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

Lead Research Organisation: University of Cambridge
Department Name: Engineering

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).

Planned Impact

The major impacts of this project can be summarised as follows: (i) Development of a high-fidelity alternative scalar dissipation rate (SDR) based LES modelling of turbulent premixed flames: The project outcomes will be disseminated through participation in international conferences (e.g. International Combustion Symposium, European Combustion Meeting, Society of Automotive Engineers meeting, ASME Gas Turbine meetings) and publication in scientific journals (e.g. Combustion and Flame, Physics of Fluids etc.). The DNS database resulting from the project will be made available to other interested researchers upon request. The project-students will manage a website for data-exchange and documentation, and specific results will be made available for public download. A one-day workshop on SDR based premixed combustion modelling for LES at CUED at the end of the project to maximise the chances of technical dissemination and to attract attentions of relevant industrial sectors. (ii) IC-engine and gas turbine users and manufacturers: Improving the prediction abilities of models for turbulent premixed combustion will be of great benefit to the aforementioned industries for the development of new generation energy-efficient and environment friendly combustors. The supporting letters attached with the Case for Support indicate that Ford, ESR network, Rolls-Royce in the UK will be interested in the outcome of this work. The industrial colleagues will be invited to attend half-yearly progress meetings and the planned workshop at the end of this project so that they remain aware of the project development and their feedback is taken on board during the course of the project. In interactive website will be maintained throughout the project with information on data-exchange, documentation, and specific results will be made available for public download along with the latest findings in the open literature. It will therefore serve as an important source of information for combustion modellers both in academia and industry. (iii)PhD students who will be engaged in this project: The PhD students will receive significant training on a variety of topics (DNS, LES, reduced chemistry, combustion model development). In the project, both students will learn advanced computational techniques for simulation (LES, DNS) and improve their analytical and mathematical skills. It is hoped that the experience of presenting their research in the form of peer-reviewed papers and conference presentations will make them a well-rounded researcher during the course of this project. Moreover, the PhD students need to present their work periodically in project review meetings and maintain the project website, which will also be beneficial for them in terms of developing project management and presentation skills. They will also have opportunities to interact with the academic and industrial contacts of the PIs, which will help their academic development, and also help them to develop a range of transferable skills such as communication, teamwork and project management. This, in turn, will give an edge to the students in current competitive job markets. (iv) Research groups of UL and CUED: The collaboration between UL and CUED is one of the major strengths of this project which will lead to broadening of research capabilities of both the PIs. Moreover it is expected that this project will certainly give rise to open questions which form the basis of further investigations by the PIs, and the usefulness of the present project will be exploited to attract industrial and research grant funding for its future follow-ups. It is likely that the understanding gained from this project will subsequently be applied to engineering combustion applications, possibly through the Knowledge Transfer Partnership (KTP) scheme in collaboration with industry in future, which will also ensure effective assimilation of this project's outcome in the relevant industrial sectors.
 
Description A simple yet robust modelling framework for LES of premixed combustion is developed, tested and validated for gas turbine combustion application. The key finding is that the flame straining caused by turbulent eddies are captured inherently in LES framework and no further complication to simple unstrained flamelet modelling may not be required.
Exploitation Route The models developed and tested in this project for high fidelity simulations of combusting flows in engines are computationally economical and thus they can be used in the design and development programme of next generation engines. This can be realised by implementing these models in the inhouse CFD codes used by relevant industries. Indeed, the LES model and its framework developed in this project is transferred to Siemens Industrial Turbomachinary for their internal use. These models are also implemented in an in-house CFD code of Rolls Royce and are used by them for their analyses.
Sectors Aerospace, Defence and Marine,Energy,Transport

 
Description The student spent about 3 months at Siemens, Lincoln and Finspong Sweden, to implement the modelling framework and for knowledge transfer. This has been demonstrated successfully and there is a joint paper published at DOI: 10.2514/1.B36842
Sector Aerospace, Defence and Marine,Energy,Transport
Impact Types Societal,Economic

 
Description AMEL
Amount £372,345 (GBP)
Organisation European Commission H2020 
Sector Public
Country Belgium
Start 11/2014 
End 03/2016
 
Description CORNET - Core Noise Engine Technology
Amount € 997,772 (EUR)
Funding ID CORNET 
Organisation European Commission 
Sector Public
Country European Union (EU)
Start 03/2016 
End 03/2018
 
Description Flame Blow-off simulation using SDR model
Amount £30,000 (GBP)
Organisation Rolls Royce Group Plc 
Sector Private
Country United Kingdom
Start 10/2015 
End 09/2018
 
Description LES of circumferential instability in cannular combustor
Amount £369,018 (GBP)
Organisation Mitsubishi Heavy Industries 
Sector Private
Country Japan
Start 11/2016 
End 10/2019
 
Description MHI-Emission
Amount £374,169 (GBP)
Organisation Mitsubishi Heavy Industries 
Sector Private
Country Japan
Start 11/2019 
End 10/2021
 
Description MHI-Fellowship
Amount £244,139 (GBP)
Organisation Mitsubishi Heavy Industries 
Sector Private
Country Japan
Start 11/2019 
End 10/2022
 
Description MHI-FlaRe
Amount £200,893 (GBP)
Organisation Mitsubishi Heavy Industries 
Sector Private
Country Japan
Start 11/2019 
End 10/2022
 
Description Siemens funding
Amount £30,000 (GBP)
Funding ID RG68971 
Organisation Siemens AG 
Department Siemens Industrial Turbomachinery Ltd
Sector Private
Country United Kingdom
Start 01/2012 
End 12/2015
 
Title computer code for the models 
Description Computer codes developed in this project can be used with commercial CFD codes to capture turbulent combustion physics robustly and accurately. Thus, this code can be used as a predictive tool as it involves 'no' tunable parameters. Using this, one can study fuel burn rate, pollutant formation, etc. and how they variation in space and time in gas turbine and automobile engines. 
Type Of Material Technology assay or reagent 
Year Produced 2017 
Provided To Others? Yes  
Impact Quicker solutions, which are dependable and trustworthy, considerable saving of computational efforts required for gas turbine combustion simulations. The computational time can be reduced from many months to few weeks. 
 
Title LES data 
Description A collection of numerical data sets generated in this project for various turbulent flame configurations using a single modelling framework and a set of model parameters 
Type Of Material Database/Collection of data 
Provided To Others? No  
Impact A practical and robust model resulted from this project which can be used in gas turbine and automotive engine simulations to research and develop "greener" engines for future transport sector. 
 
Title LES model 
Description A robust, accurate and simple modelling framework for large eddy simulation of fuel-lean premixed combustion 
Type Of Material Computer model/algorithm 
Provided To Others? No  
Impact Accurate predictions of gas turbine combustion and flames in various configurations. Already implemented in computer codes used by RollsRoyce, Siemens. 
 
Description Lund 
Organisation Lund University
Country Sweden 
Sector Academic/University 
PI Contribution mutual research exchange visits
Collaborator Contribution mutual research exchange visits
Impact Two papers published in high quality journal
Start Year 2017
 
Description MHI - Collaborations 
Organisation Mitsubishi Heavy Industries
Country Japan 
Sector Private 
PI Contribution Development of computer models for gas turbine combustion simulations
Collaborator Contribution direct funding, sending their employee to work with us in our lab, mutual exchange of knowledge
Impact This collaboration started only few months ago and this is not a multi-disciplinary yet.
Start Year 2019
 
Description Research Collaboration with TokyoTech 
Organisation Tokyo Institute of Technology
Department Furui-Lab
Country Japan 
Sector Academic/University 
PI Contribution Because of the initial collaboration with Tokyo Tech through this project, the PI has been invited to collaborate with TokyoTech on a number of research and educational projects. The PI has been invited to be a co-investigator on two research projects (2010-13, 2011-15) on turbulent combustion with a combined total value of about £2.7M, awarded to Tokyo Tech by JSPS and MEXT. The PI has been invited to be an international co-operative partner in their 6 year educational programme with a value of about £25M awarded to Tokyo Tech by MEXT. The initial interaction through this project has evolved into a strong and successful collaboration.
Collaborator Contribution The partner allowed us to use their numerical simulation data to get insights required for model development in this project
Impact the papers resulted from this collaboration are listed in the publication list.
Start Year 2006
 
Description Sandia-RB 
Organisation Sandia Laboratories
Country United States 
Sector Private 
PI Contribution computations of their experimental burners and comparisons of computational and experimental results
Collaborator Contribution providing the experimental data from laser diagnostics
Impact a paper is published in Combustion and Flame journal
Start Year 2018
 
Description Siemens collaborations 
Organisation Siemens AG
Department Siemens Industrial Turbomachinery Ltd
Country United Kingdom 
Sector Private 
PI Contribution Turbulent Combustion model development for their in-house use
Collaborator Contribution Direct financial contribution, exchange of complementary knowledge, exposure to practical issues and operations of gas turbines
Impact a joint paper on large eddy simulation of gas turbine combustor, published in Journal of Propulsion and Power in 2018 - listed in publication section. The models developed and implemented in their in-house code has significantly reduced the simulations times so the performance benefits of geometry change can be evaluated quickly leading to economic benefits to Siemens. Better combustor design leads to reduced emissions resulting in societal/environmental benefits.
Start Year 2012
 
Description KAUST invited talk 
Form Of Engagement Activity A talk or presentation
Part Of Official Scheme? No
Geographic Reach National
Primary Audience Postgraduate students
Results and Impact Invited talk. Research collaborations are emerging.
Year(s) Of Engagement Activity 2014
 
Description NORDITA Workshop (Stockholm) 
Form Of Engagement Activity A formal working group, expert panel or dialogue
Part Of Official Scheme? No
Geographic Reach International
Primary Audience Professional Practitioners
Results and Impact A month long workshop co-organised by the PI - to disseminate the models developed in this EPSRC project.
There were formal talks given by the PI, led to research collaborations.
Year(s) Of Engagement Activity 2016
 
Description Talk at Georgia Tech, USA 
Form Of Engagement Activity A talk or presentation
Part Of Official Scheme? No
Geographic Reach International
Primary Audience Postgraduate students
Results and Impact 25 to 30 people attended this talk and have lively dialogues (Q&A) and exchanges of knowledge. Few of them noted that they are going to try the approach described in the presentation, which resulted from this project.
Year(s) Of Engagement Activity 2018
 
Description Talk at Solar Turbines, San Diego, CA, USA 
Form Of Engagement Activity A talk or presentation
Part Of Official Scheme? No
Geographic Reach Regional
Primary Audience Professional Practitioners
Results and Impact Excellent interaction and discussion with the audience - expressed interests to try the methodology and tool in their gas turbine combustor design.
Year(s) Of Engagement Activity 2018