SCOPUS 정보 검색 플랫폼

Volumn 157, Issue 8, 2010, Pages 1510-1525

Temporally resolved planar measurements of transient phenomena in a partially pre-mixed swirl flame in a gas turbine model combustor

(4) Boxx, I a Stohr M a Carter, C b Meier, W a

a GERMAN AEROSPACE CENTER DLR (Germany)

b AIR FORCE RESEARCH LABORATORY (United States)

Author keywords

Auto ignition; Combustion diagnostics; Gas turbine model combustor; KHz OH PLIF; KHz PIV; Local extinction; Precessing vortex core; Swirl flame; Turbulent flame

Indexed keywords

AUTO-IGNITION; COMBUSTION DIAGNOSTICS; GAS TURBINE MODEL COMBUSTOR; LOCAL EXTINCTION; PRECESSING VORTEX CORE; SWIRL FLAMES; TURBULENT FLAME;

ACOUSTIC INTENSITY MEASUREMENT; COMBUSTORS; FLOW VISUALIZATION; FREE RADICALS; GAS TURBINES; IGNITION; METHANE; SWIRLING FLOW; TURBOMACHINERY; VELOCITY MEASUREMENT; VORTEX FLOW; VORTICITY;

FLAMMABILITY;

HYDROXYL RADICAL; METHANE;

ACOUSTICS; ARTICLE; CHEMOLUMINESCENCE; COMBUSTION; FLUORESCENCE; GAS TURBINE POWER; HEAT; MODEL; PARTICLE IMAGE VELOCIMETRY; PRIORITY JOURNAL; VELOCITY;

EID: 77953744150 PISSN: 00102180 EISSN: None Source Type: Journal
DOI: 10.1016/j.combustflame.2009.12.015 Document Type: Article

Times cited : (202)

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