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Experimental investigation of boundary-layer transition on a cooled 7.5 deg total-angle cone at Mach 10Boundary layer transition for cooled 7.5 deg total angle cone at Mach 10
Document ID
19670029031
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Everhart, P. E. (NASA Langley Research Center Hampton, VA, United States)
Hamilton, H. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-4188
Report Number: NASA-TN-D-4188
Accession Number
67N38360
Funding Number(s)
CONTRACT_GRANT: 129-01-08-42-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HEAT TRANSFER
BOUNDARY LAYER TRANSITION
HYPERSONIC SPEED

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