Numerical Study of Plasma-Assisted Aerodynamic Control for Hypersonic Vehicles
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio, 45433-7512
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.39032
Reference32 articles.
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5. Hypersonic Flow over a Blunt Body with Plasma Injection
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