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Flow phenomena and convective heat transfer in a conical supersonic nozzle.Turbulent boundary layer flow in conical supersonic nozzle, discussing convective heat transfer and adverse pressure gradient effect
Document ID
19670056085
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Back, L. H.
Cuffel, R. F.
Massier, P. F.
Date Acquired
August 3, 2013
Publication Date
August 1, 1967
Publication Information
Publication: JOURNAL OF SPACECRAFT AND ROCKETS
Subject Category
Aerodynamics
Report/Patent Number
JPL-TR-32-1152
Report Number: JPL-TR-32-1152
Accession Number
67A34814
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other
Keywords
GAS DYNAMICS
TURBULENT BOUNDARY LAYER
CONVECTIVE HEAT TRANSFER
PRESSURE GRADIENT
SUPERSONIC NOZZLE

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