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In high-speed engine inlets, shock waves interacting with the near-wall flow can have significant detrimental effects on the propulsion system. We help to clarify how vortex generators, a type of passive flow control device, can be used to mitigate these negative effects.

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This page is a summary of: Mach 3.5 Compression Corner Control Using Microvortex Generators, AIAA Journal, May 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j063469.
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