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Effect of controlled surface roughness on boundary-layer transition and heat transfer at mach numbers of 4.8 and 6.0Effects of controlled surface roughness on boundary layer transition and heat transfer at hypersonic speeds
Document ID
19640009039
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Holloway, P. F. (NASA Langley Research Center Hampton, VA, United States)
Sterrett, J. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1964
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TN-D-2054
Report Number: NASA-TN-D-2054
Accession Number
64N18953
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC SPEED
HEAT TRANSFER
SURFACE ROUGHNESS
BOUNDARY LAYER TRANSITION

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