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Relaxation solution of the full Euler equationsA numerical procedure for the relaxation solution of the full steady Euler equations is described. By embedding the Euler system in a second order surrogate system, central differencing may be used in subsonic regions while retaining matrix forms well suited to iterative solution procedures and convergence acceleration techniques. Hence, this method allows the development of stable, fully conservative differencing schemes for the solution of quite general inviscid flow problems. Results are presented for both subcritical and shocked supercritical internal flows. Comparisons are made with a standard time dependent solution algorithm.
Document ID
19820016983
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Johnson, G. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Numerical Analysis
Report/Patent Number
NAS 1.15:82889
NASA-TM-82889
E-1265
Report Number: NAS 1.15:82889
Report Number: NASA-TM-82889
Report Number: E-1265
Accession Number
82N24859
Funding Number(s)
PROJECT: RTOP 505-32-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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