Active combustion control for aircraft gas-turbine engines : experimental results for an advanced, low-emissions combustor prototype /

Active combustion control for aircraft gas-turbine engines : experimental results for an advanced, low-emissions combustor prototype /

Bibliographic Details
Corporate Authors: NASA Glenn Research Center, AIAA Aerospace Sciences Meeting
Other Authors: DeLaat, John C.
Format: Government Document Conference Proceeding eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:NASA technical memorandum ; 2012-217617.
Subjects:
Combustion stability.
Gas turbine engines.
Pressure sensors.
Combustion chambers.
Dynamic pressure.
Adaptive control.
Combustion control.
Online Access:https://purl.fdlp.gov/GPO/gpo31847
Description
Item Description:Title from title screen (viewed on Dec. 3, 2012).
"July 2012."
"Prepared for the 50th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics Nashville, Tennessee, January 9-12, 2012."
"AIAA-2012-783."
Electronic resource.
Physical Description:1 online resource (19 pages) : illustrations (some color).
Bibliography:Includes bibliographical references (pages 18-19).