An experimental and computational study of a multi-swirl gas turbine combustor

Proceedings of the Combustion Institute

Volumn 31 II, Issue 2, 2007, Pages 3107-3114

  Fureby, C ^a   Grinstein, F F ^b   Li, G ^c   Gutmark, E J ^c  

^a SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

^b LOS ALAMOS NATIONAL LABORATORY   (United States)

^c University of Cincinnati   (United States)

Author keywords

Experiment; Gas turbine; Large eddy simulation; Lean direct fuel injection

Indexed keywords

CHARACTERIZATION; COMPUTATIONAL METHODS; GAS TURBINES; JETS; LARGE EDDY SIMULATION; SWIRLING FLOW; THERMOCOUPLES; TURBULENT FLOW; VELOCITY MEASUREMENT;

FLAME DYNAMICS; STATE-OF-THE-ART DIAGNOSTICS; VORTEX CORES;

COMBUSTORS;

EID: 34548762131     PISSN: 15407489     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.proci.2006.07.127     Document Type: Article

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