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Nonequilibrium chemistry effects in hypersonic shock layers.Nonequilibrium flow fields over spherically blunted conical entry vehicle with chemical reaction in shock layer
Document ID
19660053460
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ball, W. H.
Lyon, F. J.
Date Acquired
August 3, 2013
Publication Date
June 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 66-420
Report Number: AIAA PAPER 66-420
Accession Number
66A32750
Funding Number(s)
CONTRACT_GRANT: NAS1-4743
Distribution Limits
Public
Copyright
Other
Keywords
NONEQUILIBRIUM FLOW
SHOCK LAYER
REENTRY PHYSICS

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