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Electronic Effects in Expansive Flow Under Hypersonic ConditionsPlasma effects in hypersonic shock tunnel nozzle using air
Document ID
19660028030
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bloom, M. H. (Polytechnic Inst. of Brooklyn New York, NY, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-78199
Report Number: NASA-CR-78199
Accession Number
66N37320
Funding Number(s)
CONTRACT_GRANT: NSG-409
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ELECTRIC PROPERTY
PLASMA FLOW
HYPERSONIC FLOW
SHOCK TUNNEL

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