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  • 1
    Publication Date: 2019-07-13
    Description: Conservative algorithms for boundary interfaces of overlaid grids are presented. The basic method is zeroth order, and is extended to a higher order method using interpolation and subcell decomposition. The present method, strictly based on a conservative constraint, is tested with overlaid grids for various applications of unsteady and steady supersonic inviscid flows with strong shock waves. The algorithm is also applied to a multi-level grid adaptation in which the next level finer grid is overlaid on the coarse base grid with an arbitrary orientation.
    Keywords: AERODYNAMICS
    Type: NASA-TM-102080 , E-4842 , NAS 1.15:102080 , AIAA PAPER 89-1980 , Computational Fluid Dynamics Conference; Jun 13, 1989 - Jun 15, 1989; Buffalo, NY; United States
    Format: application/pdf
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