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High-voltage plasma is applied to a hypersonic body in the quiet Mach 6 wind tunnel at Purdue Universtiy. The effects of the plasma are studied through flow imaging and surface pressure measurements.

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This page is a summary of: Plasma Perturbations on an Oberkampf Geometry in Quiet Mach 6 Flow, January 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2024-1519.
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