Geodesic
On an implicit scheme for simulation of low Mach number gas flow
Matematičeskoe modelirovanie, Tome 9 (1997) no. 5, pp. 108-118 Cet article a éte moissonné depuis la source Math-Net.Ru

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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 $M=0.1$. 
@article{MM_1997_9_5_a10,
     author = {L. W. Dorodnicyn and B. N. Chetverushkin},
     title = {On an implicit scheme for simulation of low {Mach} number gas flow},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {108--118},
     year = {1997},
     volume = {9},
     number = {5},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_1997_9_5_a10/}
}
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%A B. N. Chetverushkin
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%D 1997
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L. W. Dorodnicyn; B. N. Chetverushkin. On an implicit scheme for simulation of low Mach number gas flow. Matematičeskoe modelirovanie, Tome 9 (1997) no. 5, pp. 108-118. http://geodesic.mathdoc.fr/item/MM_1997_9_5_a10/