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

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Bibliographic Details
Superior document:Progress in astronautics and aeronautics ; v. 210
:
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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245 0 0 |a Combustion instabilities in gas turbine engines  |h [electronic resource] :  |b operational experience, fundamental mechanisms and modeling /  |c edited by Timothy C. Lieuwen, Vigor Yang. 
260 |a Reston, Va. :  |b American Institute of Aeronautics and Astronautics,  |c c2005. 
300 |a xiv, 657 p. :  |b ill. 
490 1 |a Progress in astronautics and aeronautics ;  |v v. 210 
504 |a Includes bibliographical references and indexes. 
505 0 |a 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. 
533 |a Electronic reproduction. Ann Arbor, MI : ProQuest, 2015. Available via World Wide Web. Access may be limited to ProQuest affiliated libraries. 
650 0 |a Gas-turbines  |x Combustion. 
655 4 |a Electronic books. 
700 1 |a Lieuwen, Timothy C. 
700 1 |a Yang, Vigor. 
710 2 |a ProQuest (Firm) 
830 0 |a Progress in astronautics and aeronautics ;  |v v. 210. 
856 4 0 |u https://ebookcentral.proquest.com/lib/oeawat/detail.action?docID=3111524  |z Click to View