Investigation of mixing and initiation characteristics of oblique detonation engine in confined spaces
The oblique detonation engine (ODE) is a novel air-breathing propulsion system capable of meeting the requirements of hypersonic flight at Mach numbers above 8. In a confined hypersonic flow channel, fuel must achieve mixing within extremely short time and distance constraints to enable reliable ini...
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| Автори: | , , , , , , |
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| Формат: | Artigo |
| Мова: | Inglês |
| Опубліковано: |
Elsevier
2026-05-01
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| Серія: | Case Studies in Thermal Engineering |
| Предмети: | |
| Онлайн доступ: | http://www.sciencedirect.com/science/article/pii/S2214157X26003680 |
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