Viscous nonequilibrium blunt-body flow.
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3902
Reference19 articles.
1. On the Validity of Continuum Theory for Satellite and Hypersonic Flight Problems at High Altitudes
2. Shock Wave and Flow Field Development in Hypersonic Re-Entry
3. Hypersonic viscous flow near the stagnation streamline of a blunt body. i - a test of local similarity
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1. An alternative interpretation of auroral precipitation and luminosity observations from the DE, DMSP, AUREOL, and Viking satellites in terms of their mapping to the nightside magnetosphere;Journal of Atmospheric and Terrestrial Physics;1993-01
2. Computation of the viscous shock layer on blunted cones;Fluid Dynamics;1976
3. Model of a viscous nonequilibrium shock layer with a thin shock wave;Fluid Dynamics;1975
4. Nonequilibrium viscous flow of a multicomponent gas in the vicinity of the stagnation point of a blunt body;Fluid Dynamics;1973
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