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Electronic effects in expansive flow under hypersonic conditions.Plasma effects in nozzle flow of hypersonic shock tunnel using air, obtaining electron density profile
Document ID
19670032713
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bloom, M. H.
Date Acquired
August 3, 2013
Publication Date
October 1, 1966
Subject Category
Physics, Plasma
Accession Number
67A11442
Funding Number(s)
CONTRACT_GRANT: NSG-409
Distribution Limits
Public
Copyright
Other
Keywords
NOZZLE FLOW
PLASMA FLOW
ELECTRON DENSITY
SHOCK TUNNEL

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