Jet-Spike Bifurcation in High-Speed Flows
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7913
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1430
Reference25 articles.
1. Theoretical and experimental study of the possibility of reducing aerodynamic drag by employing plasma injection
2. Interaction of shock waves with a pulse electrical discharge
3. Influence of a counterflow plasma jet on supersonic blunt body pressures
4. Blunt-Body Wave Drag Reduction Using Focused Energy Deposition
5. An outlook of CEM multidisciplinary applications
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