1999
DOI: 10.1002/(sici)1097-0363(19990115)29:1<97::aid-fld780>3.0.co;2-j
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An investigation of random choice method for three-dimensional steady supersonic flows

Abstract: In this paper, an unsplit random choice method (RCM) is developed and applied to numerically solve three‐dimensional supersonic steady flow problems. In order to keep the contacts (slip surfaces) crisply resolved, a new Lagrangian formulation is employed. Due to the lack of exact solutions to 3D Riemann problems, approximate Riemann solutions in the weak sense are adopted. The RCM is thus as efficient as the deterministic TVD schemes, and yields almost identical results in the model problems. Copyright © 1999 … Show more

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Cited by 3 publications
(1 citation statement)
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References 29 publications
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“…Later it was used as a numerical tool by Chorin in gas dynamics [22,23]. Chorin's work was followed by numerous researchers, with applications and further improvements in [24][25][26], and more recently [27,28], etc. The main advantage of this method is the sharp resolutions of shocks and especially, contact discontinuities.…”
Section: Introductionmentioning
confidence: 99%
“…Later it was used as a numerical tool by Chorin in gas dynamics [22,23]. Chorin's work was followed by numerous researchers, with applications and further improvements in [24][25][26], and more recently [27,28], etc. The main advantage of this method is the sharp resolutions of shocks and especially, contact discontinuities.…”
Section: Introductionmentioning
confidence: 99%