Effect of serrated trailing-edge blades on aerodynamic noise of an axial fan

被引:16
作者
Ye, Xuemin [1 ]
Zheng, Nan [2 ]
Zhang, Ruixing [3 ]
Li, Chunxi [1 ]
机构
[1] North China Elect Power Univ, Hebei Key Lab Low Carbon & High Efficiency Power, Baoding 071003, Peoples R China
[2] North China Elect Power Univ, Natl Thermal Power Engn & Technol Res Ctr, Sch Energy Power & Mech Engn, Minist Educ,Key Lab Condit Monitoring & Control P, Beijing 102206, Peoples R China
[3] North China Elect Power Univ, Dept Mech Engn, Baoding 071003, Peoples R China
基金
中国国家自然科学基金;
关键词
Serrated trailing-edge; Variable-pitch axial fan; Aerodynamic performance; Noise; Wake vortex; FLAT-PLATE; SELF-NOISE; REDUCTION; FLOW; AIRFOIL; PERFORMANCE; PREDICTION; AEROFOIL; DESIGN;
D O I
10.1007/s12206-022-0526-7
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A bionic geometric modification inspired by the trailing-edge serrations of owl wings provides a new approach for controlling the aerodynamic noise of rotary fluid machinery. The effect of different serrated trailing-edges (STEs) on aerodynamic performance and noise of a single-stage variable-pitch axial fan was numerically investigated using steady Reynolds averaged Navier-Stokes and large eddy simulation model, respectively. Results show that STEs could improve fan efficiency at the design and low flow rates, and significantly reduce the noise in the middle- and low-frequency as well as suppress the pressure pulsation of airflow. STEs split large-scale vortices into small ones by intensifying the turbulent flow mixing. STEs with appropriate serration parameters improve the spanwise distribution of the vortex, reduce the span dimension of wake vortices, and induce wake vortices distribution to be more uniform. The innovation of this paper is that a novel blade with partial serrations is presented for the realization of the apparent noise reduction and more preferred aerodynamic performance of the axial fan by improving serration parameters and rearranging the region of the serration.
引用
收藏
页码:2937 / 2948
页数:12
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