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Published in 2019 at "Flow, Turbulence and Combustion"
DOI: 10.1007/s10494-018-9999-y
Abstract: This paper presents experimental investigations in an effusion cooled single sector gas turbine combustor under close-to-reality boundary conditions, i.e. elevated pressure and combustor inlet temperature, under varying staging conditions. Flow field, flame structure and gas-phase…
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Keywords:
gas;
cooled single;
effusion cooled;
combustor ... See more keywords