Numerical Method for Hypersonic Internal Flow over Blunt Leading Edges and Two Blunt Bodies
Author:
Affiliation:
1. McGill University, Montreal, Canada
2. Polytechnic Institute of Brooklyn, New York N.Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50165
Reference21 articles.
1. The Supersonic Blunt-Body Problem - Review and Extension
2. On the calculation of flow past axisymmetric bodies with detached shock waves using an electronic computing machine
3. A direct method for computation of nonequilibrium flows with detached shock waves.
4. Application of Godunov's method to blunt-body calculations.
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