Study on the Flow Mixing and Oblique-Detonation Ignition Characteristics of RP-3 Aviation Kerosene in a Constrained Supersonic Flow Channel
Oblique detonation engines have been proposed for hypersonic propulsion because detonation-based heat addition can, in principle, provide rapid energy release with reduced total-pressure penalties. We investigate non-premixed injection/mixing of an RP-3 aviation-kerosene surrogate in a constrained s...
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| Principais autores: | , , , , , |
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| Format: | Artigo |
| Jezik: | Inglês |
| Izdano: |
MDPI AG
2026-05-01
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| Serija: | Aerospace |
| Teme: | |
| Online dostop: | https://www.mdpi.com/2226-4310/13/6/489 |
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