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

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

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Bibliographic Details
Main Authors: Csank, Jeffrey T. (Author), Stueber, Thomas J. (Author)
Corporate Author: Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format: Government Document Electronic eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
Series:NASA technical memorandum ; 217824.
Subjects:
Computerized simulation.
Engine inlets.
Feedback control.
Inlet flow.
Turbine engines.
Online Access:CONNECT
Description
Item Description:Title from title screen (viewed on Feb. 6, 2014).
"January 2013."
"Prepared for the 45th Combustion/33rd Airbreathing Propulsion/33rd Exhaust Plume and Signatures/27th Propulsion Hazards Joint Subcommittee Meeting sponsored by the Joint Army-Navy-NASA-Air Force (JANNAF), Monterey, California, December 3-7, 2012."
Physical Description:1 online resource (17 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 16-17).

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