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Experimental and Theoretical Turbulent Boundary Layer Development in a Mach 4.4 Water-Cooled Conical NozzleTurbulent boundary layer temperature and velocity measurements in supersonic water-cooled conical nozzle
Document ID
19690023975
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Boldman, Donald R. (NASA Lewis Research Center Cleveland, OH, United States)
Schmidt, James F. (NASA Lewis Research Center Cleveland, OH, United States)
Ehlers, Robert C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1969
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-5377
Report Number: NASA-TN-D-5377
Accession Number
69N33353
Funding Number(s)
CONTRACT_GRANT: 129-01-05-19-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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