Chapman-Jouguet Oblique Detonation Structure Around Hypersonic Projectiles
Author:
Affiliation:
1. Muroran Institute of Technology, Muroran 050-8585, Japan
2. Nagoya University, Nagoya 464-8603, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1480
Reference27 articles.
1. A missile technique for the study of detonation waves.
2. Mechanism of Instabilities of Exothermic Hypersonic Blunt-Body Flows
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