Spatially distributed flame transfer functions for predicting combustion dynamics in lean premixed gas turbine combustors

Combustion and Flame

Volumn 157, Issue 9, 2010, Pages 1718-1730

  Kim, K T ^a   Lee, J G ^a   Quay, B D ^a   Santavicca, D A ^a  

^a The Pennsylvania State University   (United States)

Author keywords

Combustion instability; Eigenfrequency; Flame transfer function; Heat release distribution

Indexed keywords

ACCURATE PREDICTION; CHEMILUMINESCENCE INTENSITY; COMBUSTION DYNAMICS; COMBUSTION INSTABILITIES; EIGEN FREQUENCIES; EIGENFREQUENCY; FLAME LENGTH; FLAME TRANSFER FUNCTIONS; GAS TURBINE COMBUSTOR; HEAT RELEASE DISTRIBUTION; HEAT RELEASE OSCILLATION; INLET VELOCITY; LABORATORY SCALE; LINEAR STABILITY; MODEL PREDICTION; OUTPUT FUNCTIONS; PREMIXED; PREMIXED GAS; RESPONSE CHARACTERISTIC; SUPERPOSITION PRINCIPLE; THERMO-ACOUSTIC MODEL; TWO-MICROPHONE TECHNIQUE;

COMBUSTION; COMBUSTORS; EXPLOSIVES; FLAMMABILITY; FLUID STRUCTURE INTERACTION; FORECASTING; GAS TURBINES; SWIRLING FLOW; TURBOMACHINERY;

TRANSFER FUNCTIONS;

ACCURACY; ANALYTICAL PARAMETERS; ARTICLE; CHEMOLUMINESCENCE; COMBUSTION; COMBUSTOR; DEVICE; FIRE; FLAME TRANSFER FUNCTION; GAS TURBINE POWER; GROWTH RATE; MEASUREMENT; METHODOLOGY; MICROPHONE; OSCILLATION; PREDICTION; PRIORITY JOURNAL; TRANSPORT KINETICS; VELOCITY;

EID: 77954384053     PISSN: 00102180     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.combustflame.2010.04.016     Document Type: Article

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