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

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ID: 196855
1998
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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.
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bush1998mathematicalthe Use this key to autocite in the manuscript while using SciMatic Manuscript Manager or Thesis Manager
Authors ;W. B. Bush;L. Krishnamurthy
Journal journal of power sources
Year 1998
DOI 10.1155/S1024123X98000842
URL
http://dx.doi.org/10.1155/S1024123X98000842
Keywords
civil engineering (general)mathematics engineering (general) asymptotic analysis; hypersonic flow; navier-stokes; normal shock; sutherland viscosity; uniformly valid solution

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