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Artificial dissipation and central difference schemes for the Euler and Navier-Stokes equationsAn artificial dissipation model, including boundary treatment, that is employed in many central difference schemes for solving the Euler and Navier-Stokes equations is discussed. Modifications of this model such as the eigenvalue scaling suggested by upwind differencing are examined. Multistage time stepping schemes with and without a multigrid method are used to investigate the effects of changes in the dissipation model on accuracy and convergence. Improved accuracy for inviscid and viscous airfoil flow is obtained with the modified eigenvalue scaling. Slower convergence rates are experienced with the multigrid method using such scaling. The rate of convergence is improved by applying a dissipation scaling function that depends on mesh cell aspect ratio.
Document ID
19870012739
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Swanson, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Turkel, Eli
(Tel-Aviv Univ. Israel)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ICASE-87-29
NASA-CR-178296
NAS 1.26:178296
Report Number: ICASE-87-29
Report Number: NASA-CR-178296
Report Number: NAS 1.26:178296
Accession Number
87N22172
Funding Number(s)
CONTRACT_GRANT: NAS1-18107
PROJECT: RTOP 505-90-21-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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