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The steps could affect the boundary layer transition. We show for the first time that the backward-facing step could destabilize the boundary layer and shift the transition upstream, whereas, the forward-facing steps could suppress the second-mode disturbances and shifts the transition downstream.

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This page is a summary of: Influences of Steps on the Hypersonic Boundary-Layer Transition on a Cone, AIAA Journal, October 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059888.
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