Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion /

Bibliographic Details
Main Author:	Foster, Lancert E. (Author)
Corporate Author:	Joint Propulsion Conference and Exhibit
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
Series:	NASA technical memorandum ; 2012-217724.
Subjects:	Engine inlets. Hypersonic flight. Supersonic speed. Air breathing engines. Supersonic combustion ramjet engines. Specific impulse. Propulsion system configurations.
Online Access:	https://purl.fdlp.gov/GPO/gpo38254

Description
Item Description:	Title from title screen (viewed on July 12, 2013). "December 2012." "Prepared for the Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, ASEE, Atlanta, Geogria, July 30 to August 1, 2012."
Physical Description:	1 online resource (13 pages) : illustrations (some color).
Bibliography:	Includes bibliographical references (page 13).