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Inviscid hypersonic flow around blunt bodies.Nonequilibrium flow, angles of attack and vapor injection effects on subsonic flow field of blunt body
Document ID
19650045502
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kaattari, G. E.
Katzen, E. D.
Date Acquired
August 2, 2013
Publication Date
July 1, 1965
Subject Category
Aerodynamics
Accession Number
65A28206
Distribution Limits
Public
Copyright
Other
Keywords
FLOW FIELD
SHOCK LAYER
INVISCID FLOW
BLUNT BODY
SUBSONIC FLOW

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