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Porous coatings can stabilize hypersonic boundary layers by absorbing grazing unstable modes. This numerical study aims at resolving such effects using high-order schemes and methods, and unveil some side-effects caused by these coatings on the near-field and wall pressure oscillations.

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This page is a summary of: Numerical Analysis of Porous Coatings Stabilizing Capabilities on Hypersonic Boundary-Layer Transition, AIAA Journal, July 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059830.
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