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    In:  Other Sources
    Publication Date: 2019-07-12
    Description: Four artificial-dissipation mathematical models introduced to suppress spurious numerical oscillations in finite-difference computations of hypersonic external flows. Models tested for their effects in capturing details of shocks in hypersonic flows about bodies of various shapes.
    Keywords: MATHEMATICS AND INFORMATION SCIENCES
    Type: ARC-12260 , NASA Tech Briefs (ISSN 0145-319X); 15; 6; P. 124
    Format: text
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