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Choice of implicit and explicit operators for the upwind differencing methodThe flux-vector and flux-difference splittings of Steger-Warming, van Leer and Roe are tested in all possible combinations on the implicit and explicit operators that can be distinguished in implicit relaxation methods for the steady Euler and Navier-Stokes equations. The tests include one-dimensional inviscid nozzle flow, and two-dimensional inviscid and viscous shock reflection. Roe's splitting, as anticipated, is found to uniformly yield the most accurate results. On the other hand, an approximate Roe splitting of the implicit operator (the complete Roe splitting is too complicated for practical use) proves to be the least robust with regard to convergence to the steady state. In this respect, the Steger-Warming splitting is the most robust; it leads to convergence when combined with any of the splittings in the explicit operator, although not necessarily in the most efficient way.
Document ID
19880012334
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Liou, Meng-Sing
(NASA Lewis Research Center Cleveland, OH, United States)
Vanleer, Bram
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Numerical Analysis
Report/Patent Number
ICOMP-88-8
NASA-TM-100857
NAS 1.15:100857
E-4061
Report Number: ICOMP-88-8
Report Number: NASA-TM-100857
Report Number: NAS 1.15:100857
Report Number: E-4061
Accession Number
88N21718
Funding Number(s)
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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