Reducing Blade Tonal Noise Generated by Vane‐Axial Fans

1973 ◽  
Vol 53 (1) ◽  
pp. 386-386
Author(s):  
J. V. Pierpoint
Keyword(s):  
Volume 1 ◽  
2004 ◽  
Author(s):  
T. Belamri ◽  
G. Wang

SPLNoise is an aeroacoustic program developed to predict tonal noise generated by low speed axial fans. It is based on a generalization of the acoustic analogy of Lowson. The main input to the program are the radial thrust and torque distribution along the blade. This radial distribution is obtained from a CFD calculation. An automatic link to CFX commercial CFD code was made. Noise testing was performed in the anechoic and reverberant room at the Trane Company. Comparison between predicted noise levels and experimental data is very satisfactory.


Noise Notes ◽  
2007 ◽  
Vol 6 (3) ◽  
pp. 37-46
Author(s):  
Anthony Gerard ◽  
Alain Berry ◽  
Patrice Masson

2009 ◽  
Vol 321 (1-2) ◽  
pp. 26-44 ◽  
Author(s):  
Anthony Gérard ◽  
Alain Berry ◽  
Patrice Masson ◽  
Yves Gervais

2009 ◽  
Vol 321 (1-2) ◽  
pp. 8-25 ◽  
Author(s):  
Anthony Gérard ◽  
Alain Berry ◽  
Patrice Masson ◽  
Yves Gervais

Author(s):  
Bo Luo ◽  
Wuli Chu ◽  
Wei Dong ◽  
Xiangyi Chen

Axial fans are widely used in modern industry and new regulations and stringent environmental concerns are prompting manufacturer to design efficient low-noise axial fans. This paper is focused on improving the aerodynamic performances and reducing the tonal noise at BPF and its harmonics by the optimum choice of lean-swept blade and the stacking line for the low-speed axial fan. The aerodynamic characteristics of the axial fan with a shroud are explored by CFD with ANASYS CFX. A hybrid method, SST turbulence model for flow and FW-H equation for acoustics, is chosen to predict the radiated noise. The accuracy and reliability of predicted aerodynamic and aeroacoustics results are verified by comparing both computation and experimental data. A number of modified blades with different leaned angle, swept angle and the stacking lines are modeled and analyzed, and the investigation into the optimum choice of lean-swept blade and the stacking line is conducted according to aerodynamic performances and tonal noise. Q-criterion which can visualize the major flow disturbances is applied for the purpose of identification of acoustic sources. The turbulent flow structures on the leading edge, tip and suction side of the blade are main noise sources. An optimal modification is determined through the analysis of the aerodynamic performances and noise, which is to achieve the desired performances by blade sweep and lean and adjusting the stacking line. The results show that aerodynamic and acoustic performances of the optimized fan are better than that of the original fan and the improvement is more obvious to change the stacking line with centre of gravity compare to blade sweep and lean for the low-speed axial fan.


2007 ◽  
Vol 38 (4) ◽  
pp. 12-18
Author(s):  
Anthony Gérard ◽  
Alain Berry ◽  
Patrice Masson

Author(s):  
Edward Canepa ◽  
Andrea F. Cattanei ◽  
Fabio Mazzocut Zecchin ◽  
Gabriele Milanese ◽  
Davide Parodi

Author(s):  
Tania Marie Arispe Angulo ◽  
Waldir de Oliveira ◽  
Ramiro Gustavo Ramirez Camacho ◽  
Edna da Silva ◽  
GERMÁN ENRIQUE NIÑO DEL RÍO

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