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Investigation of the influence of extinction strain rates and heat release rate on the stability of swirl stabilised hydrogen premixed flames

Reference Number
EP/Y017951/1
Title
Investigation of the influence of extinction strain rates and heat release rate on the stability of swirl stabilised hydrogen premixed flames
Status
Started
Energy Categories
Hydrogen and Fuel Cells(Hydrogen, Hydrogen end uses (incl. combustion; excl. fuel cells))
Research Types
Basic and strategic applied research
Science and Technology Fields
PHYSICAL SCIENCES AND MATHEMATICS (Applied Mathematics)
PHYSICAL SCIENCES AND MATHEMATICS (Computer Science and Informatics)
ENGINEERING AND TECHNOLOGY (Mechanical, Aeronautical and Manufacturing Engineering)
UKERC Cross Cutting Characterisation
Not Cross-cutting
Principal Investigator
Dr U Ahmed
Sch of Engineering
Newcastle University
Award Type
Standard
Funding Source
EPSRC
Start Date
01 December 2024
End Date
30 November 2027
Duration
36 months
Total Grant Value
£385,259
Industrial Sectors
Chem. React. Dyn. & mechanisms
Region
North East
Programme
NC : Engineering
Investigators
Principal Investigator
Dr U Ahmed, Sch of Engineering, Newcastle University
Industrial Collaborator
Project Contact, Rolls-Royce PLC
Project Contact, Renuda UK
Project Contact, Kyoto University (Kyodai), Japan
Web Site
Objectives
Abstract
With the need for the development of novel hydrogen-compatible combustion devices, physical understanding of the flame behaviour and the identification of thermoacoustic instabilities at relevant combustor operating conditions for hydrogen-air swirl flames will help speed up the development of hydrogen combustors, in line with the UK government's net-zero vision. The proposed research will offer potential benefits to industry and contribute to the progress of science in the areas of fluid dynamics, turbulence and net-zero combustion. These include (i) An advanced Direct Numerical Simulation (DNS) database for hydrogen-air premixed swirl flames under representative combustor operating conditions. (ii) A comprehensive understanding and a detailed analysis of the behaviour of the Precessing Vortex Core (PVC) under non-reacting and reacting flow conditions. (iii) Identification of the combustor operating conditions for which hydrodynamic/thermoacoustic instabilities exist. (iv) An in-depth analysis on extinction strain rates and heat release rate for lean hydrogen premixed flames. The outcomes of this project will offer knowledge on the flame stability limits and will contribute to the development of hydrogen based power generation and propulsion devices (e.g. gas turbines used for power generation and aircraft engines).
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Added to Database
03/07/24