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

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.

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Bibliographic Details
Published inMathematical problems in engineering Vol. 4; no. 4; pp. 289 - 300
Main Authors Bush, W. B., Krishnamurthy, L.
Format Journal Article
LanguageEnglish
Published 01.01.1998
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Summary: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.
ISSN:1024-123X
1563-5147
DOI:10.1155/S1024123X98000842