Abstract

Turbulent piloted Bunsen flames of stoichiometric methane–air mixtures are computed using the large eddy simulation (LES) paradigm involving an algebraic closure for the filtered reaction rate. This closure involves the filtered scalar dissipation rate of a reaction progress variable. The model for this dissipation rate involves a parameter βc representing the flame front curvature effects induced by turbulence, chemical reactions, molecular dissipation, and their interactions at the sub-grid level, suggesting that this parameter may vary with filter width or be a scale-dependent. Thus, it would be ideal to evaluate this parameter dynamically by LES. A procedure for this evaluation is discussed and assessed using direct numerical simulation (DNS) data and LES calculations. The probability density functions of βc obtained from the DNS and LES calculations are very similar when the turbulent Reynolds number is sufficiently large and when the filter width normalised by the laminar flame thermal thickness is larger than unity. Results obtained using a constant (static) value for this parameter are also used for comparative evaluation. Detailed discussion presented in this paper suggests that the dynamic procedure works well and physical insights and reasonings are provided to explain the observed behaviour.

Highlights

  • Detailed discussion presented in this paper suggests that the dynamic procedure works well and physical insights and reasonings are provided to explain the observed behaviour

  • High efficiency and low emission can be achieved simultaneously for power plants used in transport sectors, gas turbines, using lean turbulent premixed combustion

  • One needs robust and reliable combustion sub-modelling to achieve this, and the large eddy simulation (LES) paradigm may be more suited than the Reynolds averaged Navier–Stokes (RANS) approach to studying the above unsteady phenomenon

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Summary

Introduction

High efficiency and low emission can be achieved simultaneously for power plants used in transport sectors, gas turbines, using lean turbulent premixed combustion. The dynamics of large-scale turbulent eddies down to a cut-off scale are solved with models to represent the influences of unresolved small (known as sub-grid) scales in a typical LES [1,2] employing a numerical grid adequate to resolve the dynamic scales containing at least 80% of the turbulence energy [1]. This method is seen to be a higher

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