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Analysis of flow from plug nozzles with secondary ejector systemsCalculation of supersonic flow field with Rankine-Hugoniot equations to compute flow properties across shock
Document ID
19650011860
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Inman, S. J.
Lee, C. G.
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-62188
R-128
Report Number: NASA-CR-62188
Report Number: R-128
Accession Number
65N21461
Funding Number(s)
CONTRACT_GRANT: NAS8-5289
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW FIELD
SUPERSONIC FLOW
SHOCK WAVE

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