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Entropy Splitting and Numerical DissipationA rigorous stability estimate for arbitrary order of accuracy of spatial central difference schemes for initial-boundary value problems of nonlinear symmetrizable systems of hyperbolic conservation laws was established recently by Olsson and Oliger (1994) and Olsson (1995) and was applied to the two-dimensional compressible Euler equations for a perfect gas by Gerritsen and Olsson (1996) and Gerritsen (1996). The basic building block in developing the stability estimate is a generalized energy approach based on a special splitting of the flux derivative via a convex entropy function and certain homogeneous properties. Due to some of the unique properties of the compressible Euler equations for a perfect gas, the splitting resulted in the sum of a conservative portion and a non-conservative portion of the flux derivative. hereafter referred to as the "Entropy Splitting." There are several potential desirable attributes and side benefits of the entropy splitting for the compressible Euler equations that were not fully explored in Gerritsen and Olsson. The paper has several objectives. The first is to investigate the choice of the arbitrary parameter that determines the amount of splitting and its dependence on the type of physics of current interest to computational fluid dynamics. The second is to investigate in what manner the splitting affects the nonlinear stability of the central schemes for long time integrations of unsteady flows such as in nonlinear aeroacoustics and turbulence dynamics. If numerical dissipation indeed is needed to stabilize the central scheme, can the splitting help minimize the numerical dissipation compared to its un-split cousin? Extensive numerical study on the vortex preservation capability of the splitting in conjunction with central schemes for long time integrations will be presented. The third is to study the effect of the non-conservative proportion of splitting in obtaining the correct shock location for high speed complex shock-turbulence interactions. The fourth is to determine if this method can be extended to other physical equations of state and other evolutionary equation sets. If numerical dissipation is needed, the Yee, Sandham, and Djomehri (1999) numerical dissipation is employed. The Yee et al. schemes fit in the Olsson and Oliger framework.
Document ID
20010047483
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Yee, H. C.
(NASA Ames Research Center Moffett Field, CA United States)
Vinokur, M.
(NASA Ames Research Center Moffett Field, CA United States)
Djomehri, M. J.
(Sverdrup Technology, Inc. Moffett Field, CA United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 1999
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/TM-1999-208793
A-99V0035
NAS 1.15:208793
Report Number: NASA/TM-1999-208793
Report Number: A-99V0035
Report Number: NAS 1.15:208793
Meeting Information
Meeting: 8th International Symposium on CFD
Location: Bremen
Country: Germany
Start Date: September 5, 1999
End Date: September 10, 1999
Funding Number(s)
PROJECT: RTOP 522-31-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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