Comparison of Dual-Combustion Ramjet and Scramjet Performances Considering Combustion Efficiency
The performances of a dual-combustion ramjet (DCR) and a scramjet were compared via computational fluid dynamics numerical simulation to provide theoretical guidance for engine selection for a hypersonic vehicle. Kerosene, C<sub>12</sub>H<sub>23</sub>, with an equivalence ratio of 0.8, was employed...
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| Autors principals: | , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
MDPI AG
2022-12-01
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| Col·lecció: | Applied Sciences |
| Matèries: | |
| Accés en línia: | https://www.mdpi.com/2076-3417/13/1/480 |
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