Impact of a Near-Surface Plasma Region on the Bow Shock Wave and Aerodynamic Characteristics of a High-Speed Model in Xenon
The main objective of this study is to demonstrate the active influence on the location of the bow shock wave, as well as on the parameters of an aerodynamic body, of a gas discharge organized near the frontal surface, between the body and the bow shock wave. The research is carried out using both e...
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Veröffentlicht in: | Fluids (Basel) 2024-11, Vol.9 (12), p.277 |
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Format: | Artikel |
Sprache: | eng |
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