Hypersonic Double-Cone Flow with Applied Magnetic Field
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, University of Tokyo, Tokyo 113-8656, Japan
2. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Kanagawa 252-5210, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A32351
Reference27 articles.
1. Hypersonic Aerothermodynamics
2. AndersonJ. D.Jr., Modern Compressible Flow, 3rd ed., McGraw-Hill, New York, 2004, pp. 552–553.
3. Hypersonic and High-Temperature Gas Dynamics, Second Edition
4. Experiment on Drag Enhancement for a Blunt Body with Electrodynamic Heat Shield
5. Experimental Verification of Heat-Flux Mitigation by Electromagnetic Fields in Partially-Ionized-Argon Flows
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