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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