On the application of resonators for controlling flow noise in a stick-type vacuum cleaner

Abstract This study explores a novel resonator design to reduce airflow noise in a vacuum cleaner. The design parameters were established to target noise reduction within the frequency range of approximately 1 kHz to 5 kHz. The resonator design, geometrically integrated with the vacuum cleaner body and flow line, was initially modeled using the 1D Transfer Matrix Method (TMM) and subsequently evaluated through numerical FEM simulations. Following the acoustic analyses, flow simulations were conducted to determine the pressure drop across the resonator and assess its overall aerodynamic impact on the system. The acoustic performance of the final design was assessed through FEM-based Sound Transmission Loss (STL) predictions and whole-machine A-weighted sound power measurements with the manufactured prototype installed. The sound power measurements demonstrated the effectiveness of the design within the targeted frequency range, while the STL predictions characterized its acoustic transmission behavior.

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Publication Details

Journal
Engineering Research Express
Published
2026-10-28
DOI
https://doi.org/10.1088/2631-8695/aebaeb
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
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article

On the application of resonators for controlling flow noise in a stick-type vacuum cleaner

Haluk Erol, Türkay Karslı, Alperen Gençpelvan, Damla Duru Sevinir et al.
Engineering Research Express
Aerodynamics and Acoustics in Jet Flows
article

On the application of resonators for controlling flow noise in a stick-type vacuum cleaner

Haluk Erol, Türkay Karslı, Alperen Gençpelvan, Damla Duru Sevinir, Berkay Güler
article en

Abstract

Abstract This study explores a novel resonator design to reduce airflow noise in a vacuum cleaner. The design parameters were established to target noise reduction within the frequency range of approximately 1 kHz to 5 kHz. The resonator design, geometrically integrated with the vacuum cleaner body and flow line, was initially modeled using the 1D Transfer Matrix Method (TMM) and subsequently evaluated through numerical FEM simulations. Following the acoustic analyses, flow simulations were conducted to determine the pressure drop across the resonator and assess its overall aerodynamic impact on the system. The acoustic performance of the final design was assessed through FEM-based Sound Transmission Loss (STL) predictions and whole-machine A-weighted sound power measurements with the manufactured prototype installed. The sound power measurements demonstrated the effectiveness of the design within the targeted frequency range, while the STL predictions characterized its acoustic transmission behavior.

Engineering Research Express
Istanbul Technical University (TR)
Openalex Percentile: Top 19%
Aerodynamics and Acoustics in Jet Flows
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On the application of resonators for controlling flow noise in a stick-type vacuum cleaner — Haluk Erol, Türkay Karslı, et al. · Engineering Research Express (2026) | TGRS Research Map | TGRS