Study of the Effect of Glow Discharges Near a M = 3 Bow Shock
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.28515
Reference29 articles.
1. Flow control using various plasma and aerodynamic approaches (Short review)
2. Plasmas in high speed aerodynamics
3. Strong double-layer formation by shock waves in nonequilibrium plasmas
4. Shock wave propagation and dispersion in glow discharge plasmas
5. Shock wave structure and velocity at propagation through non-homogeneous plasma
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