Introduction
A great number of researches in the recent years deal with the problem of non-equilibriums plasma flow control in aerodynamics [1]. Different approaches are used for efficient flow moderation with energy deposition in a boundary layer, compression wave area, duct inlets and others [1, 2, 3]. Energy input using pulse discharge plasmas appeared to be rather promising. Pulse and pulse-periodic energy supply is the most effective way to improve high-speed flow characteristics; shock waves arising from local pulse energy input area may influence high speed flow with shock configurations.
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Jin, J., Koroteev, D., Mursenkova, I., Sysoev, N., Znamenskaya, I. (2012). Two Modes of Shock Interaction with Zone of Pulse Volume Discharges in the Channel. In: Kontis, K. (eds) 28th International Symposium on Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-25685-1_134
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DOI: https://doi.org/10.1007/978-3-642-25685-1_134
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