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Published in 2020 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2020.106187
Abstract: Abstract To study the influence of injector geometrical parameters on combustor flow fields, detailed numerical and experimental investigations of a single-element injector with gaseous hydrogen and gaseous oxygen (GH2/GO2) propellants were performed at atmospheric pressure.…
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Keywords:
experimental investigations;
numerical experimental;
flow;
gh2 go2 ... See more keywords