Experimental study on effects of nozzles and combustors on the rotating detonation rocket engine in pulse operation
The rotating detonation engine (RDE) is an innovative pressure-gain combustion device that harnesses detonation waves for efficient fuel combustion. This paper examines the impact of various nozzle and combustor configurations on the operating characteristics of a rotating detonation rocket engine (...
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| Autors principals: | , , , , , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
Elsevier
2025-09-01
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| Col·lecció: | Results in Engineering |
| Matèries: | |
| Accés en línia: | http://www.sciencedirect.com/science/article/pii/S2590123025020468 |
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