Numerical analysis of LOx-BioLPG combustion in high-pressure liquid rocket engine propulsion system
The present work numerically investigates the steady state LOx-BioLPG combustion in a high-pressure liquid rocket engine propulsion system, based on the RANS approach using Eulerian single-phase thermo-chemical modeling with Peng-Robinson equation of state. The study primarily focuses on the less ca...
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| Autori principali: | , , |
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| Natura: | Artigo |
| Lingua: | Inglês |
| Pubblicazione: |
Elsevier
2023-07-01
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| Serie: | South African Journal of Chemical Engineering |
| Soggetti: | |
| Accesso online: | http://www.sciencedirect.com/science/article/pii/S1026918523000379 |
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