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Combustion instabilities in gas turbine engines [[electronic resource] ] : operational experience, fundamental mechanisms and modeling / / edited by Timothy C. Lieuwen, Vigor Yang



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Titolo: Combustion instabilities in gas turbine engines [[electronic resource] ] : operational experience, fundamental mechanisms and modeling / / edited by Timothy C. Lieuwen, Vigor Yang Visualizza cluster
Pubblicazione: Reston, Va., : American Institute of Aeronautics and Astronautics, c2005
Descrizione fisica: 1 online resource (672 p.)
Disciplina: 629.134/353
Soggetto topico: Gas-turbines - Combustion
Altri autori: LieuwenTimothy C  
YangVigor  
Note generali: Description based upon print version of record.
Nota di bibliografia: Includes bibliographical references and indexes.
Nota di contenuto: Combustion instabilities: basic concepts -- Combustion instabilities in industrial gas turbines: Solar Turbine's experience -- Incorporation of combustion instability issues into design process: GE aeroderivative and aero engines experience -- Combustion instability and its passive control: Rolls-Royce aeroderivative engine experience -- Thermoacoustic design tools and passive control: Siemens power generation approaches -- Characterization and control of aeroengine combustion Instability: Pratt & Whitney and NASA experience -- Monitoring of combustion instabilities: Calpine's experience -- Monitoring combustion instabilities: E.ON UK's experience -- Combustion instability mechanisms in premixed combustors -- Flow and flame dynamics of lean premixed swirl Injectors -- Acoustic-vortex-flame interactions in gas turbines -- Physics of premixed combustion-acoustic wave interactions -- Acoustic analysis of gas-turbine combustors -- Three-dimensional linear stability analysis of gas turbine combustion dynamics -- Implementation of instability prediction in design: ALSTOM approaches -- Experimental diagnostics of combustion instabilities -- Passive control of combustion instabilities in stationary gas turbines -- Factors affecting the control of unstable combustors -- Implementation of active control in a full-scale gas-turbine combustor.
Titolo autorizzato: Combustion instabilities in gas turbine engines  Visualizza cluster
ISBN: 1-60086-680-8
1-60086-461-9
1-61583-076-6
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910824692903321
Lo trovi qui: Univ. Federico II
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Serie: Progress in astronautics and aeronautics ; ; v. 210.