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.
Artificial Dissipation In Computations Of Hypersonic Flows
NASA Tech Briefs ; 15 , 6
1991-06-01
Miscellaneous
No indication
English
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