Finite rate chemistry large-eddy simulation of self-ignition in a supersonic combustion ramjet

AIAA Journal

Volumn 48, Issue 3, 2010, Pages 540-550

  Berglund, M ^a,c,d   Fedina, E ^a,e   Fureby, C ^a,e   Tegner J ^a,e   Sabel'nikov, V ^b,f  

^a SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

^b ONERA   (France)

^c Defense Security Systems Technology   (United States)

^d Scania CVAB   (Sweden)

^e Grindsjön Research Center   (Sweden)

^f Chemin de la Huniére   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AIR HEATER; CENTERLINES; COMBUSTION CHEMISTRY; COMBUSTION PHYSICS; COMPLICATED FLOW; CROSS SECTION; EXPERIMENTAL DATA; FINITE VOLUME; FINITE-RATE CHEMISTRY; FLAME STABILIZATION; FUEL INJECTORS; ION RADICALS; LARGE-EDDY SIMULATION MODELS; NATIONAL AEROSPACE LABORATORIES; PLANAR LASER INDUCED FLUORESCENCE; QUANTITATIVE AGREEMENT; REACTION MECHANISM; SELF IGNITION; STIRRED REACTORS; STRUT INJECTORS; SUBGRID MODEL; SUPERSONIC COMBUSTION; SUPERSONIC COMBUSTORS; SUPPLEMENTARY INFORMATION; TURBULENCE-CHEMISTRY INTERACTIONS; TWO STAGE; TWO-STAGE INJECTOR; WALL-PRESSURE DISTRIBUTION;

ATMOSPHERIC BOUNDARY LAYER; FLOW SIMULATION; IGNITION; JET PUMPS; LARGE EDDY SIMULATION; MIXING; SMOKE; STRUTS; SUPERSONIC AERODYNAMICS; SUPERSONIC FLOW;

COMBUSTORS;

EID: 77949815733     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.43746     Document Type: Article

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