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Heat-transfer measurements in the shock-induced flow separation region in a supersonic nozzle.Pressure and semilocal wall heat flux measurements in shock induced flow separation region in supersonic nozzle, noting shock waves-flow interaction
Document ID
19680046124
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Back, L. H.
Cuffel, R. F.
Massier, P. F.
Date Acquired
August 4, 2013
Publication Date
May 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
JPL-TR-32-1278
Report Number: JPL-TR-32-1278
Accession Number
68A27096
Distribution Limits
Public
Copyright
Other

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