Geodesic
Burnett hypersonic thin shock layer nеаr the windward side of a flat plate
Matematičeskoe modelirovanie, Tome 26 (2014) no. 4, pp. 110-118

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The simplification of the thin shock one-layer Burnett equations in reference to task of the rarefied gas hypersonic flow around the windward side of a flat plate with the great angle of attack is made on the basis of the two-layer ideology of a thin viscous shock layer theory for the non-thin bodies, assumed two (smear shock plus own shock layer) specific regions (layers) between the free-stream flow and the streamlined surface. It is demonstrated, that the Burnett thin shock layer problem under consideration in two-layer approach fully reduce to a corresponding Navier–Stokes one.
Keywords: Burnett equations, hypersonic flow, thin shock layer, two-layer model, windward side of flat plate with great angle of attack. 
@article{MM_2014_26_4_a8,
     author = {A. L. Ankudinov},
     title = {Burnett hypersonic thin shock layer n{\cyre}{\cyra}r the windward side of a flat plate},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {110--118},
     publisher = {mathdoc},
     volume = {26},
     number = {4},
     year = {2014},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2014_26_4_a8/}
}
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A. L. Ankudinov. Burnett hypersonic thin shock layer nеаr the windward side of a flat plate. Matematičeskoe modelirovanie, Tome 26 (2014) no. 4, pp. 110-118. http://geodesic.mathdoc.fr/item/MM_2014_26_4_a8/