Volume 5, Issue 1, March 2020, Page: 11-19
Wind Tunnel Test Research on Aerodynamic Characteristics of Iced Conductors
Li Li, School of Civil Engineering & Mechanics, Huazhong University of Science and Technology, Wuhan, P. R. China
Guo Li, School of Civil Engineering & Mechanics, Huazhong University of Science and Technology, Wuhan, P. R. China
Huajin Cao, China Railway Siyuan Survey and Design Group Co., Ltd., Wuhan, P. R. China
Received: Dec. 5, 2019;       Accepted: Dec. 12, 2019;       Published: Apr. 1, 2020
DOI: 10.11648/j.aas.20200501.12      View  312      Downloads  77
Aiming at that the wind tunnel tests on aerodynamic characteristics of iced conductors were not systematic enough, the wind tunnel test for different icing types was conducted to study the aerodynamic characteristics of iced conductors more systematically. It can accounts for the characteristics of structure and wind field. The aerodynamic characteristics of different icing types such as crescent, fan and corona shapes with different icing thickness were obtained, and the effect of mean wind speed, turbulence and two-dimensional flow on aerodynamic characteristics were also investigated. It is concluded that the icing shapes have much effect on aerodynamic characteristics. The aerodynamic characteristics of rigid segment model with crescent-shaped are regular, while these of corona-shaped and fan-shaped have more peaks and troughs. In addition, the aerodynamic instability of iced conductors is more pronounced in turbulence. Furthermore, the wind speed has significant effects on drag coefficient, but the effects on lift coefficient is little.
Galloping, Aerodynamic Characteristic, Wind Tunnel Test, Iced Conductor
To cite this article
Li Li, Guo Li, Huajin Cao, Wind Tunnel Test Research on Aerodynamic Characteristics of Iced Conductors, Advances in Applied Sciences. Vol. 5, No. 1, 2020, pp. 11-19. doi: 10.11648/j.aas.20200501.12
Copyright © 2020 Authors retain the copyright of this article.
This article is an open access article distributed under the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0/) which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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