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Oblique detonation wave ramjetTwo conceptual designs of the oblique detonation wave ramjet are presented. The performance is evaluated for stoichiometric hydrogen-air equivalence ratios of phi = 1/3, 2/3 and 1 for a range of flight Mach numbers from 6 to 10.
Document ID
19800005874
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Morrison, R. B. (Universal Systems, Inc. Arlington, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-159192
Report Number: NASA-CR-159192
Accession Number
80N14131
Funding Number(s)
CONTRACT_GRANT: NAS1-15344
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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