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Evaluation of the oblique detonation wave ramjetThe potential performance of oblique detonation wave ramjets is analyzed in terms of multishock diffusion, oblique detonation waves, and heat release. Results are presented in terms of thrust coefficients and specific impulses for a range of flight Mach numbers of 6 to 16.
Document ID
19780017411
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Morrison, R. B. (Universal Systems, Inc. Arlington, VA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-145358
Report Number: NASA-CR-145358
Accession Number
78N25354
Funding Number(s)
CONTRACT_GRANT: NAS1-14771
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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