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Study on noise reduction mechanism of aerodynamic noise in axial flow fans based on multiple combined noise reduction structures
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Yichen YE1, Yuan HE2, Zhunyuan SHAO2, Canxing WANG1, 2
Fluid Machinery | 2025, 53(12) : 38 - 46
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Fluid Machinery | 2025, 53(12): 38-46
Study on noise reduction mechanism of aerodynamic noise in axial flow fans based on multiple combined noise reduction structures
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Yichen YE1, Yuan HE2, Zhunyuan SHAO2, Canxing WANG1, 2
Affiliations
  • 1School of Aeronautics and Astronautics,Zhejiang University,Hangzhou 310027,China
  • 2Faculty of Engineering and Physical Sciences,University of Southampton,Southampton SO17 1BJ,UK
Published: 2025-12-31 doi: 10.3969/j.issn.1005-0329.2025.12.005
Outline
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To address the aerodynamic noise issue in axial flow fans caused by tip leakage flow,a noise reduction structure combining “bionic serrations-suction surface tip winglet modification-multi‑scheme grooving” was designed.Using the SBES(stress‑blended eddy simulation) turbulence model coupled with the FW-H acoustic analogy method,the noise reduction mechanisms of each structure were analyzed.The results show that the combination of a biomimetic wavy leading‑edge serration with a suction side tip winglet modification can reduce the overall sound pressure level by 4.5dB.Further combining this with a tip longitudinal airfoil ribbed slot structure leads to a reduction of 7.9dB in the overall sound pressure level.The biomimetic leading‑edge serration-suction side tip winglet modification reduces the discrete noise peaks by disrupting the periodic shedding of leakage vortices,optimizes the flow uniformity at the tip,and suppresses abrupt local pressure fluctuations.The combined structure of biomimetic leading‑edge serrations,tip longitudinal airfoil ribbed slots,and suction side tip winglets accelerates vortex energy dissipation by dynamically dividing the leakage flow paths.In experiments,the prototype demonstrated significant noise reduction effects,and the observed phenomenon of “low‑frequency noise energy shifting to high frequencies” was consistent with the numerical simulation results,verifying the reliability of the proposed method.This study provides a reference for the optimization design of low‑noise axial flow fan tips.

SBES turbulence model  /  tip clearance  /  suction side tip winglet modification  /  biomimetic serration  /  aerodynamic noise  /  vortex breakdown  /  noise reduction mechanism
叶一辰, 何源, 邵准远, 王灿星. 基于多种组合降噪结构对轴流风机气动噪声的降噪机理研究. 流体机械, 2025 , 53 (12) : 38 -46 . DOI: 10.3969/j.issn.1005-0329.2025.12.005
Yichen YE, Yuan HE, Zhunyuan SHAO, Canxing WANG. Study on noise reduction mechanism of aerodynamic noise in axial flow fans based on multiple combined noise reduction structures[J]. Fluid Machinery, 2025 , 53 (12) : 38 -46 . DOI: 10.3969/j.issn.1005-0329.2025.12.005
Year 2025 volume 53 Issue 12
138
58
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Article Info
doi: 10.3969/j.issn.1005-0329.2025.12.005
  • Receive Date:2025-03-24
  • Online Date:2026-10-22
  • Published:2025-12-31
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  • Received:2025-03-24
  • Revised:2025-10-21
Affiliations
    1School of Aeronautics and Astronautics,Zhejiang University,Hangzhou 310027,China
    2Faculty of Engineering and Physical Sciences,University of Southampton,Southampton SO17 1BJ,UK
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表12种不同金属材料的力学参数
科
Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
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属
Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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