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Experimental investigation of the turbulent boundary layer at a Mach number of 6 with heat transfer at high Reynolds numbersTurbulent boundary layer skin friction and heat transfer on hollow cylinder in hypersonic flow at high Reynolds numbers
Document ID
19670010557
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Adcock, J. B. (NASA Langley Research Center Hampton, VA, United States)
Peterson, J. B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Samuels, R. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-3858
Report Number: NASA-TN-D-3858
Accession Number
67N19886
Funding Number(s)
CONTRACT_GRANT: 129-01-09-04-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CYLINDRICAL SHELL
HYPERSONIC FLOW
SKIN FRICTION
HEAT TRANSFER
TURBULENT BOUNDARY LAYER

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