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...
Kaydedildi:
| Asıl Yazarlar: | , , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
Elsevier
2023-07-01
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| Seri Bilgileri: | South African Journal of Chemical Engineering |
| Konular: | |
| Online Erişim: | http://www.sciencedirect.com/science/article/pii/S1026918523000379 |
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