Analysis of the combustion instability of a model gas turbine combustor by the transfer matrix method

Journal of Mechanical Science and Technology

Volumn 23, Issue 6, 2009, Pages 1602-1612

  Cha, Dong Jin ^a   Kim, Jay H ^b   Joo, Yong Jin ^c  

^a Hanbat National University   (South Korea)

^b University of Cincinnati   (United States)

^c Korea Electric Power Research Institute (KEPRI)   (South Korea)

Author keywords

Combustion instability; Model gas turbine combustor; Normal mode method; Stability margin; Thermoacoustics; Transfer matrix method

Indexed keywords

ACOUSTIC SYSTEMS; CLOSED-LOOP FEEDBACK SYSTEM; COMBUSTION INSTABILITIES; COMBUSTION INSTABILITY; COMBUSTION PRO-CESS; COMBUSTION SYSTEMS; COMPLEX GEOMETRIES; GAS TURBINE COMBUSTOR; HEAT SOURCES; LOW EMISSION; MODELING AND ANALYSIS; NORMAL MODE METHOD; SIDE BRANCHES; STABILITY ANALYSIS; STABILITY MARGIN; SYSTEM REPRESENTATION; THERMOACOUSTICS; TRANSFER MATRIXES;

ACOUSTIC FIELDS; COMBUSTION; COMBUSTORS; CONTROL SYSTEM STABILITY; CONTROL THEORY; ENGINES; GAS EMISSIONS; GAS TURBINES; LEAKAGE (FLUID); POSITION MEASUREMENT; SMOKE; STABILITY; SYSTEM STABILITY; THERMOCHEMISTRY; TURBOMACHINERY;

TRANSFER MATRIX METHOD;

EID: 67650876242     PISSN: 1738494X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s12206-009-0427-z     Document Type: Article

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