4.7 Article

Analytical shock solutions at large and small Prandtl number

Journal

JOURNAL OF FLUID MECHANICS
Volume 726, Issue -, Pages -

Publisher

CAMBRIDGE UNIV PRESS
DOI: 10.1017/jfm.2013.262

Keywords

compressible flows; Navier-Stokes equations; shock waves

Funding

  1. Lawrence Livermore National Security, LLC (LLNS) [DE-AC52-07NA27344]

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Exact one-dimensional solutions to the equations of fluid dynamics are derived in the Pr -> infinity and Pr -> 0 limits (where Pr is the Prandtl number). The solutions are analogous to the Pr = 3/4 solution discovered by Becker and analytically capture the profile of shock fronts in ideal gases. The large-Pr solution is very similar to Becker's solution, differing only by a scale factor. The small-Pr solution is qualitatively different, with an embedded isothermal shock occurring above a critical Mach number. Solutions are derived for constant viscosity and conductivity as well as for the case in which conduction is provided by a radiation field. For a completely general density- and temperature-dependent viscosity and conductivity, the system of equations in all three limits can be reduced to quadrature. The maximum error in the analytical solutions when compared to a numerical integration of the finite-Pr equations is O(Pr-1) as Pr -> infinity and O(Pr) as Pr -> 0.

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