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Published in 2021 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2021.106517
Abstract: Abstract The effect of inlet boundaries on combustion instabilities in a spray combustor is investigated experimentally in this paper. The combustor is operated at pressure-elevated conditions and fueled with aviation kerosene. Three different inlet conditions,…
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Keywords:
pressure elevated;
inlet boundaries;
effect inlet;
inlet ... See more keywords