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A direct method for computation of nonequilibrium flows with detached shock waves.Nonequilibrium inviscid flow about arbitrarily shaped body with detached shock waves, using method with time derivative and bypassing boundary conditions
Document ID
19660048114
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bohachevsky, I. O.
Rubin, E. L.
Date Acquired
August 3, 2013
Publication Date
April 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 65-24
Report Number: AIAA PAPER 65-24
Accession Number
66A27404
Funding Number(s)
CONTRACT_GRANT: NONR-285/53/
CONTRACT_GRANT: NONR-839/34/
CONTRACT_GRANT: NAS5-3976
Distribution Limits
Public
Copyright
Other
Keywords
NONEQUILIBRIUM FLOW
SHOCK WAVE
FLOW FIELD
REENTRY BODY
AXISYMMETRIC FLOW

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