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Ignition and Flame Stabilization of a Strut-Jet RBCC Combustor with Small Rocket Exhaust
A Rocket Based Combined Cycle combustor model is tested at a ground direct connected rig to investigate the flame holding characteristics with a small rocket exhaust using liquid kerosene. The total temperature and the Mach number of the vitiated air flow, at exit of the nozzle are 1505 K and 2.6, r...
| Autores principales: | , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
Hindawi Publishing Corporation
2014
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| Materias: | |
| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC3918380/ https://www.ncbi.nlm.nih.gov/pubmed/24578655 http://dx.doi.org/10.1155/2014/675498 |