Numerical solution of the hypersonic viscous shock-layer equations
Author:
Affiliation:
1. Virginia Polytechnic Institute, Blacksburg, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5776
Reference18 articles.
1. Second-order boundary-layer effects in hypersonic flow past axisymmetric blunt bodies
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