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Transition and flow reattachment behind an Apollo-like body at Mach numbers to 9Transition from laminar to turbulent flow in near wake of supersonic reentry body
Document ID
19680018748
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Kruse, R. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4645
Report Number: NASA-TN-D-4645
Accession Number
68N28220
Funding Number(s)
CONTRACT_GRANT: 129-01-09-04-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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