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Turbulent heat transfer associated with control surface at Mach 6.Turbulent heat transfer associated with controls for attached or separated flow analyzed for design of hypersonic cruise aircraft
Document ID
19680056351
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Emery, J. C.
Goldberg, T. J.
Keyes, J. W.
Date Acquired
August 4, 2013
Publication Date
August 1, 1968
Subject Category
Aerodynamics
Accession Number
68A37323
Distribution Limits
Public
Copyright
Other

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