Thermoacoustic modeling of a gas turbine using transfer functions measured at full engine pressure

Proceedings of the ASME Turbo Expo

Volumn 2, Issue , 2009, Pages 503-514

  Schuermans, Bruno ^a   Guethe, Felix ^a   Pennel, Douglas ^a   Guyot, Daniel ^b   Paschereit, Christian Oliver ^b  

^a ALSTOM   (France)

^b TECHNISCHE UNIVERSITÄT BERLIN   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC EXCITATION; ACOUSTIC METHOD; ACOUSTIC RESPONSE; ACOUSTIC TECHNIQUES; CHEMILUMINESCENCE INTENSITY; ENGINE PRESSURE; EQUIVALENCE RATIOS; FLAME TRANSFER FUNCTIONS; GAS TURBINE BURNERS; HEAT RELEASE; HEAT RELEASE FLUCTUATIONS; MASS FLOW FLUCTUATION; NETWORK MODELS; NON-LINEAR; OPTICAL METHODS; OPTICAL SIGNALS; OPTICAL TECHNIQUE; OPTICAL WAVELENGTH; PHOTO MULTIPLIER TUBE; PRESSURE TESTS; SOURCE TERMS; THERMOACOUSTICS; TIME DOMAIN;

COMBUSTION; COMBUSTION CHAMBERS; FLAMMABILITY; FUEL BURNERS; GAS TURBINES; LUMINESCENCE; MASS TRANSFER; OPTICAL ENGINEERING; PHOTOMULTIPLIERS; PROPULSION; SIGNALING; TEST FACILITIES; THREE DIMENSIONAL; TIME DOMAIN ANALYSIS; TRANSDUCERS; TURBOMACHINERY;

TRANSFER FUNCTIONS;

EID: 77953194267     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2009-59605     Document Type: Conference Paper

References (14)

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