correlation at Ka=820, 0 correlation at Ka=7000 In both cases: low heat release rate regions correspond to negatively curved elements (importance of curvature effects)

33 25 Remarks In cases 1 and 3, at Ka=7000, the flames belong to the distributed flame regime: Presence of small vortices inside the fuel consumption layer The reaction layer is quite irregular exhibiting locally stretched elements In case 2, at Ka=820, the flame seems not to belong to the distributed flame regime: No vortices are able to penetrate the reaction zone The reaction layer is very regular, with a constant thickness In all cases: The inner reaction layer is locally quenched, showing reduced HR rate Two important conclusions: The fuel consumption layer can be quenched even if small scale vortices cannot survive within it The distributed flame regime is reached for Karlovitz numbers much higher than 100

34 26 Remarks The limit Ka=100 is largely exceeded mainly because the definition of Ka doesn t account for thermal expansion as temperature increases Previous studies of laminar flame/vortex interactions have shown that the vortex surface in the burnt gases is multiplied by The vortex rotation velocity is divided by the same factor

35 26 Remarks The limit Ka=100 is largely exceeded mainly because the definition of Ka doesn t account for thermal expansion as temperature increases Previous studies of laminar flame/vortex interactions have shown that the vortex surface in the burnt gases is multiplied by The vortex rotation velocity is divided by the same factor Redifining the Karlovitz number according to gas expansion: Methane/air at Φ=0.7: τ=6.2

36 27 Remarks Corrected Ka estimates: Cases L (cm) Ka Ka* Cases Case Ka* is still a rough estimate but is coherent with the observations According to this new definition, Case 3 no longer belongs to the distributed flame regime, as suggested by the snapshots

37 27 Remarks Corrected Ka estimates: Cases L (cm) Ka Ka* Cases Case Ka* is still a rough estimate but is coherent with the observations According to this new definition, Case 3 no longer belongs to the distributed flame regime, as suggested by the snapshots In the following, another definition of the progress variable will be employed: Allows a detailed description of the entire flame front (including the oxidation layer)

38 28 Turbulent flame structure (case 2) Scatter plots of temperature and species mass fractions accross the flame with respect to the progress variable: Quasi linear response of T and major species mass fractions: consistent with the results of Aspden et al. (PCI 2011) with various fuels

39 29 Turbulent flame structure (case 2) Radical peaks (here H) are dramatically increased in the turbulent flame: chain branching reactions become dominant to the expense of chain terminating reactions Direct effect of turbulent mixing within the flame front Increased CO peak and equilibrium level: consistent with turbulent flame experiments

40 30 Turbulent flame structure (case 2) CH2O becomes significant early in the preheat zone suggesting flame broadening (in agreement with recent experimental observations) Unlike other radicals, CH3 formation is mainly decreased accross the flame

41 30 Turbulent flame structure (case 2) Overestimated levels of CH3 in the preheat zone: effects of reduced chemistry CH2O becomes significant early in the preheat zone suggesting flame broadening (in agreement with recent experimental observations) Unlike other radicals, CH3 formation is mainly decreased accross the flame

42 31 Conclusion Summary: 2D DNS of lean premixed turbulent methane/air flames at Ka > 100 were achieved Use of the pencil-code (evaluation of the code for complexe reactive flows) with reduced chemistry and simplified transport Investigation of turbulent flame structure and response of the inner reaction zone Conclusions: The pencil-code is perfectly adapted to the kind of simulations proposed here, and performed better than expected in terms of CPU time: simulation time of 120 h (for case 2) Case Nproc Phys. time N steps mean Δt CPU/Δt/pts total CPU µs ns 4.45 µs 3840 h

43 32 Conclusion Conclusions: Local quenching was observed along the inner reaction layer, but no global extinction (that seems far more difficult to achieve as the burnt gases constantly provide heat) The distributed flame regime is reached for higher Ka than expected: accounting for flow dilataion in the definition of Ka seems to provide a better evaluation of this limit The inner flame structure and species distributions seem consistent with experimental observations and numerical simulations:» Quasi linear response of temperature with respect to the fuel mass fraction» Broadening of the formaldehyde layer» Increased CO levels The chemical paths at such high turbulence intensities are highly perturbed:» Chain branching reactions are more dominant» The formation of formaldehyde via CH3 seems pivotal during the quenching process which raises one crucial issue:

44 32 Conclusion Conclusions: Local quenching was observed along the inner reaction layer, but no global extinction (that seems far more difficult to achieve as the burnt gases constantly provide heat) The distributed flame regime is reached for higher Ka than expected: accounting for flow dilataion in the definition of Ka seems to provide a better evaluation of this limit The inner flame structure and species distributions seem consistent with experimental observations and numerical simulations:» Quasi linear response of temperature with respect to the fuel mass fraction» Broadening of the formaldehyde layer» Increased CO levels The chemical paths at such high turbulence intensities are highly perturbed:» Chain branching reactions are more dominant» The formation of formaldehyde via CH3 seems pivotal during the quenching process which raises one crucial issue: Is it appropriate to use a reduced kinetic mechanism to predict small scale turbulence/flame interactions; & how accurate must be the CH3 reaction path?

45 33 Conclusion Future works: At least two more simulations could bring additional informations:» Ka=2000 (or Ka*=150): limit of the distributed flame regime in terms of Ka*» Ka=150: limit of the distributed flame regime in terms of Ka Detailed investigation of transport processes within the flame front: turbulent transport vs. differential diffusion (in progress) Study of time history of the quenching process: how the holes will evolve? Given the available computational resources, it seems still difficult to increase the accuracy of the simulations (3D, better resolution, more detailed chemistry...)

46 34 Overview of the chemical structure Carbon chain: Importance of reaction R13: Contribution of 2 reactions to the consumption of CH3: comparison between a positively curved region and a hole

47 34 Overview of the chemical structure Carbon chain: Importance of reaction R13: Contribution of 2 reactions to the consumption of CH3: comparison between a positively curved region and a hole Clear change in the chemical path: R11 becomes dominant to the expense of R13

48 34 Overview of the chemical structure Carbon chain: Importance of reaction R13: Contribution of 2 reactions to the consumption of CH3: comparison between a positively curved region and a hole Clear change in the chemical path: R11 becomes dominant to the expense of R13 The carbon chain is broken by a default of formaldehyde production

Turbulent Premixed Combustion

Turbulent Premixed Combustion Turbulent Premixed Combustion Combustion Summer School 2018 Prof. Dr.-Ing. Heinz Pitsch Example: LES of a stationary gas turbine velocity field flame 2 Course Overview Part II: Turbulent Combustion Turbulence

More information

A Priori Model for the Effective Lewis Numbers in Premixed Turbulent Flames

A Priori Model for the Effective Lewis Numbers in Premixed Turbulent Flames Paper # 070LT-0267 Topic: Turbulent Flames 8 th US National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22, 2013.

More information

Flame / wall interaction and maximum wall heat fluxes in diffusion burners

Flame / wall interaction and maximum wall heat fluxes in diffusion burners Flame / wall interaction and maximum wall heat fluxes in diffusion burners de Lataillade A. 1, Dabireau F. 1, Cuenot B. 1 and Poinsot T. 1 2 June 5, 2002 1 CERFACS 42 Avenue Coriolis 31057 TOULOUSE CEDEX

More information

Laminar Premixed Flames: Flame Structure

Laminar Premixed Flames: Flame Structure Laminar Premixed Flames: Flame Structure Combustion Summer School 2018 Prof. Dr.-Ing. Heinz Pitsch Course Overview Part I: Fundamentals and Laminar Flames Introduction Fundamentals and mass balances of

More information

Multicomponent transport impact on turbulent premixed H 2 /O 2 flames

Multicomponent transport impact on turbulent premixed H 2 /O 2 flames Multicomponent transport impact on turbulent premixed H /O flames Julien de Charentenay and Alexandre Ern ONERA, F-93 Châtillon, France and EC, ECP, F-995 Châtenay-Malabry cedex, France CERMICS, Ecole

More information

Best Practice Guidelines for Combustion Modeling. Raphael David A. Bacchi, ESSS

Best Practice Guidelines for Combustion Modeling. Raphael David A. Bacchi, ESSS Best Practice Guidelines for Combustion Modeling Raphael David A. Bacchi, ESSS PRESENTATION TOPICS Introduction; Combustion Phenomenology; Combustion Modeling; Reaction Mechanism; Radiation; Case Studies;

More information

D. VEYNANTE. Introduction à la Combustion Turbulente. Dimanche 30 Mai 2010, 09h00 10h30

D. VEYNANTE. Introduction à la Combustion Turbulente. Dimanche 30 Mai 2010, 09h00 10h30 D. VEYNANTE Introduction à la Combustion Turbulente Dimanche 30 Mai 2010, 09h00 10h30 Introduction to turbulent combustion D. Veynante Laboratoire E.M2.C. CNRS - Ecole Centrale Paris Châtenay-Malabry France

More information

Effects of turbulence and flame instability on flame front evolution

Effects of turbulence and flame instability on flame front evolution PHYSICS OF FLUIDS 18, 104105 2006 Effects of turbulence and flame instability on flame front evolution Jiao Yuan, Yiguang Ju, and Chung K. Law a Department of Mechanical and Aerospace Engineering, Princeton

More information

Flamelet Analysis of Turbulent Combustion

Flamelet Analysis of Turbulent Combustion Flamelet Analysis of Turbulent Combustion R.J.M. Bastiaans,2, S.M. Martin, H. Pitsch,J.A.vanOijen 2, and L.P.H. de Goey 2 Center for Turbulence Research, Stanford University, CA 9435, USA 2 Eindhoven University

More information

Exercises in Combustion Technology

Exercises in Combustion Technology Exercises in Combustion Technology Exercise 4: Turbulent Premixed Flames Turbulent Flow: Task 1: Estimation of Turbulence Quantities Borghi-Peters diagram for premixed combustion Task 2: Derivation of

More information

Application of a Laser Induced Fluorescence Model to the Numerical Simulation of Detonation Waves in Hydrogen-Oxygen-Diluent Mixtures

Application of a Laser Induced Fluorescence Model to the Numerical Simulation of Detonation Waves in Hydrogen-Oxygen-Diluent Mixtures Supplemental material for paper published in the International J of Hydrogen Energy, Vol. 30, 6044-6060, 2014. http://dx.doi.org/10.1016/j.ijhydene.2014.01.182 Application of a Laser Induced Fluorescence

More information

Modeling flame brush thickness in premixed turbulent combustion

Modeling flame brush thickness in premixed turbulent combustion Center for Turbulence Research Proceedings of the Summer Program 2006 299 Modeling flame brush thickness in premixed turbulent combustion By E. Knudsen, O. Kurenkov, S. Kim, M. Oberlack AND H. Pitsch Turbulent

More information

Lecture 14. Turbulent Combustion. We know what a turbulent flow is, when we see it! it is characterized by disorder, vorticity and mixing.

Lecture 14. Turbulent Combustion. We know what a turbulent flow is, when we see it! it is characterized by disorder, vorticity and mixing. Lecture 14 Turbulent Combustion 1 We know what a turbulent flow is, when we see it! it is characterized by disorder, vorticity and mixing. In a fluid flow, turbulence is characterized by fluctuations of

More information

Thermoacoustic Instabilities Research

Thermoacoustic Instabilities Research Chapter 3 Thermoacoustic Instabilities Research In this chapter, relevant literature survey of thermoacoustic instabilities research is included. An introduction to the phenomena of thermoacoustic instability

More information

Combustion basics... We are discussing gaseous combustion in a mixture of perfect gases containing N species indexed with k=1 to N:

Combustion basics... We are discussing gaseous combustion in a mixture of perfect gases containing N species indexed with k=1 to N: Combustion basics... T. Poinsot poinsot@imft.fr Only the things you should know to understand the following courses Mainly elements of laminar flame theory for premixed and diffusion flames 1 Copyright

More information

FLAME AND EDDY STRUCTURES IN HYDROGEN AIR TURBULENT JET PREMIXED FLAME

FLAME AND EDDY STRUCTURES IN HYDROGEN AIR TURBULENT JET PREMIXED FLAME FLAME AND EDDY STRUCTURES IN HYDROGEN AIR TURBULENT JET PREMIXED FLAME M. Shimura, K. Yamawaki, Y.-S. Shim, M. Tanahashi and T. Miyauchi Department of Mechanical and Aerospace Engineering Tokyo Institute

More information

A G-equation formulation for large-eddy simulation of premixed turbulent combustion

A G-equation formulation for large-eddy simulation of premixed turbulent combustion Center for Turbulence Research Annual Research Briefs 2002 3 A G-equation formulation for large-eddy simulation of premixed turbulent combustion By H. Pitsch 1. Motivation and objectives Premixed turbulent

More information

Lecture 8 Laminar Diffusion Flames: Diffusion Flamelet Theory

Lecture 8 Laminar Diffusion Flames: Diffusion Flamelet Theory Lecture 8 Laminar Diffusion Flames: Diffusion Flamelet Theory 8.-1 Systems, where fuel and oxidizer enter separately into the combustion chamber. Mixing takes place by convection and diffusion. Only where

More information

Simulating the combustion of gaseous fuels 6th OpenFoam Workshop Training Session. Dominik Christ

Simulating the combustion of gaseous fuels 6th OpenFoam Workshop Training Session. Dominik Christ Simulating the combustion of gaseous fuels 6th OpenFoam Workshop Training Session Dominik Christ This presentation shows how to use OpenFoam to simulate gas phase combustion Overview Theory Tutorial case

More information

DARS overview, IISc Bangalore 18/03/2014

DARS overview, IISc Bangalore 18/03/2014 www.cd-adapco.com CH2O Temperatur e Air C2H4 Air DARS overview, IISc Bangalore 18/03/2014 Outline Introduction Modeling reactions in CFD CFD to DARS Introduction to DARS DARS capabilities and applications

More information

S. Kadowaki, S.H. Kim AND H. Pitsch. 1. Motivation and objectives

S. Kadowaki, S.H. Kim AND H. Pitsch. 1. Motivation and objectives Center for Turbulence Research Annual Research Briefs 2005 325 The dynamics of premixed flames propagating in non-uniform velocity fields: Assessment of the significance of intrinsic instabilities in turbulent

More information

A comparison between two different Flamelet reduced order manifolds for non-premixed turbulent flames

A comparison between two different Flamelet reduced order manifolds for non-premixed turbulent flames 8 th U. S. National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22, 2013 A comparison between two different Flamelet

More information

DNS and LES of Turbulent Combustion

DNS and LES of Turbulent Combustion Computational Fluid Dynamics In Chemical Reaction Engineering IV June 19-24, 2005 Barga, Italy DNS and LES of Turbulent Combustion Luc Vervisch INSA de Rouen, IUF, CORIA-CNRS Pascale Domingo, Julien Réveillon

More information

Predicting NO Formation with Flamelet Generated Manifolds

Predicting NO Formation with Flamelet Generated Manifolds Predicting NO Formation with Flamelet Generated Manifolds J. A. van Oijen and L. P. H. de Goey Dept. Mechanical Engineering, Technische Universiteit Eindhoven P.O. Box, 6 MB Eindhoven, The Netherlands

More information

A validation study of the flamelet approach s ability to predict flame structure when fluid mechanics are fully resolved

A validation study of the flamelet approach s ability to predict flame structure when fluid mechanics are fully resolved Center for Turbulence Research Annual Research Briefs 2009 185 A validation study of the flamelet approach s ability to predict flame structure when fluid mechanics are fully resolved By E. Knudsen AND

More information

ANSYS Advanced Solutions for Gas Turbine Combustion. Gilles Eggenspieler 2011 ANSYS, Inc.

ANSYS Advanced Solutions for Gas Turbine Combustion. Gilles Eggenspieler 2011 ANSYS, Inc. ANSYS Advanced Solutions for Gas Turbine Combustion Gilles Eggenspieler ANSYS, Inc. 1 Agenda Steady State: New and Existing Capabilities Reduced Order Combustion Models Finite-Rate Chemistry Models Chemistry

More information

Advanced Numerical Methods for non-premixed Flames

Advanced Numerical Methods for non-premixed Flames 0 Advanced Numerical Methods for non-premixed Flames Annarita Viggiano Department of Environmental Engineering and Physics University of Basilicata Italy 1. Introduction Engine designers are under increasing

More information

LES Approaches to Combustion

LES Approaches to Combustion LES Approaches to combustion LES Approaches to combustion LES Approaches to Combustion W P Jones Department of Mechanical Engineering Imperial College London Exhibition Road London SW7 2AZ SIG on Combustion

More information

arxiv: v1 [physics.chem-ph] 6 Oct 2011

arxiv: v1 [physics.chem-ph] 6 Oct 2011 Calculation of the Minimum Ignition Energy based on the ignition delay time arxiv:1110.1163v1 [physics.chem-ph] 6 Oct 2011 Jens Tarjei Jensen a, Nils Erland L. Haugen b, Natalia Babkovskaia c a Department

More information

Analysis of lift-off height and structure of n-heptane tribrachial flames in laminar jet configuration

Analysis of lift-off height and structure of n-heptane tribrachial flames in laminar jet configuration Analysis of lift-off height and structure of n-heptane tribrachial flames in laminar jet configuration Stefano Luca*, Fabrizio Bisetti Clean Combustion Research Center, King Abdullah University of Science

More information

Application of FGM to DNS of premixed turbulent spherical flames

Application of FGM to DNS of premixed turbulent spherical flames Application of FGM to DNS of premixed turbulent spherical flames R.J.M. Bastiaans, G.R.A Groot, J.A. van Oijen and L.P.H. de Goey, Section Combustion Technology, Department of Mechanical Engineering, Eindhoven

More information

CFD Analysis of Vented Lean Hydrogen Deflagrations in an ISO Container

CFD Analysis of Vented Lean Hydrogen Deflagrations in an ISO Container 35 th UKELG Meeting, Spadeadam, 10-12 Oct. 2017 CFD Analysis of Vented Lean Hydrogen Deflagrations in an ISO Container Vendra C. Madhav Rao & Jennifer X. Wen Warwick FIRE, School of Engineering University

More information

Process Chemistry Toolbox - Mixing

Process Chemistry Toolbox - Mixing Process Chemistry Toolbox - Mixing Industrial diffusion flames are turbulent Laminar Turbulent 3 T s of combustion Time Temperature Turbulence Visualization of Laminar and Turbulent flow http://www.youtube.com/watch?v=kqqtob30jws

More information

A Ghost-fluid method for large-eddy simulations of premixed combustion in complex geometries

A Ghost-fluid method for large-eddy simulations of premixed combustion in complex geometries Center for Turbulence Research Annual Research Briefs 2005 269 A Ghost-fluid method for large-eddy simulations of premixed combustion in complex geometries By V. Moureau, P. Minot, C. Bérat AND H. Pitsch

More information

Overview of Turbulent Reacting Flows

Overview of Turbulent Reacting Flows Overview of Turbulent Reacting Flows Outline Various Applications Overview of available reacting flow models LES Latest additions Example Cases Summary Reacting Flows Applications in STAR-CCM+ Ever-Expanding

More information

Numerical Simulation of Pollutant Emission and Flame Extinction in Lean Premixed Systems. Gilles Eggenspieler

Numerical Simulation of Pollutant Emission and Flame Extinction in Lean Premixed Systems. Gilles Eggenspieler Numerical Simulation of Pollutant Emission and Flame Extinction in Lean Premixed Systems A Thesis Presented to The Academic Faculty by Gilles Eggenspieler In Partial Fulfillment of the Requirements for

More information

Impact of numerical method on auto-ignition in a temporally evolving mixing layer at various initial conditions

Impact of numerical method on auto-ignition in a temporally evolving mixing layer at various initial conditions Journal of Physics: Conference Series PAPER OPEN ACCESS Impact of numerical method on auto-ignition in a temporally evolving mixing layer at various initial conditions To cite this article: A Rosiak and

More information

Asymptotic Structure of Rich Methane-Air Flames

Asymptotic Structure of Rich Methane-Air Flames Asymptotic Structure of Rich Methane-Air Flames K. SESHADRI* Center for Energy and Combustion Research, Department of Mechanical and Aerospace Engineering, University of California at San Diego, La Jolla,

More information

Large-eddy simulation of an industrial furnace with a cross-flow-jet combustion system

Large-eddy simulation of an industrial furnace with a cross-flow-jet combustion system Center for Turbulence Research Annual Research Briefs 2007 231 Large-eddy simulation of an industrial furnace with a cross-flow-jet combustion system By L. Wang AND H. Pitsch 1. Motivation and objectives

More information

REDIM reduced modeling of quenching at a cold inert wall with detailed transport and different mechanisms

REDIM reduced modeling of quenching at a cold inert wall with detailed transport and different mechanisms 26 th ICDERS July 3 th August 4 th, 217 Boston, MA, USA REDIM reduced modeling of quenching at a cold inert wall with detailed transport and different mechanisms Christina Strassacker, Viatcheslav Bykov,

More information

Lecture 6 Asymptotic Structure for Four-Step Premixed Stoichiometric Methane Flames

Lecture 6 Asymptotic Structure for Four-Step Premixed Stoichiometric Methane Flames Lecture 6 Asymptotic Structure for Four-Step Premixed Stoichiometric Methane Flames 6.-1 Previous lecture: Asymptotic description of premixed flames based on an assumed one-step reaction. basic understanding

More information

Fluid Dynamics and Balance Equations for Reacting Flows

Fluid Dynamics and Balance Equations for Reacting Flows Fluid Dynamics and Balance Equations for Reacting Flows Combustion Summer School 2018 Prof. Dr.-Ing. Heinz Pitsch Balance Equations Basics: equations of continuum mechanics balance equations for mass and

More information

Lecture 15. The Turbulent Burning Velocity

Lecture 15. The Turbulent Burning Velocity Lecture 15 The Turbulent Burning Velocity 1 The turbulent burning velocity is defined as the average rate of propagation of the flame through the turbulent premixed gas mixture. In the laminar case, solutions

More information

Towards regime identification and appropriate chemistry tabulation for computation of autoigniting turbulent reacting flows

Towards regime identification and appropriate chemistry tabulation for computation of autoigniting turbulent reacting flows Center for Turbulence Research Annual Research Briefs 009 199 Towards regime identification and appropriate chemistry tabulation for computation of autoigniting turbulent reacting flows By M. Kostka, E.

More information

NUMERICAL ANALYSIS OF TURBULENT FLAME IN AN ENCLOSED CHAMBER

NUMERICAL ANALYSIS OF TURBULENT FLAME IN AN ENCLOSED CHAMBER NUMERICAL ANALYSIS OF TURBULENT FLAME IN AN ENCLOSED CHAMBER Naveen Kumar D 1*, Pradeep R 2 and Bhaktavatsala H R 3 1 Assistant Professor Department of Mechanical Engineering, M S Engineering College,

More information

CFD modeling of combustion

CFD modeling of combustion 2018-10 CFD modeling of combustion Rixin Yu rixin.yu@energy.lth.se 1 Lecture 8 CFD modeling of combustion 8.a Basic combustion concepts 8.b Governing equations for reacting flow Reference books An introduction

More information

Insights into Model Assumptions and Road to Model Validation for Turbulent Combustion

Insights into Model Assumptions and Road to Model Validation for Turbulent Combustion Insights into Model Assumptions and Road to Model Validation for Turbulent Combustion Venke Sankaran AFRL/RQR 2015 AFRL/RQR Basic Research Review UCLA Jan 20, 2015 AFTC PA Release# 15011, 16 Jan 2015 Goals

More information

Direct Numerical Simulations of Diffusion Flame Extinction at Different Pressures

Direct Numerical Simulations of Diffusion Flame Extinction at Different Pressures Paper # 070LT-0330 Topic: Laminar & Turbulent flames 8 th US National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22,

More information

New sequential combustion technologies for heavy-duty gas turbines

New sequential combustion technologies for heavy-duty gas turbines New sequential combustion technologies for heavy-duty gas turbines Conference on Combustion in Switzerland 07.09.2017 ETH Zurich Nicolas Noiray, Oliver Schulz CAPS Lab D-MAVT ETH Nicolas Noiray 07/09/17

More information

Modeling of Wall Heat Transfer and Flame/Wall Interaction A Flamelet Model with Heat-Loss Effects

Modeling of Wall Heat Transfer and Flame/Wall Interaction A Flamelet Model with Heat-Loss Effects 9 th U. S. National Combustion Meeting Organized by the Central States Section of the Combustion Institute May 17-20, 2015 Cincinnati, Ohio Modeling of Wall Heat Transfer and Flame/Wall Interaction A Flamelet

More information

Extinction and reignition in a diffusion flame: a direct numerical simulation study

Extinction and reignition in a diffusion flame: a direct numerical simulation study J. Fluid Mech. (24), vol. 518, pp. 231 259. c 24 Cambridge University Press DOI: 1.117/S22112414 Printed in the United Kingdom 231 Extinction and reignition in a diffusion flame: a direct numerical simulation

More information

Unsteady Flow Evolution and Combustion Dynamics of Homogeneous Solid Propellant in a Rocket Motor

Unsteady Flow Evolution and Combustion Dynamics of Homogeneous Solid Propellant in a Rocket Motor Unsteady Flow Evolution and Combustion Dynamics of Homogeneous Solid Propellant in a Rocket Motor SOURABH APTE and VIGOR YANG* Department of Mechanical and Nuclear Engineering, The Pennsylvania State University,

More information

THE DOMAIN OF INFLUENCE OF FLAME INSTABILITIES IN TURBULENT PREMIXED COMBUSTION

THE DOMAIN OF INFLUENCE OF FLAME INSTABILITIES IN TURBULENT PREMIXED COMBUSTION Twenty-Seventh Symposium (International) on Combustion/The Combustion Institute, 1998/pp. 971 978 THE DOMAIN OF INFLUENCE OF FLAME INSTABILITIES IN TURBULENT PREMIXED COMBUSTION H. BOUGHANEM and A. TROUVÉ

More information

DNS of EGR-Type Turbulent Flame in MILD Condition

DNS of EGR-Type Turbulent Flame in MILD Condition DNS of EGR-Type Turbulent Flame in MILD Condition Y. Minamoto, T. D. Dunstan, N. Swaminathan, R. S. Cant Department of Engineering, University of Cambridge, Cambridge CB2 1PZ, UK Abstract Three-dimensional

More information

Advanced Turbulence Models for Emission Modeling in Gas Combustion

Advanced Turbulence Models for Emission Modeling in Gas Combustion 1 Advanced Turbulence Models for Emission Modeling in Gas Combustion Ville Tossavainen, Satu Palonen & Antti Oksanen Tampere University of Technology Funding: Tekes, Metso Power Oy, Andritz Oy, Vattenfall

More information

Combustion Theory and Applications in CFD

Combustion Theory and Applications in CFD Combustion Theory and Applications in CFD Princeton Combustion Summer School 2018 Prof. Dr.-Ing. Heinz Pitsch Copyright 201 8 by Heinz Pitsch. This material is not to be sold, reproduced or distributed

More information

Boundary-Layer Theory

Boundary-Layer Theory Hermann Schlichting Klaus Gersten Boundary-Layer Theory With contributions from Egon Krause and Herbert Oertel Jr. Translated by Katherine Mayes 8th Revised and Enlarged Edition With 287 Figures and 22

More information

Dr.-Ing. Frank Beyrau Content of Lecture

Dr.-Ing. Frank Beyrau Content of Lecture Content of Lecture 1. Phenomenology of Combustion 2. Thermodynamic Fundamentals 3. Chemical Reaction Kinetics 4. Ignition and Ignition Limits 5. Laminar Flame Theory 6. Turbulent Combustion 7. Pollutants

More information

Modeling and Simulation of Plasma-Assisted Ignition and Combustion

Modeling and Simulation of Plasma-Assisted Ignition and Combustion Modeling and Simulation of Plasma-Assisted Ignition and Combustion Vigor Yang and Sharath Nagaraja Georgia Institute of Technology Atlanta, GA AFOSR MURI Fundamental Mechanisms, Predictive Modeling, and

More information

CHAPTER 7 SEVERAL FORMS OF THE EQUATIONS OF MOTION

CHAPTER 7 SEVERAL FORMS OF THE EQUATIONS OF MOTION CHAPTER 7 SEVERAL FORMS OF THE EQUATIONS OF MOTION 7.1 THE NAVIER-STOKES EQUATIONS Under the assumption of a Newtonian stress-rate-of-strain constitutive equation and a linear, thermally conductive medium,

More information

There are no simple turbulent flows

There are no simple turbulent flows Turbulence 1 There are no simple turbulent flows Turbulent boundary layer: Instantaneous velocity field (snapshot) Ref: Prof. M. Gad-el-Hak, University of Notre Dame Prediction of turbulent flows standard

More information

A first investigation on using a species reaction mechanism for flame propagation and soot emissions in CFD of SI engines

A first investigation on using a species reaction mechanism for flame propagation and soot emissions in CFD of SI engines A first investigation on using a 1000+ species reaction mechanism for flame propagation and soot emissions in CFD of SI engines F.A. Tap *, D. Goryntsev, C. Meijer, A. Starikov Dacolt International BV

More information

Analysis of Turbulent Flame Propagation in Equivalence Ratio-Stratified Flow

Analysis of Turbulent Flame Propagation in Equivalence Ratio-Stratified Flow Analysis of Turbulent Flame Propagation in Equivalence Ratio-Stratified Flow Edward S. Richardson 1 and Jacqueline H. Chen 2 1 Faculty of Engineering and the Environment, University of Southampton, Southampton,

More information

Extinction Limits of Premixed Combustion Assisted by Catalytic Reaction in a Stagnation-Point Flow

Extinction Limits of Premixed Combustion Assisted by Catalytic Reaction in a Stagnation-Point Flow 44th AIAA Aerospace Sciences Meeting and Exhibit 9-12 January 2006, Reno, Nevada AIAA 2006-164 Extinction Limits of Premixed Combustion Assisted by Catalytic Reaction in a Stagnation-Point Flow Jingjing

More information

Effects of Damköhler number on flame extinction and reignition in turbulent nonpremixed flames using DNS

Effects of Damköhler number on flame extinction and reignition in turbulent nonpremixed flames using DNS Effects of Damköhler number on flame extinction and reignition in turbulent nonpremixed flames using DNS David O. Lignell a,, Jacqueline H. Chen b, Hans A. Schmutz a a Chemical Engineering Department,

More information

ADVANCED DES SIMULATIONS OF OXY-GAS BURNER LOCATED INTO MODEL OF REAL MELTING CHAMBER

ADVANCED DES SIMULATIONS OF OXY-GAS BURNER LOCATED INTO MODEL OF REAL MELTING CHAMBER ADVANCED DES SIMULATIONS OF OXY-GAS BURNER LOCATED INTO MODEL OF REAL MELTING CHAMBER Ing. Vojtech Betak Ph.D. Aerospace Research and Test Establishment Department of Engines Prague, Czech Republic Abstract

More information

Turbulent boundary layer

Turbulent boundary layer Turbulent boundary layer 0. Are they so different from laminar flows? 1. Three main effects of a solid wall 2. Statistical description: equations & results 3. Mean velocity field: classical asymptotic

More information

The Effect of Flame Structure on Soot Formation and Transport in Turbulent Nonpremixed Flames Using Direct Numerical Simulation

The Effect of Flame Structure on Soot Formation and Transport in Turbulent Nonpremixed Flames Using Direct Numerical Simulation The Effect of Flame Structure on Soot Formation and Transport in Turbulent Nonpremixed Flames Using Direct Numerical Simulation David O. Lignell a,, Jacqueline H. Chen a, Philip J. Smith b, Tianfeng F.

More information

Before we consider two canonical turbulent flows we need a general description of turbulence.

Before we consider two canonical turbulent flows we need a general description of turbulence. Chapter 2 Canonical Turbulent Flows Before we consider two canonical turbulent flows we need a general description of turbulence. 2.1 A Brief Introduction to Turbulence One way of looking at turbulent

More information

Scalar gradient and small-scale structure in turbulent premixed combustion

Scalar gradient and small-scale structure in turbulent premixed combustion Center for Turbulence Research Annual Research Briefs 6 49 Scalar gradient and small-scale structure in turbulent premixed combustion By S. H. Kim AND H. Pitsch. Motivation and objectives The scalar gradient

More information

Lecture 7. Turbulence

Lecture 7. Turbulence Lecture 7 Content Basic features of turbulence Energy cascade theory scales mixing Basic features of turbulence What is turbulence? spiral galaxies NGC 2207 and IC 2163 Turbulent jet flow Volcano jet flow

More information

arxiv: v1 [physics.flu-dyn] 25 Nov 2018

arxiv: v1 [physics.flu-dyn] 25 Nov 2018 Combustion regimes in sequential combustors: Flame propagation and autoignition at elevated temperature and pressure O. Schulz,a, N. Noiray,a a CAPS Laboratory, Department of Mechanical and Process Engineering,

More information

Computational issues and algorithm assessment for shock/turbulence interaction problems

Computational issues and algorithm assessment for shock/turbulence interaction problems University of Nebraska - Lincoln DigitalCommons@University of Nebraska - Lincoln NASA Publications National Aeronautics and Space Administration 2007 Computational issues and algorithm assessment for shock/turbulence

More information

Large-eddy simulations of turbulent reacting stagnation point flows

Large-eddy simulations of turbulent reacting stagnation point flows Copyright 1997, American Institute of Aeronautics and Astronautics, Inc. AIAA Meeting Papers on Disc, January 1997 A9715437, AIAA Paper 97-0372 Large-eddy simulations of turbulent reacting stagnation point

More information

Berlin Institute of Technology (TU Berlin) Prof. Dr. Frank Behrendt Contact Fabien Halter Confirmation of paper submission Name: Co-author:

Berlin Institute of Technology (TU Berlin) Prof. Dr. Frank Behrendt Contact Fabien Halter Confirmation of paper submission Name:   Co-author: Berlin Institute of Technology Fasanenstr. 89 10623 Berlin CNRS ORLEANS Fabien Halter Avenue de Recherche Scientifique ORLEANS, France 4. Juni 14 www.flame-structure-2014.com Berlin Institute of Technology

More information

MUSCLES. Presented by: Frank Wetze University of Karlsruhe (TH) - EBI / VB month review, 21 September 2004, Karlsruhe

MUSCLES. Presented by: Frank Wetze University of Karlsruhe (TH) - EBI / VB month review, 21 September 2004, Karlsruhe MUSCLES Modelling of UnSteady Combustion in Low Emission Systems G4RD-CT-2002-00644 R&T project within the 5 th Framework program of the European Union: 1 Numerical computations of reacting flow field

More information

Analysis of dynamic models for turbulent premixed combustion

Analysis of dynamic models for turbulent premixed combustion Center for Turbulence Research Proceedings of the Summer Program 2012 387 Analysis of dynamic models for turbulent premixed combustion By D. Veynante, T. Schmitt, M. Boileau AND V. Moureau Very few attempts

More information

Modelling of transient stretched laminar flame speed of hydrogen-air mixtures using combustion kinetics

Modelling of transient stretched laminar flame speed of hydrogen-air mixtures using combustion kinetics Loughborough University Institutional Repository Modelling of transient stretched laminar flame speed of hydrogen-air mixtures using combustion kinetics This item was submitted to Loughborough University's

More information

DEVELOPMENT OF CFD MODEL FOR A SWIRL STABILIZED SPRAY COMBUSTOR

DEVELOPMENT OF CFD MODEL FOR A SWIRL STABILIZED SPRAY COMBUSTOR DRAFT Proceedings of ASME IMECE: International Mechanical Engineering Conference & Exposition Chicago, Illinois Nov. 5-10, 2006 IMECE2006-14867 DEVELOPMENT OF CFD MODEL FOR A SWIRL STABILIZED SPRAY COMBUSTOR

More information

Modeling Turbulent Combustion

Modeling Turbulent Combustion Modeling Turbulent Combustion CEFRC Combustion Summer School 2014 Prof. Dr.-Ing. Heinz Pitsch Copyright 2014 by Heinz Pitsch. This material is not to be sold, reproduced or distributed without prior written

More information

Lecture 12 The Level Set Approach for Turbulent Premixed Combus=on

Lecture 12 The Level Set Approach for Turbulent Premixed Combus=on Lecture 12 The Level Set Approach for Turbulent Premixed Combus=on 12.- 1 A model for premixed turbulent combus7on, based on the non- reac7ng scalar G rather than on progress variable, has been developed

More information

Direct Numerical Simulation of Nonpremixed Flame Extinction by Water Spray

Direct Numerical Simulation of Nonpremixed Flame Extinction by Water Spray 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 4-7 January 2010, Orlando, Florida AIAA 2010-218 Direct Numerical Simulation of Nonpremixed Flame Extinction

More information

Rouen LBV 2012 ACCURACY OF TWO METHODS TO MEASURE LAMINAR FLAME SPEEDS: (1) STEADY BUNSEN BURNER FLAMES AND (2) SPHERICAL FLAMES IN BOMBS.

Rouen LBV 2012 ACCURACY OF TWO METHODS TO MEASURE LAMINAR FLAME SPEEDS: (1) STEADY BUNSEN BURNER FLAMES AND (2) SPHERICAL FLAMES IN BOMBS. Rouen LBV 2012 ACCURACY OF TWO METHODS TO MEASURE LAMINAR FLAME SPEEDS: (1) STEADY BUNSEN BURNER FLAMES AND (2) SPHERICAL FLAMES IN BOMBS. A. Bonhomme, T. Boushaki*, L. Selle, B. Ferret and T. Poinsot

More information

Numerical Simulations of Hydrogen Auto-ignition in a Turbulent Co-flow of Heated Air with a Conditional Moment Closure

Numerical Simulations of Hydrogen Auto-ignition in a Turbulent Co-flow of Heated Air with a Conditional Moment Closure Numerical Simulations of Hydrogen Auto-ignition in a Turbulent Co-flow of Heated Air with a Conditional Moment Closure I. Stanković*, 1, A. Triantafyllidis, E. Mastorakos, C. Lacor 3 and B. Merci 1, 4

More information

Investigation of ignition dynamics in a H2/air mixing layer with an embedded vortex

Investigation of ignition dynamics in a H2/air mixing layer with an embedded vortex Paper # 070LT-0211 The 8th US National Meeting of the Combustion Institute, Park City, UT, May 19-22, 2013 Investigation of ignition dynamics in a H2/air mixing layer with an embedded vortex S.K. Menon

More information

CFD and Kinetic Analysis of Bluff Body Stabilized Flame

CFD and Kinetic Analysis of Bluff Body Stabilized Flame CFD and Kinetic Analysis of Bluff Body Stabilized ame A. Dicorato, E. Covelli, A. Frassoldati, T. Faravelli, E. Ranzi Dipartimento di Chimica, Materiali e Ingegneria Chimica, Politecnico di Milano, ITALY

More information

Assessment of a flame surface density-based subgrid turbulent combustion model for nonpremixed flames of wood pyrolysis gas

Assessment of a flame surface density-based subgrid turbulent combustion model for nonpremixed flames of wood pyrolysis gas PHYSICS OF FLUIDS VOLUME 16, NUMBER 10 OCTOBER 2004 Assessment of a flame surface density-based subgrid turbulent combustion model for nonpremixed flames of wood pyrolysis gas Xiangyang Zhou a) Department

More information

CAN A ONE-DIMENSIONAL STRAINED FLAME MODEL COMBUSTION IN FLAME-VORTEX INTERACTIONS?

CAN A ONE-DIMENSIONAL STRAINED FLAME MODEL COMBUSTION IN FLAME-VORTEX INTERACTIONS? CAN A ONE-DIMENSIONAL STRAINED FLAME MODEL COMBUSTION IN FLAME-VORTEX INTERACTIONS? Youssef Marzouk *, Habib Nam, and Ahmed Ghoniem * ymarz@mit.edu, hnnam@sandia.gov, ghoniem@mit.edu * Massachusetts Institute

More information

Nonpremixed ignition of H 2 /air in a mixing layer with a vortex

Nonpremixed ignition of H 2 /air in a mixing layer with a vortex Proceedings of the Combustion Institute 30 (2004) 415 421 Proceedings of the Combustion Institute www.elsevier.com/locate/proci Nonpremixed ignition of H 2 /air in a mixing layer with a vortex X.L. Zheng,

More information

Abstract It is of great theoretical interest to investigate the interaction between flames and vortices as a model problem to study turbulent combusti

Abstract It is of great theoretical interest to investigate the interaction between flames and vortices as a model problem to study turbulent combusti Reduced Kinetic Mechanisms in Time Dependent Numerical Simulations of Nonpremixed Flames JOSHUA HSU 1 and SHANKAR MAHALINGAM Joint Center for Combustion and Environmental Research Department of Mechanical

More information

Interactions between oxygen permeation and homogeneous-phase fuel conversion on the sweep side of an ion transport membrane

Interactions between oxygen permeation and homogeneous-phase fuel conversion on the sweep side of an ion transport membrane Interactions between oxygen permeation and homogeneous-phase fuel conversion on the sweep side of an ion transport membrane The MIT Faculty has made this article openly available. Please share how this

More information

Extinction of stratified counterflow H 2 /air premixed flames under intense turbulence and strain

Extinction of stratified counterflow H 2 /air premixed flames under intense turbulence and strain Paper # 070LT-0219 Topic: Turbulent Flames 8 th U. S. National Combustion Meeting Organized by the Western States Section of the Combustion Institute and hosted by the University of Utah May 19-22, 2013

More information

Effects of Variation of the Flame Area and Natural Damping on Primary Acoustic Instability of Downward Propagating Flames in a Tube

Effects of Variation of the Flame Area and Natural Damping on Primary Acoustic Instability of Downward Propagating Flames in a Tube 5 th ICDERS August 7, 015 Leeds, UK Effects of Variation of the Flame Area and Natural Damping on Primary Acoustic Instability of Downward Propagating Flames in a Tube Sung Hwan Yoon and Osamu Fujita Division

More information

XXXVIII Meeting of the Italian Section of the Combustion Institute

XXXVIII Meeting of the Italian Section of the Combustion Institute Coupling a Helmholtz solver with a Distributed Flame Transfer Function (DFTF) to study combustion instability of a longitudinal combustor equipped with a full-scale burner D. Laera*, S.M. Camporeale* davide.laera@poliba.it

More information

TOPICAL PROBLEMS OF FLUID MECHANICS 97

TOPICAL PROBLEMS OF FLUID MECHANICS 97 TOPICAL PROBLEMS OF FLUID MECHANICS 97 DOI: http://dx.doi.org/10.14311/tpfm.2016.014 DESIGN OF COMBUSTION CHAMBER FOR FLAME FRONT VISUALISATION AND FIRST NUMERICAL SIMULATION J. Kouba, J. Novotný, J. Nožička

More information

Mixing and Combustion in Dense Mixtures by William A. Sirignano and Derek Dunn-Rankin

Mixing and Combustion in Dense Mixtures by William A. Sirignano and Derek Dunn-Rankin Mixing and Combustion in Dense Mixtures by William A. Sirignano and Derek Dunn-Rankin At very high pressures and densities, what is different and what is similar about the processes of Injection and Atomization,

More information

Lecture 9 Laminar Diffusion Flame Configurations

Lecture 9 Laminar Diffusion Flame Configurations Lecture 9 Laminar Diffusion Flame Configurations 9.-1 Different Flame Geometries and Single Droplet Burning Solutions for the velocities and the mixture fraction fields for some typical laminar flame configurations.

More information

A priori Tabulation of Turbulent Flame Speeds via a Combination of a Stochastic Mixing Model and Flamelet Generated Manifolds 5

A priori Tabulation of Turbulent Flame Speeds via a Combination of a Stochastic Mixing Model and Flamelet Generated Manifolds 5 Konrad-Zuse-Zentrum für Informationstechnik Berlin Takustraße 7 D-14195 Berlin-Dahlem Germany HEIKO SCHMIDT 1 MICHAEL OEVERMANN 2 ROB J.M. BASTIAANS 3 ALAN R. KERSTEIN 4 A priori Tabulation of Turbulent

More information

Flow and added small-scale topologies in a turbulent premixed flame

Flow and added small-scale topologies in a turbulent premixed flame Flow and added small-scale topologies in a turbulent premixed flame L. Cifuentes*, A. Kempf* and C. Dopazo** luis.cifuentes@uni-due.de *University of Duisburg-Essen, Chair of Fluid Dynamics, Duisburg -

More information

Fluctuation dynamo amplified by intermittent shear bursts

Fluctuation dynamo amplified by intermittent shear bursts by intermittent Thanks to my collaborators: A. Busse (U. Glasgow), W.-C. Müller (TU Berlin) Dynamics Days Europe 8-12 September 2014 Mini-symposium on Nonlinear Problems in Plasma Astrophysics Introduction

More information