The hybersonic navier-stokes approximation for the normal shock structure of a perfect gas with the Sutherland viscosity law: Review and extension

W. B. Bush and L. Krishnamurthy

Mathematical Problems in Engineering, 1998, vol. 4, 1-12

Abstract:

By means of a four-region asymptotic analysis, a uniformly valid description of the Sutherland-viscosity-law Navier-Stokes structure of the normal shock wave in the hypersonic approximation is obtained.

Date: 1998
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Persistent link: https://EconPapers.repec.org/RePEc:hin:jnlmpe:872051

DOI: 10.1155/S1024123X98000842

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