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Hypersonic flight faces challenges like heat and vibration due to shock waves. To address this technical challenge, we investigate using phononic metamaterials (PMs) as a passive flow control mechanism. Experimental results showcase the material's ability to reduce turbulent fluctuations, providing experimental evidence on applying phononic metamaterials for flow control in hypersonic flight.

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This page is a summary of: Flow Control of Hypersonic Shock-Wave/Boundary-Layer Interactions Using Phononic Metamaterials, January 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2024-0031.
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