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