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The intake buzz is the self-excited oscillation of the shock wave occurring in supersonic and hypersonic intakes. We test the effects of the inflow/outflow rate balance on the buzz characteristics. Based on the results, we propose novel domination mechanism of the buzz.
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This page is a summary of: Investigation of Intake Buzz Focusing on Shock Wave Movement and Inflow/Outflow Balance, Journal of Propulsion and Power, May 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b39483.
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