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Boundary-layer measurements in accelerated flows near Mach 1Velocity and temperature profile measurements for adiabatic boundary layers on cylindrical bodies in transonic parallel accelerated flows
Document ID
19670010561
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Wesoky, H. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-3882
Report Number: NASA-TN-D-3882
Accession Number
67N19890
Funding Number(s)
CONTRACT_GRANT: 129-01-09-06-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VELOCITY PROFILE
TRANSONIC FLOW
TEMPERATURE PROFILE
BOUNDARY LAYER FLOW

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