Some Features of Supersonic and Hypersonic Flow About Blunted Cones
Author:
Affiliation:
1. The Martin Company,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.9473
Reference33 articles.
1. The Generalized Shock-Expansion Method and Its Application to Bodies Traveling at High Supersonic Air Speeds
2. Inviscid Hypersonic Flow Over Blunt-Nosed Slender Bodies
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