Comprehensive analysis of tubular combustion chambers in Turbo-Ramjet engines for enhanced hypersonic propulsion
Anticipating a doubling in global air travel demand by 2040, the present work underscores the need for innovation in aviation propulsion systems. This study presents the design and analysis of tubular combustors for lower Mach numbers in Turbo-Ramjet engines, utilizing input parameters derived from...
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| Principais autores: | , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
KeAi Communications Co. Ltd.
2025-06-01
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| coleção: | FirePhysChem |
| Assuntos: | |
| Acesso em linha: | http://www.sciencedirect.com/science/article/pii/S2667134424000828 |
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