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

Clicks: 120
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.
Reference Key
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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