AIAA SCITECH 2022 Forum 2022
DOI: 10.2514/6.2022-2553
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Control of Shock Positions in a Supersonic Duct by Plasma Array

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Cited by 6 publications
(4 citation statements)
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“…By analyzing cross-flow pressure distributions for single and triple plasma filament configurations as well as observing carbon dioxide Mie scattering, the predicted effect is now experimentally demonstrated at M = 4. For various conditions [12][13][14]23], including supersonic flows with M = 2 and M = 4, filamentary plasma authority has been well demonstrated. This essentially thermal interaction mechanism is illustrated in Figure 11: with a high local gas temperature, the multifilamentary plasma zone presents an array of longitudinal subsonic jets enclosed in a supersonic flow.…”
Section: Discussionmentioning
confidence: 92%
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“…By analyzing cross-flow pressure distributions for single and triple plasma filament configurations as well as observing carbon dioxide Mie scattering, the predicted effect is now experimentally demonstrated at M = 4. For various conditions [12][13][14]23], including supersonic flows with M = 2 and M = 4, filamentary plasma authority has been well demonstrated. This essentially thermal interaction mechanism is illustrated in Figure 11: with a high local gas temperature, the multifilamentary plasma zone presents an array of longitudinal subsonic jets enclosed in a supersonic flow.…”
Section: Discussionmentioning
confidence: 92%
“…It creates a new SW, similar to solid obstacles, but much faster than any mechanical element. In an advanced approach [12][13][14], a spatial modulation of gas temperature is credited with redistributing pressure in the flowfield. High gas temperatures result in higher sonic velocity in the plasma zone, resulting in faster propagation of pressure disturbances or even the appearance of subsonic channels within supersonic flows.…”
Section: Introductionmentioning
confidence: 99%
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