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Numerical solution of supersonic three-dimensional free-mixing flows using the parabolic-elliptic Navier-Stokes equationsA numerical method is presented for solving the parabolic-elliptic Navier-Stokes equations. The solution procedure is applied to three-dimensional supersonic laminar jet flow issuing parallel with a supersonic free stream. A coordinate transformation is introduced which maps the boundaries at infinity into a finite computational domain in order to eliminate difficulties associated with the imposition of free-stream boundary conditions. Results are presented for an approximate circular jet, a square jet, varying aspect ratio rectangular jets, and interacting square jets. The solution behavior varies from axisymmetric to nearly two-dimensional in character. For cases where comparisons of the present results with those obtained from shear layer calculations could be made, agreement was good.
Document ID
19770004399
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hirsh, R. S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1976
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TN-D-8195
L-10750
Report Number: NASA-TN-D-8195
Report Number: L-10750
Accession Number
77N11342
Funding Number(s)
PROJECT: RTOP 505-06-11-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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