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Investigation of an actively cooled leading edge for hypersonic ramjet engines.Water cooled tubular leading edge for hypersonic ramjet engine inlets, discussing wind tunnel analysis
Document ID
19680053411
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Billig, F. S.
Grenleski, S. E.
Date Acquired
August 4, 2013
Publication Date
August 1, 1968
Subject Category
Propulsion Systems
Accession Number
68A34383
Funding Number(s)
CONTRACT_GRANT: NOW-62-0604-C
Distribution Limits
Public
Copyright
Other

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