A comparative study of flamelet and finite rate chemistry LES for an axisymmetric dump combustor

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Present-day demands on combustion equipment are increasing the need for improved understanding and prediction of turbulent combustion. Large eddy simulation (LES), in which the large-scale flow is resolved on the grid, leaving only the small-scale flow to be modeled, provides a natural framework for combustion simulations, as the transient nature of the flow is resolved. In most situations, however, the flame is thinner than the LES grid, and subgrid modeling is required to also handle the turbulence-chemistry interactions. Here, we examine the predictive capabilities of the flamelet LES models, such as the Flamelet Progress Variable LES (LES-FPV) models, and the finite rate chemistry LES models, such as the LES-Thickened Flame Model (LES-TFM), the partially stirred reactor model (LES-PaSR) and the Eddy Dissipation Concept (LES-EDC) model. These different combustion LES models are used here to study the reacting flow in an axisymmetric dump combustor at a Reynolds number of 55,800, the Damköhler number of 167 and a Karlowitz number of 0.15, placing the flame in the corrugated flame regime. The computational results are compared to experimental data of velocity and temperature to examine predictive capabilities of the different models.

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CitationsShowing 10 of 25 papers
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  • Research Article
  • Cite Count Icon 3
  • 10.1155/2019/7042692
Large Eddy Simulation of Premixed Stratified Swirling Flame Using the Finite Rate Chemistry Approach
  • Mar 31, 2019
  • International Journal of Aerospace Engineering
  • Yinli Xiao + 2 more

Large eddy simulations of a stratified swirling flow of a Cambridge swirl burner for both nonreacting and reacting cases are conducted using a finite rate chemistry approach represented by a partially stirred reactor model. The large eddy simulation predictions are compared with experimental measurements for velocity, temperature, and concentrations of major species. The agreement is found in overall trend of velocity prediction, but temperature and concentration of major species show slight discrepancies in the central region. Two reduced chemical mechanisms are examined in the present paper with the objective of assessing their capabilities in predicting swirling flame characteristics, and the distinct difference using two mechanisms is found in CO distribution profiles, which is considered the consequence of different kinetics of CO-CO2 equilibrium. Flow structures are qualitatively and quantitatively analyzed with numerical results. Large-scale vortex structures and precession motions are observed in both nonreacting and reacting cases. Frequency of vortex shedding is identified from the point data of instantaneous velocity in the discharging stream-induced shear layer. On this basis, the intensity and frequency of precession motion are shown to be enhanced in the presence of combustion. Large-scale wrinkling of the flame surface is resolved and characterized in the flame zone, and the effect of mixture stratification is then further discussed.

  • Book Chapter
  • Cite Count Icon 6
  • 10.1007/978-981-10-7410-3_20
Combustion in Supersonic Flows and Scramjet Combustion Simulation
  • Dec 13, 2017
  • Vladimir A Sabelnikov + 1 more

The scramjet (supersonic combustion ramjet) is an air-breathing engine with the supersonic flow at the combustor entrance, i.e., with essentially lower deceleration of flow in the inlet with respect to common ramjet. The scramjet is designed for hypersonic flight of vehicle with Mach number large than 5 or 6, where the efficiency of a subsonic ramjet decreases, because the deceleration of high-speed flow to small subsonic speeds leads to extremely high temperature at the entrance to combustor, that, in its turn, generates a series of effects, deteriorating the performance of classical ramjet. The scramjet is characterized by strong coupling of all its elements. Supersonic core from the inlet to the nozzle, essential subsonic zones in thick boundary layers and high losses caused by strong shock waves, by viscous effects, by dissociation and radiation result in a situation, when positive thrust may be reached only on the basis of joint optimization of the whole flowpath. In comparison with experimental investigations, which remain very challenging to conduct in such flow conditions, computational fluid dynamics is an attractive complementary tool for the study supersonic reactive flow in the scramjet flowpath. Understanding and prediction of the flow structure are necessary for achieving the stable and efficient combustion, high thrust, and thermostable construction of the scramjet. The first half of the chapter addresses fundamentals of turbulent supersonic combustion: physics of combustion in supersonic flows with regard to scramjets, Navier--Stokes equations for multispecies reacting gas flow, kinetic schemes for simulation of scramjets, RANS/URANS, and LES approaches, the closure problems for turbulent fluxes. Particular attention is paid to the discussion of the difficulties when resolving closure problems for reaction rates. The contemporary models to account for turbulence-chemistry interactions (TCI) are shortly presented. The second half of the chapter focuses on partially stirred reactor (PaSR) turbulent combustion models. Transported PaSR (TPaSR) and unsteady PaSR models are described in details, and experience of their application to simulation of experiments on supersonic combustion (within the framework of LES approach) is demonstrated. Finally, the problem of the selection of “correct” solution among multiple solutions of PaSR steady-state equations is considered.

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  • Conference Article
  • Cite Count Icon 41
  • 10.1051/eucass/201304539
Extended LES-PaSR model for simulation of turbulent combustion
  • Jan 1, 2013
  • V Sabelnikov + 1 more

In this work, a novel model for Large Eddy Simulations (LES) of high Reynolds moderate Damkohler number turbulent flames is proposed. The development is motivated by the need for more accurate and versatile LES combustion models for engineering applications such as jet engines. The model is based on the finite rate chemistry approach in which the filtered species equations of a reduced reaction mechanism are solved prior to closure modeling. The modeling of the filtered reaction rate provides the challenge: as most of the chemical activity, and thus also most of the exothermicity occurs on the subgrid scales, this model needs to be based on the properties of fine-scale turbulence and mixing and Arrhenius chemistry. The model developed here makes use of the similarities with the mathematical treatment of multiphase flows together with the knowledge of fine-scale turbulence and chemistry obtained by Direct Numerical Simulation (DNS) and experiments. In the model developed, equations are proposed for the fine-structure composition and volume fraction that are solved together with the LES equations for the resolved scales. If subgrid convection can be neglected, the proposed model simplifies to the Partially Stirred Reactor (PaSR) model. To validate the proposed LES model, comparisons with experimental data and other LES results are made, using other turbulence chemistry interaction models, for a lean premixed bluff-body stabilized flame.

  • Research Article
  • Cite Count Icon 6
  • 10.1080/13647830.2018.1447148
LES modelling of turbulent non-premixed jet flames with correlated dynamic adaptive chemistry
  • Mar 27, 2018
  • Combustion Theory and Modelling
  • Zaigang Liu + 3 more

Large eddy simulations (LES) for turbulent flames with detailed kinetic mechanisms have received growing interest. However, a direct implementation of detailed kinetic mechanisms in LES modelling of turbulent combustion remains a challenge due to the requirement of huge computational resources. An on-the-fly mechanism reduction method named correlated dynamic adaptive chemistry (CoDAC) is proposed to overcome this issue. A LES was conducted for Sandia Flame-D, with the reaction mechanism of GRI-Mech 3.0 consisting of 53 species and 325 reactions. The reduction threshold used in LES was obtained a priori by using auto-ignition model and partially stirred reactor (PaSR) with pairwise mixing model. LES results with CoDAC are in good agreement with experimental data and those without reduction. The conditional mean of the number of selected species indicates that a large size of locally reduced mechanism is required in the reaction zone where CH4 is destructed. A computational time analysis shows that the PaSR model predicts better than the auto-ignition model on the wall time reduction with CoDAC in LES.

  • Research Article
  • Cite Count Icon 113
  • 10.1016/j.combustflame.2012.09.008
LES combustion modeling for high Re flames using a multi-phase analogy
  • Oct 25, 2012
  • Combustion and Flame
  • Vladimir Sabelnikov + 1 more

LES combustion modeling for high Re flames using a multi-phase analogy

  • Conference Article
  • Cite Count Icon 1
  • 10.2514/6.2024-0580
Large-Eddy Simulation of Supersonic Combustion in a Mach 2 Cavity-Based Model Scramjet Combustor
  • Jan 4, 2024
  • Guillaume Sahut + 5 more

Large-Eddy Simulation of Supersonic Combustion in a Mach 2 Cavity-Based Model Scramjet Combustor

  • Research Article
  • Cite Count Icon 12
  • 10.1016/j.fuel.2022.124756
Modeling of spray flame in gas turbine combustors with LES and FGM
  • Jun 22, 2022
  • Fuel
  • Fanfu Kong + 4 more

Modeling of spray flame in gas turbine combustors with LES and FGM

  • Research Article
  • Cite Count Icon 78
  • 10.1080/13647830.2013.779388
A posteriori testing of algebraic flame surface density models for LES
  • Jun 1, 2013
  • Combustion Theory and Modelling
  • T Ma + 3 more

In the application of Large Eddy Simulation (LES) to premixed combustion, the unknown filtered chemical source term can be modelled by the generalised flame surface density (FSD) using algebraic models for the wrinkling factor Ξ. The present study compares the behaviour of the various models by first examining the effect of sub-grid turbulent velocity fluctuation on Ξ through a one-dimensional analysis and by the LES of the ORACLES burner (Nguyen, Bruel, and Reichstadt, Flow, Turbulence and Combustion Vol. 82 [2009], pp. 155–183) and the Volvo Rig (Sjunnesson, Nelsson, and Max, Laser Anemometry, Vol. 3 [1991], pp. 83–90; Sjunnesson, Henrikson, and Löfström, AIAA Journal, Vol. 28 [1992], pp. AIAA–92–3650). Several sensitivity studies on parameters such as the turbulent viscosity and the grid resolution are also carried out. A statistically 1-D analysis of turbulent flame propagation reveals that counter gradient transport of the progress variable needs to be accounted for to obtain a realistic flame thickness from the simulations using algebraic FSD based closure. The two burner setups are found to operate mainly within the wrinkling/corrugated flamelet regime based on the premixed combustion diagram for LES (Pitsch and Duchamp de Lageneste, Proceedings of the Combustion Institute, Vol. 29 [2002], pp. 2001–2008) and this suggests that the models are operating within their ideal range. The performance of the algebraic models are then assessed by comparing velocity statistics, followed by a detailed error analysis for the ORACLES burner. Four of the tested models were found to perform reasonably well against experiments, and one of these four further excels in being the most grid-independent. For the Volvo Rig, more focus is placed upon the comparison of temperature data and identifying changes in flame structure amongst the different models. It is found that the few models which largely over-predict velocities in the ORACLES case and volume averaged in a previous a priori DNS analysis (Chakraborty and Klein, Physics of Fluids, Vol. 20 [2008], p. 085108), deliver satisfactory agreement with experimental observations in the Volvo Rig, whereas a few of the other models are only able to capture the experimental data of the Volvo Rig either quantitatively or qualitatively.

  • Conference Article
  • Cite Count Icon 9
  • 10.2514/6.2015-3838
Understanding Scramjet Combustion using LES of the HyShot II Combustor: Stable Combustion and Incipient Thermal Choking
  • Jul 23, 2015
  • Kevin Nordin-Bates + 1 more

Unsteady combustion phenomena in scramjet combustors are challenging to understand and difficult to study computationally and experimentally. The most important unsteady phenomena are dual-mode ramjet/scramjet transition and onset of inlet unstart, of which the latter can be caused by either aerodynamic phenomena associated with the inlet flow itself or processes taking place in the combustor. Both these processes are complicated, and will typically involve situations in which the Mach number locally falls below unity, and the flow temporally becomes thermally choked. In this study we focus on deepening our knowledge about stable scramjet combustion and creating fundamental know-ledge about incipient unstart, primarily by means of thermal choking. For the purpose of this study we use the HyShot II model combustor, for which experimental data for both stable combustion and incipient thermal choking is available. The computational methods used consist of Large Eddy Simulation (LES) models and skeletal reaction mechanisms. The LES predictions are successfully validated against the experimental data and used to analyze the combined flow, mixing and combustion processes involved. The tools used include conventional as well as modern methods such as Takeno Flame Index and Chemical Explosive Model Analysis. These methods give a concise description of the flow, fuel-air mixing and combustion, identifies the factors contributing to the thermal choking and stabilization of the shock-system.

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  • Research Article
  • Cite Count Icon 2
  • 10.1063/5.0208228
Adaptive detached eddy simulation of turbulent combustion with the subgrid dissipation concept
  • May 1, 2024
  • Physics of Fluids
  • Haochen Liu + 2 more

Detached eddy simulation has become a widely used method in eddy simulations due to its balance between cost and accuracy. The recently developed subgrid dissipation concept (SDC) combustion model [Liu et al., “On the subgrid dissipation concept for large eddy simulation of turbulent combustion,” Combust. Flame 258, 113099 (2023)] is found to be more reasonable and accurate than the conventional eddy dissipation concept model in large eddy simulation (LES). In this paper, the SDC model is adapted to the ℓ2-ω adaptive detached eddy simulation framework, named DES-SDC. The required key quantities, including the fine structure mass fraction and dissipation rate, are appropriately blended across Reynolds-averaged Navier–Stokes and LES regions. The DES-SDC approach is validated using premixed bluff body stabilized flame, non-premixed swirl flame, and premixed swirl flame with complex geometry. It is much more tolerant to coarse mesh resolution than pure LES, yet it preserves the capability of resolving the key unsteady feature critical for the combustion process, as it is designed to be. The DES-SDC approach is relatively insensitive to the grid resolution. The present research provides a promising approach for accurately simulating practical unsteady turbulent combustion problems at an affordable computational cost.

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Present-day demands on combustion equipment are increasing the need for improved understanding and prediction of turbulent combustion. Large Eddy Simulation (LES), in which the large-scale flow is resolved on the grid, leaving only the small-scale flow to be modeled, provides a natural framework for combustion calculations as the transient nature of the flow is resolved. In most situations, however, the flame is thinner than the LES grid, and subgrid modeling is required to handle the turbulence-chemistry interaction. Here, we examine the predictive capabilities and the theoretical links between LES flamelet models, such as the G-equation model (G-LES), and LES finite rate chemistry models, such as the Thickened Flame Model (TFM-LES), the Partially Stirred Reactor model (PaSR-LES), the Eddy Dissipation Concept (EDC-LES) model, a Presumed Probability Density Function (PPDF-LES) model and the Implicit LES (QL-LES) model. The models are described, and theoretical links between these are discussed in terms of the turbulent flame speed and flame thickness. In addition, the different models are used to study a bluff-body stabilized flame and the resulting predictions are compared with experimental data for two operating conditions.

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Present-day demands on combustion equipment are increasing the need for improved understanding and prediction of turbulent combustion. Large eddy simulation (LES), in which the large-scale flow is resolved on the grid, leaving only the small-scale flow to be modeled, provides a natural framework for combustion simulations as the transient nature of the flow is resolved. In most situations; however, the flame is thinner than the LES grid, and subgrid modeling is required to handle the turbulence-chemistry interaction. Here we examine the predictive capabilities between LES flamelet models, such as the flamelet progress variable (LES-FPV) model, and LES finite rate chemistry models, such as the thickened flame model (LES-TFM), the eddy dissipation concept (LES-EDC) model, and the partially stirred reactor model (LES-PaSR). The different models are here used to examine a swirl-stabilized premixed flame in a laboratory gas turbine combustor, featuring the triple annular research swirler (TARS), for which high-quality experimental data is available. The comparisons include velocity and temperature profiles as well as combustor dynamics and NO formation.

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Application of modified eddy dissipation concept with large eddy simulation for numerical investigation of internal combustion engines
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Finite-rate combustion models for Large Eddy Simulation of non-premixed combustion; an a priori DNS analysis
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Turbulence and chemistry interaction (TCI) is still an open problem in the combustion science. Models are needed to account for the unclosed chemistry source terms when the averaged or filtered Navier-Stokes governing equations are solved for chemical species in reactive flows. Finite-rate (FR) combustion models attempting to model the low-pass filtered production/consumption rates (in the case of Large Eddy Simulation or LES) directly. The Eddy Dissipation Concept (EDC) and Scale Similarity (SS) models are two types of FR combustion models for LES. The aim of the study is to assess and improve the performance of the two mentioned models using Direct Numerical Simulation (DNS) databases. In DNS all flow and chemistry scales are resolved and no TCI modeling is required. The DNS databases of reactive flows with relatively detailed chemistry, which are now available thanks to massively large parallel computational tools and codes, can be utilized to both gain fundamental insights on the turbulent reactive flows and directly assess TCI models. The assessment can be through a priori and a posterior DNS analyses. In the current work, fundamental analyses are carried out, using DNS databases of non-premixed jet flames, on the spectral behavior (velocity and dissipation of kinetic energy spectra) and the internal intermittency phenomenon in this type of flames. The physical findings are applied to develop new FR combustion models for LES. In particular, Eddy Dissipation Concept (EDC) is improved by the modifications on the coefficients and the intermittency factor of the model. The modification on the coefficients follows a theoretical basis in which the new findings on spectral behavior have been applied to reduce the degree of freedom of the model by relating the two free coefficients of the model. On the other hand, the modification in the intermittency factor of EDC is the direct application of the observations in the scaling of dissipation fluctuations. The new EDC models are then a priori assessed using the DNS databases. Besides, the existing Scale Similarity (SS) models for LES are a priori assessed using the DNS databases and new dynamic SS models are developed based on Germano's identity for LES and further assessed using the a priori DNS analysis.

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Large Eddy Simulation of Turbulent Flow in a Marine Convective Boundary Layer with Snow
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Large-eddy simulation of wind flow and air pollutant transport inside urban street canyons of different aspect ratios
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of thesis entitled Large-Eddy Simulation of Wind Flow and Air Pollutant Transport inside Urban Street Canyons of Different Aspect Ratios submitted by Li, Xianxiang for the degree of Doctor of Philosophy at the University of Hong Kong in June 2008 The characteristics of the wind flow and air pollutant transport inside urban street canyons are of fundamental importance to the air quality monitoring and improvement. An investigation of these characteristics was performed in this study using both experimental and numerical techniques. The focus is on the mechanisms of pollutant transport and removal inside urban street canyons of high aspect ratios (AR, ratio of the building height to the street width). A physical model in water channel was first developed to study the wind flow in street canyons of different ARs of 0.5, 1.0, and 2.0. The velocity and turbulent fluctuation were measured by a Laser-Doppler Anemometer (LDA). The measured velocity and turbulent fluctuation at various locations were validated with several experimental datasets available in literature. The measured results in most locations were also in good agreement with previous numerical results. The comprehensive measurement data can provide a validation database for the numerical model development. To take into account the detailed transient turbulent processes, a large-eddy simulation (LES) model was developed based on a one-equation subgrid-scale (SGS) model and finite element method (FEM). This model was validated and fine-tuned by applying to an open channel flow at Reτ = 180. By comparing the calculated velocity and fluctuations with those obtained from experiment and direct numerical simulation (DNS), a set of model constants was determined for the LES model. A 1/7th wall model was further incorporated into this LES model to mitigate the strict near-wall resolution requirement. To validate the newly developed LES model for street canyons, the LES results for the street canyons of AR 1 and 2 were compared extensively with the waterchannel experimental data and previous LES results. The good agreement showed that the newly developed LES model was capable of predicting the complicated flow patterns and pollutant dispersion in street canyons. The validated LES model was then employed to simulate the street canyons of AR 3, 5, and 10. Three, five, and eight vertically aligned primary recirculations were found for the three cases, respectively, which showed decreasing strength with decreasing height. The very small ground-level wind speeds made the ground-level pollutants extremely difficult to disperse. Local maxima of the turbulence intensities were found at the interfaces between the primary recirculations and the free surface layer. The pollutant followed the trajectories of the primary recirculations. High pollutant concentration and variance were found near the buildings where wind flowed upward. Large gradients of pollutant concentration and variance were also observed at the interfaces between the primary recirculations and the free surface layer. Detailed analyses of concentration budget terms showed that the advection terms were responsible for pollutant redistribution within primary recirculations, while the turbulent transport terms were responsible for pollutant penetration between primary recirculations and pollutant removal from the street canyon. Based on the LES results, several quantities were introduced to compare the pollutant removal capability of different street canyon configurations. It was found that these quantities were all non-linear functions of the street canyon AR. Large-Eddy Simulation of Wind Flow and Air Pollutant Transport inside Urban Street Canyons of Different Aspect Ratios

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As part of the European Project on Cloud Systems in Climate Models, the diurnal cycle of stratocumulus has been simulated with Large‐Eddy Simulation (LES) models and Single Column Models (SCMs). The models were initialized and compared with observations collected in marine stratocumulus in July 1987 during the First International Satellite Cloud Climatology Project Regional Experiment. The results of the six LES models are found to be in a fair agreement with the observations. They all capture the distinct diurnal variation in the cloud liquid‐water path, the turbulence profiles and clearly show a decoupled boundary layer during daytime and a vertically well‐mixed boundary layer during the night. Entrainment of relatively dry and warm air from just above the inversion into the boundary layer is the major process modifying the thermodynamic structure of the boundary layer during the night. The differences that arise in the liquid‐water path evolution can therefore be attributed mainly to differences in the entrainment rate. The mean entrainment rates computed from the LES model results are 0.58±0.08 cm s−1 and 0.36±0.03 cm s−1 for the night‐time and daytime periods, respectively. If the horizontal domain size in a LES model is enlarged, mesoscale fluctuations develop. This leads to a broader liquid‐water path distribution and a reduction of the cloud albedo.To assess the quality of the representation of stratocumulus in general‐circulation models, results from ten SCMs are compared with observations and LES results. The SCM latent and sensible heat fluxes at the surface agree fairly well with the LES results. Many of the SCMs predict a liquid‐water path which is much too low, a cloud cover smaller than unity, and cloud tops that are lower than the observations and the LES results. This results in a much larger amount of downwelling short‐wave radiation absorbed at the sea surface. Improvement of entrainment parametrizations is needed for a better representation of stratocumulus in SCMs.Observations and LES results of entrainment rates for different stratocumulus cases are compared. The observed entrainment rates in Atlantic stratocumulus clouds during the Atlantic Stratocumulus Transition Experiment (ASTEX) are larger than for the ones over the Pacific Ocean off the coast of California. Results from LES models corroborate these findings. The differences in the entrainment rate can likely be attributed to the smaller inversion jumps of the liquid‐water potential temperature for the ASTEX stratocumulus cases. © Royal Meteorological Society, 2004. A. P. Lock's contribution is Crown copyright

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  • Atmosphere
  • Meng Li + 4 more

In this study, a hybrid large-eddy simulation (LES) model is developed and applied to simulate the transport of oil droplet aerosols in wind over progressive water waves. The LES model employs a hybrid spectral and finite difference method for simulating the wind turbulence and a bounded finite-volume method for modeling the oil aerosol transport. Using a wave-following coordinate system and computational grid, the LES model captures the turbulent flow and oil aerosol fields in the region adjacent to the unsteady wave surface. A flat-surface case with prescribed roughness (representing a pure wind-sea) and a wavy-surface case with regular plane progressive 100 m long waves (representing long-crest long-wavelength ocean swells) are considered to illustrate the capability of the LES model and study the effects of long progressive waves on the transport of oil droplet aerosols with four different droplet diameters. The simulation results and statistical analysis reveal enhanced suspension of oil droplets in wind turbulence due to strong disturbance from the long progressive waves. The spatial distribution of the aerosol concentration also exhibits considerable streamwise variations that correlate with the phase of the long progressive waves.

  • Research Article
  • Cite Count Icon 37
  • 10.1016/j.ijhydene.2008.05.071
LES model of large scale hydrogen–air planar detonations: Verification by the ZND theory
  • Aug 29, 2008
  • International Journal of Hydrogen Energy
  • M Zbikowski + 2 more

LES model of large scale hydrogen–air planar detonations: Verification by the ZND theory

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