Experimental data-based reduced-order model for analysis and prediction of flame transition in gas turbine combustors
Author:
Affiliation:
1. Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI, USA
2. Institute for Aerospace Studies, University of Toronto, Toronto, ON, Canada
Funder
Air Force Office of Scientific Research
Publisher
Informa UK Limited
Subject
General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,Modeling and Simulation,General Chemical Engineering,General Chemistry
Link
https://www.tandfonline.com/doi/pdf/10.1080/13647830.2019.1602286
Reference28 articles.
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5. Dynamics of lean blowout of a swirl-stabilized flame in a gas turbine model combustor
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