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Steady state spurious errors in shock-capturing numerical schemesThe behavior of the steady state spurious error modes of the MacCormack scheme and the upwind scheme of Warming and Beam was obtained from a linearized difference equation for the steady state error. It was shown that the spurious errors can exist either as an eigensolution of the homogeneous part of this difference equation or because of excitation from large discretization errors near oblique shocks. It was found that the upwind scheme does not permit spurious oscillations on the upstream side of shocks. Examples are given for the inviscid Burgers' equation and for one and two dimensional gasdynamic flows.
Document ID
19800024845
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Karlsen, L. K.
(Royal Inst. of Tech. Stockholm, Sweden)
Date Acquired
September 4, 2013
Publication Date
December 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
KTH-AERO-TN-60
TRITA-FPT-032
Report Number: KTH-AERO-TN-60
Report Number: TRITA-FPT-032
Accession Number
80N33353
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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