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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Published in | Mathematical problems in engineering Vol. 4; no. 4; pp. 289 - 300 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
01.01.1998
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Online Access | Get full text |
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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. |
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ISSN: | 1024-123X 1563-5147 |
DOI: | 10.1155/S1024123X98000842 |