Combustion instabilities in gas turbine engines

Series: Progress in astronautics and aeronautics ; . v. 210 Published by : American Institute of Aeronautics and Astronautics, (Reston, Va. :) Physical details: xiv, 657 p. : ill. Year: 2005
Online resources:
Tags from this library: No tags from this library for this title. Log in to add tags.
    Average rating: 0.0 (0 votes)
No physical items for this record

Includes bibliographical references and indexes.

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.

Electronic reproduction. Palo Alto, Calif. : ebrary, 2013. Available via World Wide Web. Access may be limited to ebrary affiliated libraries.

There are no comments on this title.

to post a comment.

Powered by Koha