Shock position control for mode transition in a turbine based combined cycle engine inlet model / Jeffrey T. Csank and Thomas J. Stueber.

Author/creator Csank, Jeffrey T. author.
Other author Stueber, Thomas J., author.
Other author NASA Glenn Research Center, issuing body.
Other author Fundamental Aeronautics Program (U.S.), sponsoring body.
Format Electronic
PublicationCleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
Description1 online resource (17 pages) : color illustrations.
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo45744

SeriesNASA/TM ; 2013-217824
NASA technical memorandum 217824. ^A467613
General noteTitle from title screen (viewed on Feb. 6, 2014).
General note"January 2013."
General note"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."
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (pages 16-17).
Funding informationSponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center WBS 599489.02.07.03.07.11.01
Funding informationE-18574
GPO item number0830-D (online)
Govt. docs number NAS 1.15:2013-217824

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