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Improved simulation of cryogenic fluid mixing at supercritical pressures
The combustion chamber pressure of rockets, gas turbines and diesel engines is known to be above the critical pressure of fuel and oxidizers. In the case of rocket engines the fuel and/or oxidizer is often injected at cryogenic temperatures. This elevated combustion chamber pressure and low temperat...
| Autores principales: | , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
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Public Library of Science
2023
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| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9851497/ https://www.ncbi.nlm.nih.gov/pubmed/36656839 http://dx.doi.org/10.1371/journal.pone.0277711 |