Analysis of combustion modes in a cavity based scramjet

Large eddy simulations (LES) of non reactive and reactive flows in a cavity-based scramjet combustor configuration from the U.S Air Force Research Laboratory (AFRL) are performed. These simulations feature a 22 species and 206 reactions chemical scheme for ethylene/air. The ability of LES to reprodu...

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Veröffentlicht in:	Combustion and flame 2020-05, Vol.215, p.238-251
Hauptverfasser:	Ruan, Jiangheng L., Domingo, Pascale, Ribert, Guillaume
Format:	Artikel
Sprache:	eng
Schlagworte:	Chemical reactions Combustion chambers Combustion regimes Computer simulation Diffusion layers Engineering Sciences Finite element method Flame Stabilisation High temperature Large Eddy Simulation Micrometers Reactive fluid environment Residence time Simulation Supersonic combustion ramjet engines Turbulent supersonic combustion Velocity distribution
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