This article is cited in 10 papers

Computational methods and algorithms

On an implicit scheme for simulation of low Mach number gas flow

L. W. Dorodnicyn^a, B. N. Chetverushkin<sup>b

a</sup> Institute for Mathematical Modelling, Russian Academy of Sciences
^b M. V. Lomonosov Moscow State University

Abstract: A new approach to construction of the difference scheme for viscous subsonic gas flows is considered. The scheme is based on an implicit approximation of Boltzmann equation. The boundary layer at a plate has been simulated for the Mach number $M=0.1$.

Received: 26.02.1996

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