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Abstract

Centrifugal fans are widely used in the ventilation and domestic appliance industries. Their aerodynamic and aeroacoustic characteristics vary significantly in different application scenarios and operating conditions. This study applied a double-suction multiblade centrifugal fan to a range hood. The full three-dimensional flow and acoustic field were calculated synchronously using direct computational aeroacoustics (CAA) based on the lattice Boltzmann method (LBM) to investigate the internal flow, aerodynamic noise, and acoustic source characteristics of the fan under different operating conditions. We focused on two typical operating conditions: the maximum volume flow rate and working volume flow rate. The accuracy of the numerical simulation was verified using experimental data measured from the performance test bench and the semianechoic chamber. The flow field results show that more than 70% of the airflow enters the volute from the main wind inlet; this asymmetric wind intake condition creates an asymmetric flow pattern inside the volute. Acoustic waves radiate to the far-field mainly through the inlet and outlet of the range hood. The propagation characteristics of a dipole source are not very obvious and the tonal noise associated with the blade passage frequency (BPF) is not significant. In addition to the acoustic sources identified in the impeller region, the volute tongue, and the gap between the impeller and the inlet nozzle, two other significant acoustic sources are identified in the outlet collector and inlet nozzle regions.

Details

1009240
Title
Numerical Investigation of the Aerodynamic and Aeroacoustic Characteristics of a Double-suction Centrifugal Fan under Different Operating Conditions
Publication title
Volume
18
Issue
6
Pages
1412-1429
Publication year
2025
Publication date
Jun 2025
Section
Regular Article
Publisher
Isfahan University of Technology
Place of publication
Isfahan
Country of publication
Iran
ISSN
1735-3572
e-ISSN
1735-3645
Source type
Scholarly Journal
Language of publication
English
Document type
Journal Article
Publication history
 
 
Milestone dates
2025-03-30 (Issued); 2025-03-30 (Published)
ProQuest document ID
3185984203
Document URL
https://www.proquest.com/scholarly-journals/numerical-investigation-aerodynamic-aeroacoustic/docview/3185984203/se-2?accountid=208611
Copyright
© 2025. This work is published under https://creativecommons.org/licenses/by-nc-nd/4.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
Last updated
2025-08-25
Database
ProQuest One Academic