Combustion instabilities in gas turbine engines : operational experience, fundamental mechanisms and modeling / / edited by Timothy C. Lieuwen, Vigor Yang.
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| Superior document: | Progress in astronautics and aeronautics ; v. 210 |
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| TeilnehmendeR: | |
| Year of Publication: | 2005 |
| Language: | English |
| Series: | Progress in astronautics and aeronautics ;
v. 210. |
| Online Access: | |
| Physical Description: | xiv, 657 p. :; ill. |
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Table of Contents:
- 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.