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Roughness effects on boundary-layer transition for blunt-leading-edge plates at Mach 6Effects of controlled roughness on boundary layer transition for upswept blunted plates in free stream
Document ID
19660023725
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Holloway, P. F. (NASA Langley Research Center Hampton, VA, United States)
Morrisette, E. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3517
Report Number: NASA-TN-D-3517
Accession Number
66N33015
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BLUNT BODY
FLAT PLATE
SURFACE ROUGHNESS
FREE STREAM
BOUNDARY LAYER TRANSITION

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