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Porous coatings have been demonstrated to greatly suppress the Mack second mode, and then delay hypersonic transition. We show the recent development of theoretical models to descript the stabilization effect of the coatings on the hypersonic flow.
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This page is a summary of: Theoretical Modeling of Porous Coatings with Simple Microstructures for Hypersonic Boundary-Layer Stabilization, AIAA Journal, February 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058403.
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