Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber

Published 2020 View Full Article

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Title
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Authors
Keywords
Combustion instabilities, Liquid propellant rocket engines, Flame visualization, Transcritical injection
Journal
PROCEEDINGS OF THE COMBUSTION INSTITUTE
Volume -, Issue -, Pages -
Publisher
Elsevier BV
Online
2020-07-11
DOI
10.1016/j.proci.2020.05.020

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