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Fuel Sensitivity of Lean Blowout in a RQL Gas Turbine CombustorTransition from fossil fuels to synthetic drop-in fuels without the need to change existing combustors is the current research topic. The combustor performances such as cold-day ignition limits, lean blow-out (LBO) limits and altitude relight limits are the main focus points. The objective of this work is to evaluate the effect of different fuel candidates on the operability of gas turbines by comparing a conventional petroleum-based fuel with one other alternative fuel candidate. Time filtered Navier-Stokes simulations (TFNS) and K-LES are performed to examine the performance of these fuels at the stable conditions close to blow-out in a referee combustor rig.
Document ID
20190032081
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Wey, C. Thomas
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
October 15, 2019
Publication Date
August 19, 2019
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN72312
Meeting Information
Meeting: AIAA Propulsion and Energy Forum 2019
Location: Indianapolis, IN
Country: United States
Start Date: August 19, 2019
End Date: August 22, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 109492.02.03.01.20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
referee rig
Fuel sensitivity
Lean blow-out
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