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Reference Number EP/G008841/1
Title Development of Unified Flame Surface Density Based Reaction Rate Models for the LES of Turbulent Premixed Flames
Status Completed
Energy Categories Not Energy Related 50%;
Other Power and Storage Technologies(Electric power conversion) 25%;
Energy Efficiency(Industry) 25%;
Research Types Basic and strategic applied research 100%
Science and Technology Fields ENGINEERING AND TECHNOLOGY (Mechanical, Aeronautical and Manufacturing Engineering) 100%
UKERC Cross Cutting Characterisation Not Cross-cutting 100%
Principal Investigator Professor N (Nilanjan ) Chakraborty
No email address given
Mechanical and Systems Engineering
Newcastle University
Award Type Standard
Funding Source EPSRC
Start Date 01 August 2009
End Date 31 January 2013
Duration 42 months
Total Grant Value £137,051
Industrial Sectors No relevance to Underpinning Sectors
Region North East
Programme Materials, Mechanical and Medical Engineering
 
Investigators Principal Investigator Professor N (Nilanjan ) Chakraborty , Mechanical and Systems Engineering, Newcastle University (100.000%)
Web Site
Objectives Linked to grant EP/G009783/1
Abstract We aim to develop an efficient Flame Surface Density (FSD) based reaction rate closure for the Large Eddy Simulation (LES) of turbulent premixed flames. Although FSD closures are well established for Reynolds Averaged Navier Stokes (RANS) simulations, they are relatively rare for LES, and no detailed evaluation of their performance is available so far. In this project, FSD 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 actual LES results, in a configuration for which experimental data is available. Based on the simultaneous a-priori and a-posteriori analyses, new unified models will be developed and their performance will then be assessed by the same analysis as carried out for the existing models. The model implementation will then be generalised in such a format that they can be used as an "add-on" to any commercial or inhouse general purpose code involving complex geometrical configurations. The new subroutines where this will be implemented will be made freely available to interested national and international colleagues. An efficient FSD-based reaction rate closure will provide a reliable CFD based design tool for reliable, cleaner and cost-effective combustion devices where combustion takes place in premixed mode (e.g. Spark Ignition engines, Lean Premixed Pre-vaporised (LPP) and industrial gas turbine combustors.
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Added to Database 22/08/08