Geodesic
Mathematical model of a kinetic boundary layer
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 54 (2014) no. 6, pp. 1000-1007
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The two-dimensional (plane) problem of a hypersonic kinetic boundary layer developing on a thin body in the case of a homogeneous polyatomic gas flow with no dissociation or electron excitation is considered assuming that energy exchange between translational and internal molecular degrees of freedom is easy. (The approximation of a hypersonic kinetic boundary layer arises from the kinetic theory of gases and, within the thin-layer model, takes into account the strong nonequilibrium of the hypersonic flow with respect to translational and internal degrees of freedom of the gas particles.) A method is proposed for constructing the solution of the given kinetic problem in terms of a given solution of an equivalent well-studied classical Navier–Stokes hypersonic boundary layer problem (which is traditionally formulated on the basis of the Navier–Stokes equations). 
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A. L. Ankudinov. Mathematical model of a kinetic boundary layer. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 54 (2014) no. 6, pp. 1000-1007. http://geodesic.mathdoc.fr/item/ZVMMF_2014_54_6_a10/

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