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.
Main Authors: | W. B. Bush, L. Krishnamurthy |
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Format: | Article |
Language: | English |
Published: |
Hindawi Limited
1998-01-01
|
Series: | Mathematical Problems in Engineering |
Subjects: | |
Online Access: | http://dx.doi.org/10.1155/S1024123X98000842 |
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