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Development of scalar dissipation rate based reaction rate models for the large eddy simulations of premixed flames

Reference Number
EP/I027556/1
Title
Development of scalar dissipation rate based reaction rate models for the large eddy simulations of premixed flames
Status
Completed
Energy Categories
Energy Efficiency(Transport)
Fossil Fuels: Oil Gas and Coal(Oil and Gas, Oil and gas combustion)
Research Types
Basic and strategic applied research
Science and Technology Fields
ENGINEERING AND TECHNOLOGY (Mechanical, Aeronautical and Manufacturing Engineering)
UKERC Cross Cutting Characterisation
Not Cross-cutting
Principal Investigator
Dr N Swaminathan
Engineering
University of Cambridge
Award Type
Standard
Funding Source
EPSRC
Start Date
01 January 2012
End Date
30 October 2015
Duration
46 months
Total Grant Value
£156,288
Industrial Sectors
Mechanical engineering
Region
East of England
Programme
Energy : Engineering
Investigators
Principal Investigator
Dr N Swaminathan, Engineering, University of Cambridge
Industrial Collaborator
Project Contact, Rolls-Royce PLC
Project Contact, Siemens Industrial Turbomachinery
Web Site
Objectives
Abstract
This project aims to develop an efficient Scalar Dissipation Rate (SDR) based reaction rate closure for the Large Eddy Simulation (LES) of turbulent premixed flames. Although SDR based closures are well established for Reynolds Averaged Navier Stokes (RANS) simulations of non-premixed flames, they are rare for RANS and LES of turbulent premixed flames, and no detailed evaluation of their performance in LES is available so far. In this project, the SDR based reaction rate closures will be developed and simultaneously assessed by a-priori analyses of explicitly filtered Direct Numerical Simulation (DNS) data, and a-posteriori evaluations of model performances in LES calculations, in a configuration for which experimental data is available. Based on the simultaneous a-priori and a-posteriori analyses, new models will be developed and their performance will subsequently be assessed. The best models will then be implemented in a LES code for turbulent premixed flame modelling. An efficient SDR-based reaction rate closure will provide a robust CFD based design tool for reliable, cleaner and cost-effective combustion devices operating in lean premixed mode (e.g. Spark Ignition engines, Lean Premixed Pre-vaporised (LPP) industrial gas turbine combustors)
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Added to Database
06/02/12