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Note on a correlation of boundary-layer transition results on highly cooled blunt bodiesBoundary layer transition from hypersonic laminar to turbulent flow around blunt bodies
Document ID
19660024018
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Wisniewski, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1958
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-MEMO-10-8-58E
Report Number: NASA-MEMO-10-8-58E
Accession Number
66N33308
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC FLOW
TURBULENT FLOW
BLUNT BODY
BOUNDARY LAYER TRANSITION
LAMINAR FLOW

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