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A MULTITEMPERATURE BOUNDARY LAYEREnd-wall boundary layer behind a reflected shock in a shock tube in highly ionized argon
Document ID
19630025519
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Camac, M.
Kemp, N. H.
Date Acquired
August 1, 2013
Publication Date
August 28, 1963
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER 63-460
Report Number: AIAA PAPER 63-460
Accession Number
63A21578
Funding Number(s)
CONTRACT_GRANT: NASW-748
Distribution Limits
Public
Copyright
Other
Keywords
ARGON
SHOCK TUNNEL
PLASMA CONDUCTIVITY
BOUNDARY LAYER

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