Simulation of a GOx-GCH4 Rocket Combustor and the Effect of the GEKO Turbulence Model Coefficients

In this study, a single injector methane-oxygen rocket combustor is numerically studied. The simulations included in this study are based on the hardware and experimental data from the Technical University of Munich. The focus is on the recently developed generalized <i>k–ω</i> turbulenc...

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Autores principales: Evgeny Strokach, Victor Zhukov, Igor Borovik, Andrej Sternin, Oscar J. Haidn
Formato: article
Lenguaje:EN
Publicado: MDPI AG 2021
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Acceso en línea:https://doaj.org/article/9e1c94f5edcb4b8b945cb7683e7eec6f
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