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.
Open Access
The hybersonic navier-stokes approximation for the normal shock structure of a perfect gas with the Sutherland viscosity law: Review and extension
Received30 Sept 1997
Copyright
Copyright © 1998 Hindawi Publishing Corporation. This is an open access article distributed under the
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