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This article investigates the aerodynamic instabilities in the vaneless diffuser of a centrifugal compressor used in turbochargers, focusing on the effects of asymmetric boundary conditions. Through numerical simulations and sensitivity analysis, it identifies that the instability is primarily influenced by flow interactions near the shroud and the backflow regions. The study contributes to understanding stall mechanisms and provides insights into improving compressor design without significantly increasing

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ubig88w4iu

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