Experimental Investigation of the Sound Emission of Skewed Axial Fans with Leading-Edge Serrations

被引:32
作者
Kroemer, Florian [1 ,2 ]
Czwielong, Felix [1 ]
Becker, Stefan [1 ]
机构
[1] Friedrich Alexander Univ Erlangen Nurnberg, Inst Proc Machinery & Syst Engn, Cauerstr 4, D-91058 Erlangen, Germany
[2] Vienna Univ Technol, Inst Mech & Mechatron, Getreidemarkt 9-32, A-1060 Vienna, Austria
关键词
TIP CLEARANCE NOISE; FLOW ROTORS; TURBULENCE; REDUCTION; PERFORMANCE; DESIGN; SWEEP; FIELD;
D O I
10.2514/1.J058134
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Axial fans represent a major source of noise in technical systems. Based on investigations on airfoils, a promising measure for reducing the sound emission of such systems with axial fans is the application of leading-edge serrations to the fan blade. Hence in this study, the joint impact of fan-blade skew-as a commonly used noise-reduction approach-and leading-edge serrations on the sound emission of low-speed axial fans was investigated. Forward-, backward-, and unskewed fans with five different leading-edge modifications were used. For each fan, a reference configuration with straight leading edges and four configurations with sinusoidal leading-edge serrations (with two different amplitude values and two different wavelength values) were examined. The results show that, among the reference fans with unmodified leading edges, the forward-skewed fan had the lowest sound emission. The serrations applied to the unskewed fan lead to an increase in the efficiency and a decrease in the sound emission. When applied in combination with fan-blade skew, the serrated fans showed an even lower sound emission and a higher efficiency-even the forward-skewed fan, which already has a low sound emission without any leading-edge modifications. The highest sound reduction was achieved by applying the serrations with the smallest wavelength and the highest amplitude. The findings prove that even for low-noise fans with forward-skewed fan blades, a further sound reduction is possible with the use of leading-edge serrations.
引用
收藏
页码:5182 / 5196
页数:15
相关论文
共 50 条
[41]   Numerical Investigation on the Effect of Leading-Edge Tubercles on the Laminar Separation Bubble [J].
Sathyabhama, A. ;
Sreejith, B. K. .
JOURNAL OF APPLIED FLUID MECHANICS, 2022, 15 (03) :767-780
[42]   Numerical and experimental investigation of bionic airfoils with leading-edge tubercles at a low-Re in considering stall delay [J].
Fan, Menghao ;
Sun, Zhaocheng ;
Dong, Xiangwei ;
Li, Zengliang .
RENEWABLE ENERGY, 2022, 200 :154-168
[43]   Experimental Investigation of a Wavy Leading Edge Cylinder [J].
Ferreira, Paulo H. ;
Moura, Rodrigo C. ;
Araujo, Tiago B. .
AIAA AVIATION 2022 FORUM, 2022,
[44]   CFD analysis of the aerodynamic performance of airfoils with leading-edge tubercles: A parametric investigation [J].
Luo, Dahai ;
Lu, Bingxiao ;
Bai, Yihao ;
Yang, Haojie .
OCEAN ENGINEERING, 2025, 331
[45]   Experimental investigation of the 3D unsteady flow field downstream of axial fans [J].
Kergourlay, Gerald ;
Kouidri, Smaine ;
Rankin, Gary W. ;
Rey, Robert .
FLOW MEASUREMENT AND INSTRUMENTATION, 2006, 17 (05) :303-314
[46]   Hydroacoustic and hydrodynamic investigation of bio-inspired leading-edge tubercles on marine-ducted thrusters [J].
Stark, Callum ;
Shi, Weichao .
ROYAL SOCIETY OPEN SCIENCE, 2021, 8 (09)
[47]   Influence of leading-edge obstacles on flow field and noise of axial flow fan for building ventilation [J].
Yu, Tao ;
Yao, Hailu ;
Mi, Ruiyang ;
Song, Yongxing ;
Liu, Peng .
JOURNAL OF BUILDING ENGINEERING, 2025, 109
[48]   An experimental investigation of aerodynamic and aeroacoustic performance of a wind turbine airfoil with trailing edge serrations [J].
Cao, Huijing ;
Zhou, Teng ;
Zhang, Yinan ;
Zhang, Mingming .
JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2022, 151 (02) :1211-1222
[49]   INVESTIGATION OF THE LEADING-EDGE EROSION OF WIND TURBINE BLADES USING MULTIVARIANT ANALYSIS METHOD [J].
Alajmi, Abdullah F. ;
Ramulu, M. .
PROCEEDINGS OF ASME 2022 INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, IMECE2022, VOL 6, 2022,
[50]   Numerical investigation on cavitation and induced noise reduction mechanisms of a three-dimensional hydrofoil with leading-edge protuberances [J].
Yang, Chen ;
Zhang, Jinsong ;
Huang, Zhenwei .
PHYSICS OF FLUIDS, 2024, 36 (05)