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Real-gas hypersonic-nozzle flow parameters for nitrogen in thermodynamic equilibriumReal gas hypersonic nozzle flow parameters for nitrogen in thermodynamic equilibrium
Document ID
19640000148
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Clark, F. L. (NASA Langley Research Center Hampton, VA, United States)
Johnson, C. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-2019
Accession Number
64N10057
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REAL GAS
NOZZLE FLOW
THERMODYNAMIC EQUILIBRIUM
NITROGEN
HYPERSONIC FLOW

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