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The paper investigates the fluid dynamics mechanism for the observed sharp increase in viscous drag in turbulent boundary layers over acoustic absorbing panels when subjected to high sound levels. This is relevant to aircraft engine nacelles and parts of a fuselage subjected to high sound levels.

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This page is a summary of: Mechanism for Increased Viscous Drag over Porous Sheet Acoustic Liners, AIAA Journal, August 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059039.
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