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Orifice Flow Dynamics in a Rocket Injector as an Excitation Source of Injector-Driven Combustion Instabilities

To investigate a hypothesis of the orifice flow-induced instability in rocket engine thrust chambers, a single liquid oxygen (LOX) injector with an optically accessible orifice module was used for experiments, with water as a simulant for LOX. The unsteady pressure downstream of the orifice was meas...

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Principais autores: Min Son, Michael Börner, Wolfgang Armbruster, Justin S. Hardi
Format: Artigo
Sprog:Inglês
Udgivet: MDPI AG 2023-05-01
Serier:Aerospace
Fag:
combustion instability
rocket injector
flow visualization
cavitation
whistling
Online adgang:https://www.mdpi.com/2226-4310/10/5/452
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