Complex conservative difference schemes for computing supersonic flows past simple aerodynamic forms

DOI10.1134/S0965542515120039zbMath1381.76232OpenAlexW2216079243MaRDI QIDQ266099

O. A. Azarova

Publication date: 13 April 2016

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

Full work available at URL: https://doi.org/10.1134/s0965542515120039

zbMATH Keywords

conservation lawssupersonic flowcomplex conservative schemescontact vortex structuresdivergent variablesnumerical solution of Euler equationstesting of schemes

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Finite difference methods for initial value and initial-boundary value problems involving PDEs (65M06) Supersonic flows (76J20)

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Propagation of a shock wave through a viscous heat-conducting gas in a long microchannel

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