In this study, a hybrid aeroacoustic prediction approach incorporating the effects of a rotating system is proposed to calculate the aerodynamic noise generated by centrifugal fan operation. Additionally, the blockage effect caused by the impeller on the propagation of broadband noise is investigated. The relative motion between the rotating impeller and the volute is modeled using a sliding grid technique. The Improved Delayed Detached-Eddy Simulation (IDDES) is employed to resolve the flow field and compute the acoustic source term, which is subsequently coupled with the Acoustic Perturbation Equations (APEs) to simulate the generation and propagation of the fan noise. The flow and acoustic fields are solved simultaneously on a single grid, eliminating the need to store large datasets and avoiding interpolation errors between grids. The accuracy of the approach is validated using benchmark acoustic problems. Comparison of the numerical results of the centrifugal fan with the experimental data shows that the deviation in Overall Sound Pressure Level (OASPL) at the four microphone locations ranges from 1.9 dB to 3.4 dB, demonstrating the validity of the approach in predicting aeroacoustic behavior in complex rotating systems. Furthermore, the blockage effect of the impeller on noise propagation is investigated in detail. For acoustic sources located in the volute tongue region, this effect not only influences the spatial distribution of acoustic energy but also causes a shift and redistribution of acoustic energy across different frequency bands.
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