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Starting phenomena for hypersonic inlets with thick turbulent boundary layers at Mach 6Starting phenomena of two-dimensional hypersonic inlets with turbulent intake boundary layers at free stream Mach 6
Document ID
19710021460
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Goldberg, T. J. (NASA Langley Research Center Hampton, VA, United States)
Hefner, J. N. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
L-7665
NASA-TN-D-6280
Report Number: L-7665
Report Number: NASA-TN-D-6280
Accession Number
71N30936
Funding Number(s)
CONTRACT_GRANT: 764-75-01-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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