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Influence of Coanda surface curvature on performance of bladeless fan

Authors :
Toshiaki Setoguchi
Heuy Dong Kim
Li Guoqi
Hu Yongjun
Yingzi Jin
Source :
Journal of Thermal Science. 23:422-431
Publication Year :
2014
Publisher :
Springer Science and Business Media LLC, 2014.

Abstract

The unique Coanda surface has a great influence on the performance of bladeless fan. However, there is few studies to explain the relationship between the performance and Coanda surface curvature at present. In order to gain a qualitative understanding of effect of the curvature on the performance of bladeless fan, numerical studies are performed in this paper. Firstly, three-dimensional numerical simulation is done by Fluent software. For the purpose to obtain detailed information of the flow field around the Coanda surface, two-dimensional numerical simulation is also conducted. Five types of Coanda surfaces with different curvature are designed, and the flow behaviour and the performance of them are analyzed and compared with those of the prototype. The analysis indicates that the curvature of Coanda surface is strongly related to blowing performance, It is found that there is an optimal curvature of Coanda surfaces among the studied models. Simulation result shows that there is a special low pressure region. With increasing curvature in Y direction, several low pressure regions gradually enlarged, then begin to merge slowly, and finally form a large area of low pressure. From the analyses of streamlines and velocity angle, it is found that the magnitude of the curvature affects the flow direction and reasonable curvature can induce fluid flow close to the wall. Thus, it leads to that the curvature of the streamlines is consistent with that of Coanda surface. Meanwhile, it also causes the fluid movement towards the most suitable direction. This study will provide useful information to performance improvements of bladeless fans.

Details

ISSN :
1993033X and 10032169
Volume :
23
Database :
OpenAIRE
Journal :
Journal of Thermal Science
Accession number :
edsair.doi...........cdcf0909b5a6ca155e6e50055be34000
Full Text :
https://doi.org/10.1007/s11630-014-0725-3