Advanced 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 Fundamental Aeronautics Program (U.S.), sponsoring body.
Other author NASA Glenn Research Center, issuing body.
Format Electronic
PublicationCleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2013]
Description1 online resource (12 pages) : illustrations.
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo41411

SeriesNASA/TM ; 2013-216515
NASA technical memorandum 216515. ^A467613
General noteTitle from title screen (viewed Nov. 13, 2013).
General note"May 2013."
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (pages 11-12).
Funding informationE-18676
Funding informationSponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center WBS 599489.02.07.03.07.11.02
GPO item number0830-D (online)
Govt. docs number NAS 1.15:2013-216515

Availability

Library Location Call Number Status Item Actions
Electronic Resources Access Content Online ✔ Available