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A direct method for computation of nonequilibrium flows with detached shock waves. i - two-dimensional flows. ii - axisymmetric blunt-body at an angle of attack.Nonequilibrium inviscid flow about arbitrarily shaped body with detached shock waves, using method with time derivative and bypassing boundary conditions
Document ID
19650033909
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bohachevsky, I. O.
Mates, R. E.
Rubin, E. L.
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 65-24
Report Number: AIAA PAPER 65-24
Accession Number
65A16613
Funding Number(s)
CONTRACT_GRANT: NAS5-3976
CONTRACT_GRANT: NONR-285/53/
CONTRACT_GRANT: NONR-839/34/
Distribution Limits
Public
Copyright
Other
Keywords
SHOCK WAVE
AXISYMMETRIC FLOW
REENTRY BODY
NONEQUILIBRIUM FLOW
FLOW FIELD

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