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 ; 217824.
Subjects:	Computerized simulation. Engine inlets. Feedback control. Inlet flow. Turbine engines.
Online Access:	https://purl.fdlp.gov/GPO/gpo45744 http://purl.fdlp.gov/GPO/gpo45744

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).