The Effect of Fuel Injection Location on Supersonic Hydrogen Combustion in a Cavity-Based Model Scramjet Combustor

Supersonic combustion experiments were performed using three different hydrogen fuel-injection configurations in a cavity-based model scramjet combustor with various global fuel−air equivalence ratios. The configurations tested were angled injection at 15° to the flow direction up...

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Main Authors: Eunju Jeong, Sean O’Byrne, In-Seuck Jeung, A. F. P. Houwing
Formato: Artigo
Idioma:Inglês
Publicado em: MDPI AG 2020-01-01
Colecção:Energies
Assuntos:
supersonic combustion
scramjet combustor
cavity-based combustion
hydrogen combustion
Acesso em linha:https://www.mdpi.com/1996-1073/13/1/193
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