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  • NUMERICAL ANALYSIS  (3)
  • 2020-2022
  • 1995-1999
  • 1985-1989  (1)
  • 1980-1984  (2)
  • 1
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    In:  CASI
    Publication Date: 2019-06-28
    Description: Recent developments which have improved the understanding of how finite difference methods resolve discontinuous solutions to hyperbolic partial differential equations are discussed. As a result of this understanding improved shock capturing methods are currently being developed and tested. Some of these methods are described and numerical results are presented showing their performance on problems containing shocks in one and two dimensions. A conservative difference scheme is defined. Conservation implies that, except in very special circumstances, shocks must be spread over at least two grid intervals. These two interval shocks are actually attained in one dimension if the shock is steady and an upwind scheme is used. By analyzing this case, the reason for this excellent shock resolution can be determined. This result is used to provide a mechanism for improving the resolution of two dimensional steady shocks. Unfortunately, this same analysis shows that these results cannot be extended to shocks which move relative to the computing grid. Total variation diminishing (TVD) finite difference schemes and flux limiters are introduced to deal with money shocks and contact discontinuities.
    Keywords: NUMERICAL ANALYSIS
    Type: NASA-CR-172592 , ICASE-85-25 , NAS 1.26:172592
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  • 2
    Publication Date: 2019-06-28
    Description: The total variation diminishing (TVD) finite difference scheme can be interpreted as a Lax-Wendroff scheme plus an upwind weighted artificial dissipation term. If a particular flux limiter is chosen and the requirement for upwind weighting is removed, an artificial dissipation term which is based on the theory of TVD schemes is obtained which does not contain any problem dependent parameters and which can be added to existing MacCormack method codes. Numerical experiments to examine the performance of this new method are discussed.
    Keywords: NUMERICAL ANALYSIS
    Type: NASA-CR-172373 , ICASE-84-20 , NAS 1.26:172373
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  • 3
    Publication Date: 2019-06-28
    Description: The upwind difference schemes of Godunov, Osher, Roe and van Leer are able to resolve one dimensional steady shocks for the Euler equations within one or two mesh intervals. Unfortunately, this resolution is lost in two dimensions when the shock crosses the computing grid at an oblique angle. To correct this problem, a numerical scheme was developed which automatically locates the angle at which a shock might be expected to cross the computing grid and then constructs separate finite difference formulas for the flux components normal and tangential to this direction. Numerical results which illustrate the ability of this method to resolve steady oblique shocks are presented.
    Keywords: NUMERICAL ANALYSIS
    Type: NASA-CR-172179 , NAS 1.26:172179 , REPT-83-37
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