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Record Nr. |
UNINA9910824692903321 |
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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 |
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Pubbl/distr/stampa |
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Reston, Va., : American Institute of Aeronautics and Astronautics, c2005 |
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ISBN |
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1-60086-680-8 |
1-60086-461-9 |
1-61583-076-6 |
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Descrizione fisica |
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1 online resource (672 p.) |
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Collana |
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Progress in astronautics and aeronautics ; ; v. 210 |
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Altri autori (Persone) |
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LieuwenTimothy C |
YangVigor |
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Disciplina |
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Soggetti |
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Gas-turbines - Combustion |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Description based upon print version of record. |
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Nota di bibliografia |
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Includes bibliographical references and indexes. |
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Nota di contenuto |
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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 |
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