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Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feetReal air hypersonic shock-heated flow parameters at high speeds and high altitudes
Document ID
19640014678
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Huber, P. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1963
Subject Category
Geophysics
Report/Patent Number
NASA-TR-R-163
Report Number: NASA-TR-R-163
Accession Number
64N24592
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK HEATING
HYPERSONIC FLOW

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