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Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model /

Bibliographic Details
Main Authors: Csank, Jeffrey T. (Author), Stueber, Thomas J. (Author)
Corporate Author: Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2013]
Series:NASA technical memorandum ; 216515.
Subjects:
Inlet flow.
Controllers.
Feedback control.
Computerized simulation.
Turbine engines.
Engine inlets.
Online Access:https://purl.fdlp.gov/GPO/gpo41411
http://purl.fdlp.gov/GPO/gpo41411
Description
Item Description:Title from title screen (viewed Nov. 13, 2013).
"May 2013."
Physical Description:1 online resource (12 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 11-12).