Mathematical Problems in Engineering
Volume 4 (1998), Issue 4, Pages 289-300
The hybersonic navier-stokes approximation for the normal shock structure of a perfect gas with the Sutherland viscosity law: Review and extension
1King Buck & Associates, Inc., San Diego 92110, CA, USA
2Florida Institute of Technology, Melbourne 32901-6988, FL, USA
Received 30 September 1997
Copyright © 1998 W. B. Bush and L. Krishnamurthy. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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.