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This article has been cited by the following article(s):
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Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Injector-Driven Flame Dynamics in a High-Pressure Multi-Element Oxygen–Hydrogen Rocket Thrust Chamber
Wolfgang Armbruster, Justin S. Hardi, Dmitry Suslov and Michael Oschwald Journal of Propulsion and Power 35(3) 632 (2019) https://doi.org/10.2514/1.B37406