Influence of Fuel Injection Location in a Small Radial Swirler Low NOₓ Combustor for Micro Gas Turbine Applications

Andrews, GE orcid.org/0000-0002-8398-1363 and Kim, S (2019) Influence of Fuel Injection Location in a Small Radial Swirler Low NOₓ Combustor for Micro Gas Turbine Applications. In: Proceedings of the ASME TurboExpo 2019 Volume 4A: Combustion, Fuels, and Emissions. ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, 17-21 Jun 2019, Phoenix, Arizona, USA. American Society of Mechanical Engineers . ISBN 9780791858615

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Copyright, Publisher and Additional Information: © 2019 ASME. This is an author produced version of a conference paper published in ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition. Uploaded with permission from the publisher.
Keywords: Combustion chambers, Fuels, Micro gas turbines, Nitrogen oxides, Emissions, Natural gas, Turbines, Atmospheric pressure, Combustion, Fuel injectors, Oxygen, Temperature
Dates:
  • Published: 17 June 2019
  • Accepted: 18 March 2019
  • Published (online): 5 November 2019
Institution: The University of Leeds
Academic Units: The University of Leeds > Faculty of Engineering (Leeds) > School of Chemical & Process Engineering (Leeds)
Depositing User: Symplectic Publications
Date Deposited: 15 May 2020 16:28
Last Modified: 19 May 2020 04:52
Status: Published
Publisher: American Society of Mechanical Engineers
Identification Number: https://doi.org/10.1115/gt2019-90197

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