Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines

Published 2020 View Full Article

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Title
Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines
Authors
Keywords
Liquid propellant rocket engine, Combustion instability, Injector coupling, Damping device
Journal
ACTA ASTRONAUTICA
Volume 169, Issue -, Pages 170-179
Publisher
Elsevier BV
Online
2020-01-15
DOI
10.1016/j.actaastro.2019.11.040

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