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Effect of roughness on heat transfer to hemisphere cylinders at Mach numbers 10.4 and 11.4Roughness effect on heat transfer to hemisphere cylinders in hypersonic flow
Document ID
19670010558
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dunavant, J. C. (NASA Langley Research Center Hampton, VA, United States)
Stone, H. W. (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-3871
Report Number: NASA-TN-D-3871
Accession Number
67N19887
Funding Number(s)
CONTRACT_GRANT: 129-01-09-11-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC FLOW
HEMISPHERE CYLINDER BODY
SURFACE ROUGHNESS EFFECT
HEAT TRANSFER

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