Combined cycle engine large-scale inlet for mode transition experiments : system identification rack hardware design /

Combined cycle engine large-scale inlet for mode transition experiments : system identification rack hardware design /

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Bibliographic Details
Author / Creator:Thomas, Randy, author.
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2013.
Description:1 online resource (24 pages) : illustrations (some color).
Language:English
Series:NASA/TM ; 2013-217864
NASA technical memorandum ; 2013-217864.
Subject:
Actuators.
Automatic control.
Hardware-in-the-loop simulation.
Pressure transducers.
Supersonic wind tunnels.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10031284
Hidden Bibliographic Details
Other authors / contributors:Stueber, Thomas J., author.
NASA Glenn Research Center, issuing body.
Notes:Title from title screen (viewed June 4, 2014).
"August 2013."
Includes bibliographical references (page 24).
Sponsored by National Aeronautics and Space Administration WBS 599489.02.07.03.07.11.02
E-18657
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2013-217864

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