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Published in 2020 at "AIAA Journal"
DOI: 10.2514/1.j058312
Abstract: The effects of inert diluents in the fuel mixture of a model swirl stabilized gas turbine combustor, under thermoacoustically unstable limit cycle operation, were studied experimentally. The measur...
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Keywords:
fuel diluents;
effects inert;
inert fuel;
gas turbine ... See more keywords