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...

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Detalles Bibliográficos
Autores principales: Hu, Jichao, Chang, Juntao, Bao, Wen
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Hindawi Publishing Corporation 2014
Materias:
Research Article
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

Internet

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

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