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Cited article:

Modeling of H₂/O₂ single-element rocket thrust chamber combustion at sub- and supercritical pressures with different computational fluid dynamics tools

H. Riedmann, D. Banuti, B. Ivancic, O. Knab, K. Hannemann

Published online: 2019-02-08

DOI: https://doi.org/10.1051/eucass/201911247

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