Electroaerodynamics and the effect of an electric discharge on cone/cylinder drag at Mach 5
Author:
Affiliation:
1. Defence Evaluation and Research Agency, Farnborough, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-602
Reference30 articles.
1. Sonic and shock waves in gas-discharge plasma
2. Phenomenological Analysis of Shock-Wave Propagation in Weakly Ionized Plasmas
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