Prediction Method of Unsteady Combustion Around Hypersonic Projectile in Stoichiometric Hydrogen-Air
Author:
Affiliation:
1. Keio University, Yokohama 223-8522, Japan
2. Institute of Space and Astronautical Science, Sagamihara 229-8510, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.299
Reference18 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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