http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model
1 online resource (12 pages) : illustrations.
Title from title screen (viewed Nov. 13, 2013).
Includes bibliographical references (pages 11-12).
Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center WBS 599489.02.07.03.07.11.02