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Real-gas inviscid nozzle contours for nitrogen at mach 15, 17, and 19 with tabulated properties for the calculation of boundary-layer effectsHypersonic real-gas inviscid nozzle contours for nitrogen with tabulated flow properties for boundary layer effect calculation
Document ID
19650001351
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Ellison, J. C. (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, 1964
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-2496
Report Number: NASA-TN-D-2496
Accession Number
65N10952
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INVISCID FLOW
NOZZLE GEOMETRY
NITROGEN

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