Binary scaling limits for hypersonic flight.
Author:
Affiliation:
1. Canadian Armament Research and Development Establishment, Valcartier, Quebec, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4284
Reference9 articles.
1. Correspondence between Normal-Shock and Blunt-Body Flows
2. APPROXIMATE METHOD FOR HYPERSONIC NONEQUILIBRIUM BLUNT BODY AIRFLOWS
3. Non-equilibrium flow of an ideal dissociating gas
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