Flow computation in the bottom vacuum region behind a plate in a hypersonic rarefied gas stream

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zbMath1019.76043MaRDI QIDQ1395226

E. M. Shakhov, Vladimir Titarev

Publication date: 29 June 2003

Published in: Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

zbMATH Keywords

finite difference method Boltzmann kinetic equation plate hypersonic flow collision operator nonuniform grid rarefied gas bottom vacuum region

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) Hypersonic flows (76K05)

Related Items (4)

Kinetic simulation of a supersonic compressible flow over different geometry bodies ⋮ Numerical calculation of the hypersonic rarefied transverse flow past a cold flat plate ⋮ Supersonic transverse rarefied gas flow past a strip ⋮ Conservative numerical methods for model kinetic equations

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