Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight /

Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight /

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Bibliographic Details
Main Authors: Thomas, Scott R. (Author), Perkins, H. Douglas (Author), Trefny, Charles J. (Author)
Format: Government Document Electronic eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, March 1997.
Series:NASA technical memorandum ; 107422.
Subjects:
Ejectors.
Hydrocarbon fuels.
Wind tunnel tests.
Supersonic speed.
Mach number.
Engine tests.
Propulsion system performance.
Flow distribution.
Online Access:CONNECT
Description
Item Description:"March 1997"--Report documentation page.
"Prepared for the 89th Symposium sponsored by the Propulsion and Energetics Panel of the NATO Advisory Group for Aerospace Research and Development, Palaiseau, France, April 14-17, 1997."
"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
Physical Description:1 online resource (10 pages) : illustrations.
Bibliography:Includes bibliographical references (page 4).

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