NASA NTRS · 19910000291
Artificial Dissipation In Computations Of Hypersonic Flows
Abstract
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.
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Yoon, S., Kwak, D.. 1991-06-01. Artificial Dissipation In Computations Of Hypersonic Flows. https://ntrs.nasa.gov/citations/19910000291
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