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Measurement by wake momentum surveys at Mach 1.61 and 2.01 of turbulent boundary-layer skin friction on five swept wingsMeasurement by wake momentum surveys at Mach 1.61 and 2.01 of turbulent boundary layer skin friction on five swept wings
Document ID
19670003841
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Czarnecki, K. R. (NASA Langley Research Center Hampton, VA, United States)
Jackson, M. W. (NASA Langley Research Center Hampton, VA, United States)
Sorrells, R. B., III (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3764
Accession Number
67N13170
Funding Number(s)
CONTRACT_GRANT: 720-01-00-04-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WAKE
SWEPT WING
TURBULENT BOUNDARY LAYER
SKIN FRICTION

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